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LITERATURE REVIEW
 Fikret Caliskan , Chingiz Hajiyev
The paper aims at the detection and identification of airframe
icing using statistical properties of aircraft dynamics and
reconfigurable control protecting aircraft from hazardous icing
conditions.
 Guo fan , Chang shinan
This paper describes the principle of electro-impulse de-icing
(EIDI) system of an aircraft which use electromagnetic force to
remove ice.
 Mark G. Potapczuk
The research paper covering the icing environment,
investigations into the physics of ice accretion on aircraft
surfaces,engine performance, icing instrumentation
development etc.
INTRODUCTION
 In aviation, aircraft icing are those atmospheric
conditions that can lead to the formation of
water ice on the surfaces of an aircraft.
EFFECTS OF ICING
ACCIDENTS
 Aircraft icing is one of the major weather
hazards to aviation and has resulted in several
fatal accidents.
CAUSES OF ICING
1. Liquid Water
Content
(LWC)
 Amount of available
water
 Varies from cloud to
cloud
 Varies within same cloud
2. Temperature
Most icing tends to occur
at temperatures
between 0°and -20°C
More than 50% of those
occur between -8 and -
12°C
CAUSES OF ICING
CAUSES OF ICING
3. Water Droplet Size
Icing patterns change with
droplet size.
In relation to icing hazards
–Droplet size not as important
as
LWC and Temperature
TYPES OF STRUCTURAL ICE
ICE DETECTION
ICE DETECTION
1. Lucas ice detection
system
ICE DETECTION
 Vibro Meter
ICING PREVENTION AND
REMOVAL
 Pneumatic deicing boots
 Thermal
 Electrical heating elements
 ThermaWing
 Turbine engine bleed air
 Electro-mechanical
 Weeping Wing
 Electro-Mechanical Expulsion Deicing System (EMEDS)
 Hybrid Electro-Mechanical Expulsion Deicing System
 Passive (cover system mainly used in the telecoms and
offshore domains)
 Anti icing cover
ICING PREVENTION AND
REMOVAL
 Pneumatic deicing boots
Rubber boot
ICING PREVENTION AND
REMOVAL
 Electro- Impulse De-icing System
ICING PREVENTION AND
REMOVAL
 Controlling Leading Edge Temperature by
bleed air
ICING PREVENTION AND
REMOVAL
 Weeping Wing
ICING PREVENTION AND
REMOVAL
 De-icing
fluids
ICING PREVENTION AND
REMOVAL
CONCLUSION
 Ice has a greater impact on aircrafts
performance & may causes severe accidents.
 The recent improvements results in safe flight
even in severe weather conditions.
 various technologies are in development .
REFERENCES
 Fikret Caliskan , Chingiz Hajiyev , “A review of in-flight detection
and identification of aircraft icing and reconfigurable control”,
Progress in Aerospace Sciences. 2013.
 Yiqun Dong, Jianliang Ai ,“Research on inflight parameter
identification and icing location detection of the aircraft”, Aerospace
Science and Technology.2012.
 Mark G. Potapczuk, “Aircraft Icing Research at NASA Glenn
Research Center”, journal of aerospace engineering. 2013.
 Giuseppe Mingione , Massimo Barocco, “FLIGHT IN ICING
CONDITIONS SUMMARY”
THANK YOU

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Analysis of aircraft icing and its preventive measures

  • 1.
  • 2. LITERATURE REVIEW  Fikret Caliskan , Chingiz Hajiyev The paper aims at the detection and identification of airframe icing using statistical properties of aircraft dynamics and reconfigurable control protecting aircraft from hazardous icing conditions.  Guo fan , Chang shinan This paper describes the principle of electro-impulse de-icing (EIDI) system of an aircraft which use electromagnetic force to remove ice.  Mark G. Potapczuk The research paper covering the icing environment, investigations into the physics of ice accretion on aircraft surfaces,engine performance, icing instrumentation development etc.
  • 3. INTRODUCTION  In aviation, aircraft icing are those atmospheric conditions that can lead to the formation of water ice on the surfaces of an aircraft.
  • 5. ACCIDENTS  Aircraft icing is one of the major weather hazards to aviation and has resulted in several fatal accidents.
  • 6. CAUSES OF ICING 1. Liquid Water Content (LWC)  Amount of available water  Varies from cloud to cloud  Varies within same cloud
  • 7. 2. Temperature Most icing tends to occur at temperatures between 0°and -20°C More than 50% of those occur between -8 and - 12°C CAUSES OF ICING
  • 8. CAUSES OF ICING 3. Water Droplet Size Icing patterns change with droplet size. In relation to icing hazards –Droplet size not as important as LWC and Temperature
  • 11. ICE DETECTION 1. Lucas ice detection system
  • 13. ICING PREVENTION AND REMOVAL  Pneumatic deicing boots  Thermal  Electrical heating elements  ThermaWing  Turbine engine bleed air  Electro-mechanical  Weeping Wing  Electro-Mechanical Expulsion Deicing System (EMEDS)  Hybrid Electro-Mechanical Expulsion Deicing System  Passive (cover system mainly used in the telecoms and offshore domains)  Anti icing cover
  • 14. ICING PREVENTION AND REMOVAL  Pneumatic deicing boots Rubber boot
  • 15. ICING PREVENTION AND REMOVAL  Electro- Impulse De-icing System
  • 16. ICING PREVENTION AND REMOVAL  Controlling Leading Edge Temperature by bleed air
  • 20. CONCLUSION  Ice has a greater impact on aircrafts performance & may causes severe accidents.  The recent improvements results in safe flight even in severe weather conditions.  various technologies are in development .
  • 21. REFERENCES  Fikret Caliskan , Chingiz Hajiyev , “A review of in-flight detection and identification of aircraft icing and reconfigurable control”, Progress in Aerospace Sciences. 2013.  Yiqun Dong, Jianliang Ai ,“Research on inflight parameter identification and icing location detection of the aircraft”, Aerospace Science and Technology.2012.  Mark G. Potapczuk, “Aircraft Icing Research at NASA Glenn Research Center”, journal of aerospace engineering. 2013.  Giuseppe Mingione , Massimo Barocco, “FLIGHT IN ICING CONDITIONS SUMMARY”