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Wireless Power Transmission
       EE563-Graduate Seminar
        Fall 2004    Group 5
           Alan Chun-yip Yeung
              Leanne Cheung
              Jeff Samandari
            Wehibe Belachew
                Tesfa Mael
             Jose A. Becerra
Presentation Outline

1. Introduction //Background
1. Introduction Background

2. Theory of Wireless Power Trans.
2. Theory of Wireless Power Trans.

3. Major Research Projects
3. Major Research Projects

4. Comparison of Efficiency …
4. Comparison of Efficiency …

5. Proposed Project/Experiment
5. Proposed Project/Experiment

6. Conclusion
6. Conclusion
1. Introduction // Background
1. Introduction Background
Outline
•   History/Background
•   Solar Power Satellite
•   Microwave Power Transmission
•   Conclusion



    Reference:
    http://www.kentlaw.edu/classes/fbosselm/Spring2004/Power
    Points/Wireless%20Power%20Transmission%20-
    %20Soubel.ppt
Background, Nikola Tesla
• 1856-1943
• Innovations:
   – Alternating current
   – Wireless power
     transmission
     experiments at
     Wardenclyffe
Wardenclyffe
• 1899
   – Able to light lamps
     over 25 miles away
     without using wires
   – High frequency
     current, of a Tesla
     coil, could light
     lamps filled with
     gas (like neon)
1940’s to Present
• World War II developed ability to convert
  energy to microwaves using a magnetron,
  no method for converting microwaves
  back to electricity
• 1964 William C. Brown demonstrated a
  rectenna which could convert microwave
  power to electricity
Solar Power from Satellites
• 1968’s idea for Solar Power Satellites
  proposed by Peter Glaser
  – Would use microwaves to transmit power to
    Earth from Solar Powered Satellites
• Idea gained momentum during the Oil
  Crises of 1970’s, but after prices stabilized
  idea was dropped
  – US Department of Energy research program
    1978-1981
Problems
• Issues identified during the DOE study
   – Complexity—30 years to complete
   – Size—6.5 miles long by 3.3 miles wide
      • Transmitting antenna ½ mile in
        diameter(1 km)

  – Cost—$74 billion
  – Interference
From the Satellite
• Solar power from the satellite is sent
  to Earth using a microwave
  transmitter
• Received at a “rectenna” located on
  Earth
• Recent developments suggest that
  power could be sent to Earth using a
  laser
Microwaves
• Frequency 2.45 GHz microwave
  beam
• Retro directive beam control
  capability
• Power level is well below international
  safety standard
Microwave vs. Laser Transmission
• Microwave                  • Laser
  – More developed             – Recently developed
  – High efficiency up to        solid state lasers allow
    85%                          efficient transfer of
  – Beams is far below the       power
    lethal levels of           – Range of 10% to 20%
    concentration even for       efficiency within a few
    a prolonged exposure         years
  – Cause interference         – Conform to limits on
    with satellite               eye and skin damage
    communication
    industry
Rectenna
  “An antenna comprising a mesh of
    dipoles and diodes for absorbing
    microwave energy from a transmitter
    and converting it into electric power.”
• Microwaves are received with about
  85% efficiency
• Around 5km across (3.1 miles)
• 95% of the beam will fall on the
  rectenna
5,000 MW Receiving Station
(Rectenna). This station is about a
       mile and a half long.
2. Theory of Wireless Power Trans.
2. Theory of Wireless Power Trans.
Theory of Operation
•   Electromagnetic Radiation
•   Antenna basics
•   Phased-array antenna
•   Diffraction analogy
•   Energy distribution
•   Rectenna
•   Physical limitations & relationships
Physics of Wireless Power
                     Transmission
                                                                   • Forms of
                                                                     Electromagnetic
                                                                     radiation
                                                                   • Travel at same speed
                                                                   • F = frequency
                                                                   • C = velocity of light
•http://imnh.isu.edu/digitalatlas/clima/atmosph/images/waves.jpg   • L =wavelength
Dipole Antenna
• Transmission of power
  is simpler than TV &
  Radio
• Transmitter: wire half a
  wavelength
• Pushes electrons back
  and forth
• Receiver: wire half a
  wavelength


                             http://www.zorg.org/radio/dipole_antenna.shtml
Antenna Radiation Pattern




  http://www.astromag.co.uk/portable/dipole.gif
Phased-array antenna
                                                           • The λs for microwaves
                                                             are small  dipoles small
                                                           • Beam focusing: phased-
                                                             array antenna
                                                           • Electronically steered by
                                                             varying the timing or
                                                             phase
                                                           • Waves will merge
                                                             together



http://www.mcs.harris.com/oceannet/features/antenna.html
Phased-Array Antenna




http://www.cea.com.au/products/phasedarray/i2_ceafar.html
Diffraction analogy
• Light same properties
• Laser beam shinning
  trough a narrow
  opening & spreads
  out or diffracts
• Bright spot in the
  center w/fainter spots
  on the side




                           http://planetquest.jpl.nasa.gov/technology/diffraction.html
Diffraction & Microwaves
            • Waves reinforce at
              some points and they
              cancel out at other
              points (bright and
              fainter points)
            • In microwaves: is a
              scaled up version of
              diffraction
Intensity
Main lobe energy
• Circular central max
 Main lobe
• 84% of energy
• Sidelobes surround
• No energy  minima
Intensity 84% in main lobe
Rectenna
    • Array of dipole
      antennas known as
      rectifying antenna or
      Rectenna
    • Diameter = Dr
Rectenna
Physical Limitations
• The receiving diameter Dr increases with
  transmitter receiver separation distance S.
• Dr increases if transmitter diameter Dt
  decreases
Physical Limitations
2. Sample Calculations
2. Sample Calculations
Calculations/Analysis

• Frequency, f (Hz)
• Intensity, I (watts per square meter)
• Wave-Length, L (meters)
• Received Main Beam Lope (“spot”) Diameter, Dr
  (meters or kilometers)
• Transmitting Phased Array Diameter, Dt (meters
  or kilometers)

• Example: how to estimate Intensity, I ?
Frequency                              Formula

                        Dt * Dr
• Frequency, f (Hz) = --------------        (2)
                        (L * S)

     Dt: transmitting phased array diameter
     Dr: received main beam lobe (“spot”)
          diameter
     L:   wavelength
     S:   separation
Frequency                                         Analysis

                            Dt * Dr
If   (Frequency, f (Hz) = ----------- ) ≥ 2.44 GHz          (2)
                            (L * S)
Then at least, 84% of the energy of the beam will be captured

Note:
• This energy is not linear; 42% of the energy is not
  equivalent to 1.22 GHz.
• Equation (2) represent a best case scenario.
• Practical antenna sizes may have to be larger if most of
  the beam is to be captured.
• The rectenna will have to be at least as large as Dt,
  even if (2) says Dr is smaller.
Frequency                                               Analysis


• Such a wide beam can be focused, but only to a minimum size Dr.

• For low Earth-orbit power-beaming demonstrations, it is easier to
  put the smaller antenna in space and the larger antenna on
  Earth.

• Early demonstrations may capture only a small percentage of the
  total power, in order to keep antenna sizes small.
   – to light up a 60 watt bulb, thousands of watts may have to be
      transmitted.
   – Since costly to launch such a power generating apparatus, the
      most feasible demonstration project may be Earth-to-space
      transmission from a large transmitting antenna (such as the
      Arecibo dish) to a smaller rectenna in space.
Intensity, I                                     Formula


• Intensity, I (watts per square meter)
                          P           Dt
             = ½ ( Pi * -----) * ( --------- )         (3)
                          4         L*S

      Pi:    3.14…
      P:     total power transmitted
      Dt:    transmitted phased array diameter
      L:     wave length
      S:     transmitter to receiver distance (separation)
Wave-Length, L                                      Calculations



• Wave-Length, L (meters)
     c         300,000,000 meter/sec
 = ----- = ( -------------------------------- ) = 0.1224   (1)
     f         2,450,000,000/sec                meter


     c:      speed of light
     f:      frequency
Received Main Beam Lope Diameter, Dr                      Calculations




• Received Main Beam Lope (“spot”) Diameter, Dr
  (meters or kilometers)
      f*L*S           2.44 * 0.12224m * 35,800,000m
  = -------------- = --------------------------------------------
          Dt                           1000m

  = 10,700 meter = 10.7 kilometers


       L:      wave length
       S:      separation
       Dt:     transmitting phased array diameter
Transmitting Phased Array Diameter, Dt                    Calculations



• Transmitting Phased Array Diameter, Dt (meters or
  kilometers)
      f*L*S            2.44 * 0.12224m * 35,800,000m
  = -------------- = ----------------------------------------------
         Dr                      10,700 meter

  = 1000m = 1 kilometers


       L:      wave length
       S:      separation
       Dr:     received main beam lope (“spot”) diameter
Example
What is the Intensity, I = ?
Given: f, Dr, and a typical solar power satellite transmitting 5
       billion watts from geostationary orbit 35800 kilometers
       high.

Solution: Use the following (1), (2), & (3)
             C
       f = -----            L                                      (1)
             L
                            Dt * Dr
       Frequency, f (Hz) = --------------              Dt          (2)
                            (L * S)
                                            P           Dt
       Intensity, I (watts/m^²) = ½ ( Pi * -----) * ( --------- )   (3)
                                            4          L*S
Example                                                               Calculations


• Intensity, I (watts per square meter)

              P            Dt
  = ½ ( Pi * -----) * ( --------- )                                   (3)
              4         L*S

               2287485.869w                             1000m
  = ½ ( Pi * ---------------------------) * ( ----------------------------------- )
                       4m                       0.1224m* 35800,000m

  = 205 watts/m^² or                    20.5 milliwatts/cm^²
Example                                                Analysis


• peak beam intensity, Ip = 20.5 milliwatts/cm^²
   This is about twice US industrial standard for human exposure
   This is converted (by rectenna) to electricity by 90% efficiency


• Average intensity, Ia        ≈ 1/3 * 20.5 milliwatts/cm^²
Rectangular Transmitting antenna array                Calculations


• Mathematics slightly different, but the same general principles
  apply.
• Central maximum of the beam contain 82% of the transmitted
  energy.
• Rectangular in shape, but will spread out more along TX array’s
  short direction than its long direction.

• Example: Canada’s Radar sat
      rectangular transmitting antenna:    1.5m × 15m
      “footprint” on the ground:           7,000m × 50,000m
      frequency:                           5.3 GHz
      altitude:                            800,000m
      output power:                        5000 watts
   The power is too spread out at the ground to use in a practical
      demonstration project.
Two more points

1. Use certain transmitting methods
   – to reduce the level of the sidelobes
   – to put some of the sidelobe energy into the main
     lobe
   –  Price to pay: Larger Rectenna (because main
     lobe spreads out)

2. Principal of diffraction also limits the resolution of
   optical systems:
   – Lenses
   – Telescopes
3. Major Research Projects
3. Major Research Projects
1979 SPS Reference System concept
             (GEO)
Accomplishments of Solar Power
              Satellites
• 1980, 30 kW of microwave power was
  transmitted to a receiving antenna over
  one mile
• 1993, Japan successfully transmitted a
  800W microwave beam from a rocket to a
  free-flying satellite in space.
• 1998, Microwave to DC conversion
  efficiency of 82% or higher by the
  rectenna.
NASA’s 1995-1997 Fresh Look Study
• MEO (Mid-Earth Orbit)
  Sun Tower:

  - 6 SPS yields near 24-hr
  power to sites

  - ± 30 degrees Latitude
  Coverage

  - Power services of 200-
  400 MW
Continued
• Solar Disc

  - 1 SPS provides nearly 24-
  hr
    power to markets

  - Spin-stabilized solar array,
  de-spun phased array with
  electronic beam-steering

  - Geostationary Earth Orbit

  - ± 60 degrees Latitude
    Coverage

  - Power services of about 5
  GW
1999-2000 Space Solar Power (SSP)
   Exploratory Research and Technology
             (SERT) program
• Exploration and Commercial Development
Integral Symmetrical Concentrator
NASA’s SSP Strategic Research &
    Technology Roadmaps
SPS 2000
Details of SPS 2000

• Japan is to build a low cost
  demonstration of SPS by
  2025.

• Eight countries along the
  equator agreed to be the
  rectenna sites.

• 10 MW satellite delivering
  microwave power in the low
  orbit 1100 km(683 miles)
   – Will not be in
      geosynchronous orbit,
      instead low orbit 1100 km
      (683 miles)
   – Much cheaper to put a
      satellite in low orbit
Japan’s Recent Research Efforts
•   Japan
    - 2001, Japanese’s Ministry of Economy,
    Trade and Industry (METI) launched a
    research program for a solar-powered-
    generated satellite.

     - By 2040, beginning of a SPS operation. The
    planned satellite will be able to generate
    1GW/Sec. (equivalent to the output of a
    nuclear plant) in a geostationary orbit. The
    receiving antenna (rectenna) on the ground will
    be either positioned at desert or sea.
Japan’s Roadmaps for SPS
       Development
References
•   www.on-orbit-servicing.com/pdf/OOS2004_
    presentations_pdf/OOSIssuesOverview_Oda.pdf
•   www.kentlaw.edu/classes/fbosselm/Spring2004/ PowerPoints/Wireless
    %20Power%20Transmission%20-%20Soubel.ppt
•   www.spacefuture.com/.../a_fresh_look_at_space_
    solar_power_new_architectures_concepts_and_technologies.shtml
•   Lin, James C., “Space solar power stations, wireless power transmissions,
    and biological implications”, IEEE microwave magazine, March, 2002
4. Comparisons Among Other Power
4. Comparisons Among Other Power
Sources
Sources
Efficiency and Costs

•Space Solar Power (Wireless Power
Transmission)
•Ground Based Solar Power
•Nuclear Energy
•Fossil Fuel
Advantages over Earth-based solar power
• More intense sunlight
• In geosynchronous orbit, 36,000 km (22,369
  miles) an SPS would be illuminated over 99%
  of the time
• No need for costly storage devices for when
  the sun is not in view
Cont.
• Waste heat is radiated back into space
• Power can be beamed to the location where it
  is needed, don’t have to invest in as large a
  grid
• No air or water pollution is created during
  generation
• Ground based solar only works during clear
  days, and must have storage for night. Thus
  it is More reliable than ground based solar
  power
Advantages over Nuclear Power
There are advantages…
• Possible power generation of 5 to 10
  gig watts
• If the largest conceivable space
  power station were built and
  operated 24 hours a day all year
  round, it could produce the
  equivalent output of ten 1 million
  kilowatt-class nuclear power
  stations.
Cont…
• Nuclear power doesn't pollute the
  atmosphere like fossil fuels. But it does
  produce waste. This stays radioactive for
  thousands of years and is very dangerous. At
  the moment most stations bury their waste
  deep underground, at sea or send it to other
  countries. (Britain, for example, accepts and
  buries nuclear waste from several countries.)
Cont…
• One of the disadvantage of Nuclear
• On April 26, 1986 the worst catastrophe in nuclear
  history occurred in the station at Chernobyl, Ukraine.
• Due to the failure of one of reactor, two people died
  immediately from the explosion and 29 from radiation.
  About 200 others became seriously ill from the radiation;
  some of them later died. It was estimated that eight
  years after the accident 8,000 people had died from
  diseases due to radiation (about 7,000 of them from the
  Chernobyl cleanup crew). Doctors think that about
  10,000 others will die from cancer. The most frightening
  fact is that children who were not born when the
  catastrophe occurred inherited diseases from their
  parents.
• Source http://oii.org/html/story.html by Vessela
  Daskalova
Advantages over Fossil Fuel

• Fossil fuels won't last forever (next 50yrs)
• It is not renewable
• The ability to match supply to demand
  may already have run out, especially for
  oil
• Fossil Fuel fired electric power plants in
  the US emits about 2 billion tons of
  greenhouse gas CO2 in to air every year.
  This courses climate change in the future
  via greenhouse effect.
Cost


• Cost—prototype would have cost $74 billion

• “According to Kyle Datta the Oil Factor,”
  which predicts that oil could hit $100 a barrel
  by 2010.
Disadvantages
• If microwave beams carrying power could be
  beamed uniformly over the earth. They could
  power Mobile Devices Eg. cell phones

• Microwave transmission
  – Interference with other electronic devices
  – Health and environmental effects
Cont…
• Possible health hazards
  – Effects of long term exposure
  – Exposure is equal to the amount that
    people receive from cell phones and
    Microwaves

• Location
   – The size of construction for the rectennas
     is massive and also Implementation
     Complexity
Initial conceptual looks at a mega-engineering project as shown in this Boeing design.
 New technologies point to more efficient, less expensive space solar power systems.
                         Credit: Boeing/Space Studies Institute
Early and simple schematic of how a space solar power satellite would beam
  energy to electrical power grid on Earth. Credit: Space Studies Institute
Sustainable energy

• To meet the final goal of providing sustainable energy for
  future growth and protection of the environment, the
  design and technology for space solar power should be
  evaluated by the criteria of availability of resources,
  energy economy (payback time) and waste production
  such as carbon-dioxide through all the processes
  required for production of SPS . Power from space
  should be competitive with other energy sources in this
  respect. We also need a space solar future if our
  children are to live in an intact environment. They will be
  grateful to us
5. Proposed Project/Experiment
5. Proposed Project/Experiment
Goal of the Proposal


• Obtain $10,000 grant from EPA to fund
  our research
Proposed Project
• Transmit power from AC outlet to
  a remote circuit wirelessly
  – to demonstrate the capability of the
    technology,
  – to explore the problems we'll face in a small-
    scale experiment, and
  – to use this experiment as a “probe” to explore
    the potential problems of transmitting power
    from space to earth
Benefits
1) For graduate and undergraduate
   students to research and study about
   wireless power transmission

2) Demonstration tool for a potential
   laboratory course

3) Potential commercialization of the
   proposed project
Block Diagram of Proposed Experiment
                    —1
Transmitting
   Side:

                  AC Power      Power         Microwave
                  Outlet        Conversion    Transmitter



                                                 This
                              This converts   transmits
               This is the
                              the AC power        the
               AC power      to a microwave   microwave
                supply        power signal
                                                power
                                                signal
Block Diagram of Proposed Experiment
                  —2
Receiving
  Side:

       Rectenna       Power        Power        Remote
                      Conversion   Regulator    Device




                                                   Remote
                                      This       Device uses
         This converts the
                                    regulates      this DC
     microwave power signal to                    power the
                                   DC voltage
          DC power signal                        same way it
                                      level
                                                uses a battery
Vision on Future Development

     Local
     Local                  Regional
                            Regional                  Orbital
                                                      Orbital




                                                     Ability to transmit
                                                     Ability to transmit
                              Ability to transmit
                               Ability to transmit       power
                                                          power
Ability to transmit power
Ability to transmit power        power from a
                                  power from a           from a
                                                          from a
 within a laboratory
 within a laboratory              local power
                                   local power          geostationary
                                                         geostationary
                         plant to local households satellite to a specific
                          plant to local households satellite to a specific
                                                      reception site
                                                       reception site
6. Conclusion
6. Conclusion
Conclusion
• This idea worth to invest in since this
  technology brings in virtually unlimited
  power from the sun.

• This also benefits the intercontinental
  power providers.

• Absolutely environmentally friendly since it
  is emission-free.
Reference
1)   “A Few Things you occasionally wanted to know about wireless power
     transmission.” Potter, Seth.
     http://www.spacefuture.com/archive/a_few_things_you_occasionally_wanted_to_know_ab

2)   “Solar Power Satellites and Microwave Power Transmission”
     http://www.kentlaw.edu/classes/fbosselm/Spring2004/PowerPoints/Wireless%20Power%2

3)   www.on-orbit-
     servicing.com/pdf/OOS2004_presentations_pdf/OOSIssuesOverview_Oda.pdf

4)   www.kentlaw.edu/classes/fbosselm/Spring2004/ PowerPoints/Wireless%20Power
     %20Transmission%20-%20Soubel.ppt

5)   www.spacefuture.com/.../a_fresh_look_at_space_
     solar_power_new_architectures_concepts_and_technologies.shtml

6)   Lin, James C., “Space solar power stations, wireless power transmissions, and
     biological implications”, IEEE microwave magazine, March, 2002

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Group 5 Wireless Oower

  • 1. Wireless Power Transmission EE563-Graduate Seminar Fall 2004 Group 5 Alan Chun-yip Yeung Leanne Cheung Jeff Samandari Wehibe Belachew Tesfa Mael Jose A. Becerra
  • 2. Presentation Outline 1. Introduction //Background 1. Introduction Background 2. Theory of Wireless Power Trans. 2. Theory of Wireless Power Trans. 3. Major Research Projects 3. Major Research Projects 4. Comparison of Efficiency … 4. Comparison of Efficiency … 5. Proposed Project/Experiment 5. Proposed Project/Experiment 6. Conclusion 6. Conclusion
  • 3. 1. Introduction // Background 1. Introduction Background
  • 4. Outline • History/Background • Solar Power Satellite • Microwave Power Transmission • Conclusion Reference: http://www.kentlaw.edu/classes/fbosselm/Spring2004/Power Points/Wireless%20Power%20Transmission%20- %20Soubel.ppt
  • 5. Background, Nikola Tesla • 1856-1943 • Innovations: – Alternating current – Wireless power transmission experiments at Wardenclyffe
  • 6. Wardenclyffe • 1899 – Able to light lamps over 25 miles away without using wires – High frequency current, of a Tesla coil, could light lamps filled with gas (like neon)
  • 7. 1940’s to Present • World War II developed ability to convert energy to microwaves using a magnetron, no method for converting microwaves back to electricity • 1964 William C. Brown demonstrated a rectenna which could convert microwave power to electricity
  • 8. Solar Power from Satellites • 1968’s idea for Solar Power Satellites proposed by Peter Glaser – Would use microwaves to transmit power to Earth from Solar Powered Satellites • Idea gained momentum during the Oil Crises of 1970’s, but after prices stabilized idea was dropped – US Department of Energy research program 1978-1981
  • 9.
  • 10. Problems • Issues identified during the DOE study – Complexity—30 years to complete – Size—6.5 miles long by 3.3 miles wide • Transmitting antenna ½ mile in diameter(1 km) – Cost—$74 billion – Interference
  • 11. From the Satellite • Solar power from the satellite is sent to Earth using a microwave transmitter • Received at a “rectenna” located on Earth • Recent developments suggest that power could be sent to Earth using a laser
  • 12. Microwaves • Frequency 2.45 GHz microwave beam • Retro directive beam control capability • Power level is well below international safety standard
  • 13. Microwave vs. Laser Transmission • Microwave • Laser – More developed – Recently developed – High efficiency up to solid state lasers allow 85% efficient transfer of – Beams is far below the power lethal levels of – Range of 10% to 20% concentration even for efficiency within a few a prolonged exposure years – Cause interference – Conform to limits on with satellite eye and skin damage communication industry
  • 14. Rectenna “An antenna comprising a mesh of dipoles and diodes for absorbing microwave energy from a transmitter and converting it into electric power.” • Microwaves are received with about 85% efficiency • Around 5km across (3.1 miles) • 95% of the beam will fall on the rectenna
  • 15. 5,000 MW Receiving Station (Rectenna). This station is about a mile and a half long.
  • 16. 2. Theory of Wireless Power Trans. 2. Theory of Wireless Power Trans.
  • 17. Theory of Operation • Electromagnetic Radiation • Antenna basics • Phased-array antenna • Diffraction analogy • Energy distribution • Rectenna • Physical limitations & relationships
  • 18. Physics of Wireless Power Transmission • Forms of Electromagnetic radiation • Travel at same speed • F = frequency • C = velocity of light •http://imnh.isu.edu/digitalatlas/clima/atmosph/images/waves.jpg • L =wavelength
  • 19. Dipole Antenna • Transmission of power is simpler than TV & Radio • Transmitter: wire half a wavelength • Pushes electrons back and forth • Receiver: wire half a wavelength http://www.zorg.org/radio/dipole_antenna.shtml
  • 20. Antenna Radiation Pattern http://www.astromag.co.uk/portable/dipole.gif
  • 21. Phased-array antenna • The λs for microwaves are small  dipoles small • Beam focusing: phased- array antenna • Electronically steered by varying the timing or phase • Waves will merge together http://www.mcs.harris.com/oceannet/features/antenna.html
  • 23. Diffraction analogy • Light same properties • Laser beam shinning trough a narrow opening & spreads out or diffracts • Bright spot in the center w/fainter spots on the side http://planetquest.jpl.nasa.gov/technology/diffraction.html
  • 24. Diffraction & Microwaves • Waves reinforce at some points and they cancel out at other points (bright and fainter points) • In microwaves: is a scaled up version of diffraction
  • 26. Main lobe energy • Circular central max  Main lobe • 84% of energy • Sidelobes surround • No energy  minima
  • 27. Intensity 84% in main lobe
  • 28. Rectenna • Array of dipole antennas known as rectifying antenna or Rectenna • Diameter = Dr
  • 30. Physical Limitations • The receiving diameter Dr increases with transmitter receiver separation distance S. • Dr increases if transmitter diameter Dt decreases
  • 32. 2. Sample Calculations 2. Sample Calculations
  • 33. Calculations/Analysis • Frequency, f (Hz) • Intensity, I (watts per square meter) • Wave-Length, L (meters) • Received Main Beam Lope (“spot”) Diameter, Dr (meters or kilometers) • Transmitting Phased Array Diameter, Dt (meters or kilometers) • Example: how to estimate Intensity, I ?
  • 34. Frequency Formula Dt * Dr • Frequency, f (Hz) = -------------- (2) (L * S) Dt: transmitting phased array diameter Dr: received main beam lobe (“spot”) diameter L: wavelength S: separation
  • 35. Frequency Analysis Dt * Dr If (Frequency, f (Hz) = ----------- ) ≥ 2.44 GHz (2) (L * S) Then at least, 84% of the energy of the beam will be captured Note: • This energy is not linear; 42% of the energy is not equivalent to 1.22 GHz. • Equation (2) represent a best case scenario. • Practical antenna sizes may have to be larger if most of the beam is to be captured. • The rectenna will have to be at least as large as Dt, even if (2) says Dr is smaller.
  • 36. Frequency Analysis • Such a wide beam can be focused, but only to a minimum size Dr. • For low Earth-orbit power-beaming demonstrations, it is easier to put the smaller antenna in space and the larger antenna on Earth. • Early demonstrations may capture only a small percentage of the total power, in order to keep antenna sizes small. – to light up a 60 watt bulb, thousands of watts may have to be transmitted. – Since costly to launch such a power generating apparatus, the most feasible demonstration project may be Earth-to-space transmission from a large transmitting antenna (such as the Arecibo dish) to a smaller rectenna in space.
  • 37. Intensity, I Formula • Intensity, I (watts per square meter) P Dt = ½ ( Pi * -----) * ( --------- ) (3) 4 L*S Pi: 3.14… P: total power transmitted Dt: transmitted phased array diameter L: wave length S: transmitter to receiver distance (separation)
  • 38. Wave-Length, L Calculations • Wave-Length, L (meters) c 300,000,000 meter/sec = ----- = ( -------------------------------- ) = 0.1224 (1) f 2,450,000,000/sec meter c: speed of light f: frequency
  • 39. Received Main Beam Lope Diameter, Dr Calculations • Received Main Beam Lope (“spot”) Diameter, Dr (meters or kilometers) f*L*S 2.44 * 0.12224m * 35,800,000m = -------------- = -------------------------------------------- Dt 1000m = 10,700 meter = 10.7 kilometers L: wave length S: separation Dt: transmitting phased array diameter
  • 40. Transmitting Phased Array Diameter, Dt Calculations • Transmitting Phased Array Diameter, Dt (meters or kilometers) f*L*S 2.44 * 0.12224m * 35,800,000m = -------------- = ---------------------------------------------- Dr 10,700 meter = 1000m = 1 kilometers L: wave length S: separation Dr: received main beam lope (“spot”) diameter
  • 41. Example What is the Intensity, I = ? Given: f, Dr, and a typical solar power satellite transmitting 5 billion watts from geostationary orbit 35800 kilometers high. Solution: Use the following (1), (2), & (3) C f = -----  L (1) L Dt * Dr Frequency, f (Hz) = --------------  Dt (2) (L * S) P Dt Intensity, I (watts/m^²) = ½ ( Pi * -----) * ( --------- ) (3) 4 L*S
  • 42. Example Calculations • Intensity, I (watts per square meter) P Dt = ½ ( Pi * -----) * ( --------- ) (3) 4 L*S 2287485.869w 1000m = ½ ( Pi * ---------------------------) * ( ----------------------------------- ) 4m 0.1224m* 35800,000m = 205 watts/m^² or 20.5 milliwatts/cm^²
  • 43. Example Analysis • peak beam intensity, Ip = 20.5 milliwatts/cm^²  This is about twice US industrial standard for human exposure  This is converted (by rectenna) to electricity by 90% efficiency • Average intensity, Ia ≈ 1/3 * 20.5 milliwatts/cm^²
  • 44. Rectangular Transmitting antenna array Calculations • Mathematics slightly different, but the same general principles apply. • Central maximum of the beam contain 82% of the transmitted energy. • Rectangular in shape, but will spread out more along TX array’s short direction than its long direction. • Example: Canada’s Radar sat rectangular transmitting antenna: 1.5m × 15m “footprint” on the ground: 7,000m × 50,000m frequency: 5.3 GHz altitude: 800,000m output power: 5000 watts  The power is too spread out at the ground to use in a practical demonstration project.
  • 45. Two more points 1. Use certain transmitting methods – to reduce the level of the sidelobes – to put some of the sidelobe energy into the main lobe –  Price to pay: Larger Rectenna (because main lobe spreads out) 2. Principal of diffraction also limits the resolution of optical systems: – Lenses – Telescopes
  • 46. 3. Major Research Projects 3. Major Research Projects
  • 47. 1979 SPS Reference System concept (GEO)
  • 48.
  • 49. Accomplishments of Solar Power Satellites • 1980, 30 kW of microwave power was transmitted to a receiving antenna over one mile • 1993, Japan successfully transmitted a 800W microwave beam from a rocket to a free-flying satellite in space. • 1998, Microwave to DC conversion efficiency of 82% or higher by the rectenna.
  • 50. NASA’s 1995-1997 Fresh Look Study • MEO (Mid-Earth Orbit) Sun Tower: - 6 SPS yields near 24-hr power to sites - ± 30 degrees Latitude Coverage - Power services of 200- 400 MW
  • 51. Continued • Solar Disc - 1 SPS provides nearly 24- hr power to markets - Spin-stabilized solar array, de-spun phased array with electronic beam-steering - Geostationary Earth Orbit - ± 60 degrees Latitude Coverage - Power services of about 5 GW
  • 52. 1999-2000 Space Solar Power (SSP) Exploratory Research and Technology (SERT) program • Exploration and Commercial Development
  • 53.
  • 55. NASA’s SSP Strategic Research & Technology Roadmaps
  • 57. Details of SPS 2000 • Japan is to build a low cost demonstration of SPS by 2025. • Eight countries along the equator agreed to be the rectenna sites. • 10 MW satellite delivering microwave power in the low orbit 1100 km(683 miles) – Will not be in geosynchronous orbit, instead low orbit 1100 km (683 miles) – Much cheaper to put a satellite in low orbit
  • 58. Japan’s Recent Research Efforts • Japan - 2001, Japanese’s Ministry of Economy, Trade and Industry (METI) launched a research program for a solar-powered- generated satellite. - By 2040, beginning of a SPS operation. The planned satellite will be able to generate 1GW/Sec. (equivalent to the output of a nuclear plant) in a geostationary orbit. The receiving antenna (rectenna) on the ground will be either positioned at desert or sea.
  • 59. Japan’s Roadmaps for SPS Development
  • 60. References • www.on-orbit-servicing.com/pdf/OOS2004_ presentations_pdf/OOSIssuesOverview_Oda.pdf • www.kentlaw.edu/classes/fbosselm/Spring2004/ PowerPoints/Wireless %20Power%20Transmission%20-%20Soubel.ppt • www.spacefuture.com/.../a_fresh_look_at_space_ solar_power_new_architectures_concepts_and_technologies.shtml • Lin, James C., “Space solar power stations, wireless power transmissions, and biological implications”, IEEE microwave magazine, March, 2002
  • 61. 4. Comparisons Among Other Power 4. Comparisons Among Other Power Sources Sources
  • 62. Efficiency and Costs •Space Solar Power (Wireless Power Transmission) •Ground Based Solar Power •Nuclear Energy •Fossil Fuel
  • 63. Advantages over Earth-based solar power • More intense sunlight • In geosynchronous orbit, 36,000 km (22,369 miles) an SPS would be illuminated over 99% of the time • No need for costly storage devices for when the sun is not in view
  • 64. Cont. • Waste heat is radiated back into space • Power can be beamed to the location where it is needed, don’t have to invest in as large a grid • No air or water pollution is created during generation • Ground based solar only works during clear days, and must have storage for night. Thus it is More reliable than ground based solar power
  • 65. Advantages over Nuclear Power There are advantages… • Possible power generation of 5 to 10 gig watts • If the largest conceivable space power station were built and operated 24 hours a day all year round, it could produce the equivalent output of ten 1 million kilowatt-class nuclear power stations.
  • 66. Cont… • Nuclear power doesn't pollute the atmosphere like fossil fuels. But it does produce waste. This stays radioactive for thousands of years and is very dangerous. At the moment most stations bury their waste deep underground, at sea or send it to other countries. (Britain, for example, accepts and buries nuclear waste from several countries.)
  • 67. Cont… • One of the disadvantage of Nuclear • On April 26, 1986 the worst catastrophe in nuclear history occurred in the station at Chernobyl, Ukraine. • Due to the failure of one of reactor, two people died immediately from the explosion and 29 from radiation. About 200 others became seriously ill from the radiation; some of them later died. It was estimated that eight years after the accident 8,000 people had died from diseases due to radiation (about 7,000 of them from the Chernobyl cleanup crew). Doctors think that about 10,000 others will die from cancer. The most frightening fact is that children who were not born when the catastrophe occurred inherited diseases from their parents. • Source http://oii.org/html/story.html by Vessela Daskalova
  • 68. Advantages over Fossil Fuel • Fossil fuels won't last forever (next 50yrs) • It is not renewable • The ability to match supply to demand may already have run out, especially for oil • Fossil Fuel fired electric power plants in the US emits about 2 billion tons of greenhouse gas CO2 in to air every year. This courses climate change in the future via greenhouse effect.
  • 69. Cost • Cost—prototype would have cost $74 billion • “According to Kyle Datta the Oil Factor,” which predicts that oil could hit $100 a barrel by 2010.
  • 70. Disadvantages • If microwave beams carrying power could be beamed uniformly over the earth. They could power Mobile Devices Eg. cell phones • Microwave transmission – Interference with other electronic devices – Health and environmental effects
  • 71. Cont… • Possible health hazards – Effects of long term exposure – Exposure is equal to the amount that people receive from cell phones and Microwaves • Location – The size of construction for the rectennas is massive and also Implementation Complexity
  • 72. Initial conceptual looks at a mega-engineering project as shown in this Boeing design. New technologies point to more efficient, less expensive space solar power systems. Credit: Boeing/Space Studies Institute
  • 73. Early and simple schematic of how a space solar power satellite would beam energy to electrical power grid on Earth. Credit: Space Studies Institute
  • 74. Sustainable energy • To meet the final goal of providing sustainable energy for future growth and protection of the environment, the design and technology for space solar power should be evaluated by the criteria of availability of resources, energy economy (payback time) and waste production such as carbon-dioxide through all the processes required for production of SPS . Power from space should be competitive with other energy sources in this respect. We also need a space solar future if our children are to live in an intact environment. They will be grateful to us
  • 75. 5. Proposed Project/Experiment 5. Proposed Project/Experiment
  • 76. Goal of the Proposal • Obtain $10,000 grant from EPA to fund our research
  • 77. Proposed Project • Transmit power from AC outlet to a remote circuit wirelessly – to demonstrate the capability of the technology, – to explore the problems we'll face in a small- scale experiment, and – to use this experiment as a “probe” to explore the potential problems of transmitting power from space to earth
  • 78. Benefits 1) For graduate and undergraduate students to research and study about wireless power transmission 2) Demonstration tool for a potential laboratory course 3) Potential commercialization of the proposed project
  • 79. Block Diagram of Proposed Experiment —1 Transmitting Side: AC Power Power Microwave Outlet Conversion Transmitter This This converts transmits This is the the AC power the AC power to a microwave microwave supply power signal power signal
  • 80. Block Diagram of Proposed Experiment —2 Receiving Side: Rectenna Power Power Remote Conversion Regulator Device Remote This Device uses This converts the regulates this DC microwave power signal to power the DC voltage DC power signal same way it level uses a battery
  • 81. Vision on Future Development Local Local Regional Regional Orbital Orbital Ability to transmit Ability to transmit Ability to transmit Ability to transmit power power Ability to transmit power Ability to transmit power power from a power from a from a from a within a laboratory within a laboratory local power local power geostationary geostationary plant to local households satellite to a specific plant to local households satellite to a specific reception site reception site
  • 83. Conclusion • This idea worth to invest in since this technology brings in virtually unlimited power from the sun. • This also benefits the intercontinental power providers. • Absolutely environmentally friendly since it is emission-free.
  • 84. Reference 1) “A Few Things you occasionally wanted to know about wireless power transmission.” Potter, Seth. http://www.spacefuture.com/archive/a_few_things_you_occasionally_wanted_to_know_ab 2) “Solar Power Satellites and Microwave Power Transmission” http://www.kentlaw.edu/classes/fbosselm/Spring2004/PowerPoints/Wireless%20Power%2 3) www.on-orbit- servicing.com/pdf/OOS2004_presentations_pdf/OOSIssuesOverview_Oda.pdf 4) www.kentlaw.edu/classes/fbosselm/Spring2004/ PowerPoints/Wireless%20Power %20Transmission%20-%20Soubel.ppt 5) www.spacefuture.com/.../a_fresh_look_at_space_ solar_power_new_architectures_concepts_and_technologies.shtml 6) Lin, James C., “Space solar power stations, wireless power transmissions, and biological implications”, IEEE microwave magazine, March, 2002

Editor's Notes

  1. Image: www.mercury.gr/tesla/ lifeen.html MSN Encarta, Nikola Tesla,< http://encarta.msn.com/encyclopedia_761567992_1____3/Tesla_Nikola.html#s3>(accessed April 10, 2004)
  2. Image: www.tfcbooks.com/images/teslafaq/ wardenclyffe.gif MSN Encarta, Nikola Tesla,< http://encarta.msn.com/encyclopedia_761567992_1____3/Tesla_Nikola.html#s3>(accessed April 10, 2004)
  3. Wikipedia, Microwave Power Transmission,< http://www.fact-index.com/m/mi/microwave_power_transmission.html>(accessed April 10, 2004)
  4. David, Leonard, Bright Future for Solar Power Satellites, < http://www.space.com/businesstechnology/technology/solar_power_sats_011017-1.html>(accessed April 10, 2004) Space Power, SPS Timeline,< http://www.spacefuture.com/power/timeline.shtml>(accessed April 10, 2004)
  5. http://www.ssi.org/assets/images/SPS_summary.jpg
  6. David, Leonard, Bright Future for Solar Power Satellites, < http://www.space.com/businesstechnology/technology/solar_power_sats_011017-1.html>(accessed April 10, 2004) Space Power, SPS Timeline,< http://www.spacefuture.com/power/timeline.shtml>(accessed April 10, 2004) US Department of Energy, EREC Brief Solar Power Satellites,< http://www.eere.energy.gov/consumerinfo/refbriefs/l123.html>(accessed April 10, 2004)
  7. ISIS, Highlights in Space 2000, < http://www.oosa.unvienna.org/isis/highlights2000/sect6b.html>(accessed April 10, 2004)
  8. Nagatomo, Makoto, Conceptual Study of a Solar Power Satellite, SPS 200, < http://www.spacefuture.com/pr/archive/conceptual_study_of_a_solar_power_satellite_sps_2000.shtml>(accessed April 10, 2004)
  9. ISIS, Highlights in Space: 2000, < http://www.oosa.unvienna.org/isis/highlights2000/sect6b.html> (accessed April 10, 2004) Wikipedia, Solar Power Satellite, < http://www.fact-index.com/s/so/solar_power_satellite.html>(accessed April 10, 2004)
  10. Quote: http://www.spacetalent.com/cgi/glossary.cgi?gl=term&term=Rectenna Wikipedia, Solar Power Satellite, < http://www.fact-index.com/s/so/solar_power_satellite.html>(accessed April 10, 2004)
  11. www. powersat .com/ image_library.html