Helikopter Sistemleri - Bölüm 4 - helikopter sistemleri. FAA Helicopter Flying Handbook'tan referans alınarak hazırlandı. İstanbul Arel Üniversitesi - Emre Akar
Helikopter Sistemleri - Bölüm 2 - Uçuş Aerodinamiği. FAA Helicopter Flying Handbook indeksi referans alınarak hazırlandı. İstanbul Arel Üniversitesi - Emre Akar
Helikopter Sistemleri - Bölüm 3 - Uçuş Kumandaları. FAA Helicopter Flying Handbook indeksi referans alınarak hazırlandı. İstanbul Arel Üniversitesi - Emre Akar
This document provides an introduction to helicopter flight dynamics, including:
- Definitions of helicopter flight dynamics, characteristics of helicopter flight, and scopes and methodologies used.
- Coordinate systems used including gravity, body, wind, and hub axes.
- Transformations between different coordinate systems.
- Angles used to describe helicopter orientation and motion, including Euler angles.
- Prerequisites, syllabus, and references for further study are also included.
The document summarizes helicopter flight controllers, including the external forces acting on helicopters, different control manners, and the development of helicopter controllers. It describes the aerodynamic forces on the main rotor, tail rotor, fuselage, horizontal and vertical tails. It then explains the control manners of helicopters with main and tail rotors, twin rotor helicopters, and tilt-rotor aircraft. Finally, it discusses early direct control methods and the progression to modern fly-by-wire and fly-by-light control systems.
This document outlines the course details and topics for a 18-week rotorcraft systems, maintenance, and role equipment class at the Malaysian Institute of Aviation Technology. The course will cover 10 topics related to helicopter structure and maintenance, and will evaluate students based on assignments, quizzes, and a final exam. Students who miss more than 10% of classes will be barred from the final exam. The document then provides details on helicopter structural design, including tubular, stressed skin, and bonded construction methods, as well as the stresses and loads placed on helicopter structures.
This document summarizes a presentation given by the FAASTeam to pilots and instructors on stall and spin awareness and avoidance. The presentation covers topics like normal and crosswind takeoffs, slow flight, steep turns, stalls, landings, and go-arounds. It discusses common errors during these maneuvers, such as improper pitch control, failure to maintain a stabilized approach, and inadequate compensation for wind. The goal is to help pilots identify strengths and weaknesses and reduce the risk of accidents during takeoff, landing, and low-altitude maneuvering. Quizzes are included to reinforce key concepts.
The document discusses the Boeing AH-64 Apache helicopter. It has a top speed of 293 km/h, is 18m long, and weighs 5,165 kg. It is powered by turboshaft engines and has a variety of weapons systems including a 30mm chain gun, Hellfire missiles, Hydra rockets, and air-to-air Stinger missiles. The Apache relies on advanced sensor and radar systems to detect targets and navigate using infrared and radar technology. Its armor system helps protect it from enemy fire through stealth materials and reinforced armor plating.
Helikopter Sistemleri - Bölüm 2 - Uçuş Aerodinamiği. FAA Helicopter Flying Handbook indeksi referans alınarak hazırlandı. İstanbul Arel Üniversitesi - Emre Akar
Helikopter Sistemleri - Bölüm 3 - Uçuş Kumandaları. FAA Helicopter Flying Handbook indeksi referans alınarak hazırlandı. İstanbul Arel Üniversitesi - Emre Akar
This document provides an introduction to helicopter flight dynamics, including:
- Definitions of helicopter flight dynamics, characteristics of helicopter flight, and scopes and methodologies used.
- Coordinate systems used including gravity, body, wind, and hub axes.
- Transformations between different coordinate systems.
- Angles used to describe helicopter orientation and motion, including Euler angles.
- Prerequisites, syllabus, and references for further study are also included.
The document summarizes helicopter flight controllers, including the external forces acting on helicopters, different control manners, and the development of helicopter controllers. It describes the aerodynamic forces on the main rotor, tail rotor, fuselage, horizontal and vertical tails. It then explains the control manners of helicopters with main and tail rotors, twin rotor helicopters, and tilt-rotor aircraft. Finally, it discusses early direct control methods and the progression to modern fly-by-wire and fly-by-light control systems.
This document outlines the course details and topics for a 18-week rotorcraft systems, maintenance, and role equipment class at the Malaysian Institute of Aviation Technology. The course will cover 10 topics related to helicopter structure and maintenance, and will evaluate students based on assignments, quizzes, and a final exam. Students who miss more than 10% of classes will be barred from the final exam. The document then provides details on helicopter structural design, including tubular, stressed skin, and bonded construction methods, as well as the stresses and loads placed on helicopter structures.
This document summarizes a presentation given by the FAASTeam to pilots and instructors on stall and spin awareness and avoidance. The presentation covers topics like normal and crosswind takeoffs, slow flight, steep turns, stalls, landings, and go-arounds. It discusses common errors during these maneuvers, such as improper pitch control, failure to maintain a stabilized approach, and inadequate compensation for wind. The goal is to help pilots identify strengths and weaknesses and reduce the risk of accidents during takeoff, landing, and low-altitude maneuvering. Quizzes are included to reinforce key concepts.
The document discusses the Boeing AH-64 Apache helicopter. It has a top speed of 293 km/h, is 18m long, and weighs 5,165 kg. It is powered by turboshaft engines and has a variety of weapons systems including a 30mm chain gun, Hellfire missiles, Hydra rockets, and air-to-air Stinger missiles. The Apache relies on advanced sensor and radar systems to detect targets and navigate using infrared and radar technology. Its armor system helps protect it from enemy fire through stealth materials and reinforced armor plating.
This is Part 4 (in work) of work for my Advanced Technology Demonstration Aircraft project, to inspire interest in aerospace engineering for the RAeS and AIAA.
Mechanics and types of wings of air planesDave Madhav
Wings are the main lifting surfaces of airplanes. There are various wing types and designs:
- Straight wings extend perpendicular to the fuselage and are found on low-speed planes. Swept-back wings extend backward at an angle and are used on jet planes for efficiency. Delta wings have a triangular shape that provides aerodynamic benefits. Forward-swept wings angle toward the front and have a small wing called a canard. Variable-sweep wings can change their sweep during flight. Flying wings have virtually no fuselage and the entire aircraft is the wing.
This document discusses how planes fly through aerodynamic forces. It explains that thrust produced by engines propels the plane forward, while lift forces generated by the wings when air passes over and under them allow the plane to gain altitude and remain airborne. The document also covers the different axes of motion for a plane and how control surfaces like elevators, rudders, and ailerons allow pilots to control pitching, yawing, and rolling movements. Finally, it provides specifications for the Airbus A380 and Dassault Rafale to illustrate different types of modern aircraft.
The document discusses aircraft landing gear, including:
1) The main functions of landing gear such as supporting the aircraft's weight and absorbing landing shocks.
2) The basic types of landing gear including fixed, retractable, and types based on arrangement like single, double, and tandem.
3) Key components of landing gear like shock struts, torque links, and the various actuators, links, and mechanisms involved.
This document contains 46 multiple choice questions about propeller construction and operation. It covers topics like propeller blade design and construction materials, forces acting on propeller blades like centrifugal twisting moment, blade angle adjustments, and the purpose of features like propeller twist and feathering. The questions are multiple choice with explanations provided for the correct answers referring to sources like the Jeppesen textbook on aircraft propellers and controls.
The document discusses inspections required on certificated aircraft according to FAR regulations. It covers the following key points:
- Owners are responsible for maintaining airworthiness and complying with inspections and airworthiness directives.
- Inspections required include annual inspections, 100-hour inspections, and inspections selected from FAA-approved programs depending on the aircraft type and operation.
- Additional inspections include altimeter and static system inspections every 24 months and transponder inspections every 24 months if the aircraft is equipped with a transponder.
The document summarizes the evolution of aircraft structures from early designs using wooden ribs and fabric to modern aluminum and composite designs. It describes key structural components such as those that produce lift (wings, airfoils), control (elevators, ailerons, rudders), modify lift (flaps, slats), and hold other components. Early aircraft had open wooden frameworks and fabric coverings while later warplanes used metal tubing and stressed skin construction. Modern jets widely use semi-monocoque construction.
This document provides training material on helicopter structures for the Malaysian Institute of Aviation Technology. It discusses the firewall and landing gear systems. The firewall functions to contain fires and protect the airframe and pipelines. Modern firewalls are made of titanium or composite honeycomb materials. Skid type landing gear is simpler but restricts aircraft movement compared to wheel type gear used on larger helicopters. The document describes constructing, installing, and maintaining firewalls and skid landing gear.
Structural detailing of fuselage of aeroplane /aircraft.PriyankaKg4
This presentation is about the structural detailing of fuselage of aeroplane .The fuselage or body of the airplane, holds all the pieces together. The pilots sit in the cockpit at the front of the fuselage. Passengers and cargo are carried in the rear of the fuselage. Some aircraft carry fuel in the fuselage; others carry the fuel in the wings.
An airfoil is any surface such as a wing, propeller, or helicopter blade that generates lift when air flows over it. The airfoil is designed so that the airflow speeds up over the top surface, which decreases the air pressure and increases lift. The leading edge is the front part that air first meets, and the trailing edge is the back where the top and bottom airflow meet again. Spars, ribs, and stringers make up the basic wing framework, providing structure and shape. Early wings were wood but now aluminum and lightweight composite materials are most common.
This document summarizes an FAA presentation on aircraft modifications. It discusses the regulations regarding modifications, including parts 21, 43, 91, and 135. It explains that for an aircraft to be considered airworthy, it must conform to its type design and be in a condition for safe operation. The presentation also discusses major vs minor alterations, field approvals, instructions for continued airworthiness, and other key topics relating to modifying aircraft.
This document discusses aircraft flight control systems. It describes the primary, secondary, and auxiliary flight controls, including the elevator, aileron, and rudder control systems, as well as secondary controls like trim tabs and auxiliary controls like flaps. It also provides details on how the autopilot system works, noting that it uses sensors, a gyroscope, and actuators to automatically control the aircraft without pilot input. The autopilot takes over complete control of the aircraft from take-off to landing.
This document provides an overview of aircraft basics including:
- The main components of an aircraft including wings, empennage, landing gear, and power plants. Wings can be high-wing, mid-wing, or low-wing and include ailerons and flaps. The empennage includes vertical and horizontal stabilizers with rudders and elevators.
- The four main forces acting on an aircraft during flight: lift, thrust, weight, and drag. Bernoulli's equation is presented relating to lift.
- Primary flight controls including ailerons, elevators, rudders, and various tail configurations. Pitch, yaw, and V-tail are also explained.
- Secondary flight controls
Aircraft Maintenance Manuals for Engineer's by Engr. Malay Kanti BalaMalay Kanti Bala
Aircraft Maintenance Manual is an important document for the Aircraft Maintenance Personnel. For the airworthiness of any flight, we do an inspection, servicing, repair, removal, installation, etc activities by following the approved documents which in manual or AMM. Here the presentation will disclose and familiarise with different manuals
This document provides an overview of aircraft wings, including their:
- Historical development from ancient kites to the Wright brothers' fixed-wing aircraft.
- Construction, with internal structures like ribs, spars, stringers, and skin covering the framework. Wings also contain fuel tanks, flaps, and other devices.
- Functions, as wings generate lift through Bernoulli's principle and critical angle of attack. Wing design factors like aspect ratio and camber also affect lift.
- Types based on position (fixed or movable) and structure (cantilever or strut-braced). Stability devices like ailerons and flaps are also described.
- Unconventional designs that
This document discusses airfoil and rotor blade terminology. It defines symmetrical and nonsymmetrical airfoils and their characteristics. It also defines the angles of incidence, attack, and describes how collective and cyclic feathering changes these angles to control the helicopter. Flapping, lead, and lag are also summarized as important motions of the rotor blades that help control the aircraft.
The document discusses the UH-1H helicopter flight control system. It appears to be a presentation about the topic given by Abdullah ÇELIK, who has an M.Sc. in Mechanical Engineering. The presentation provides a high-level overview of the UH-1H helicopter flight control system and thanks the audience for their attention.
The document discusses the flight control system of a UH-1H helicopter. It contains a diagram showing the collective lever, cyclic lever, and pedals used to control the helicopter during flight. The document concludes by thanking the audience for their attention.
This is Part 4 (in work) of work for my Advanced Technology Demonstration Aircraft project, to inspire interest in aerospace engineering for the RAeS and AIAA.
Mechanics and types of wings of air planesDave Madhav
Wings are the main lifting surfaces of airplanes. There are various wing types and designs:
- Straight wings extend perpendicular to the fuselage and are found on low-speed planes. Swept-back wings extend backward at an angle and are used on jet planes for efficiency. Delta wings have a triangular shape that provides aerodynamic benefits. Forward-swept wings angle toward the front and have a small wing called a canard. Variable-sweep wings can change their sweep during flight. Flying wings have virtually no fuselage and the entire aircraft is the wing.
This document discusses how planes fly through aerodynamic forces. It explains that thrust produced by engines propels the plane forward, while lift forces generated by the wings when air passes over and under them allow the plane to gain altitude and remain airborne. The document also covers the different axes of motion for a plane and how control surfaces like elevators, rudders, and ailerons allow pilots to control pitching, yawing, and rolling movements. Finally, it provides specifications for the Airbus A380 and Dassault Rafale to illustrate different types of modern aircraft.
The document discusses aircraft landing gear, including:
1) The main functions of landing gear such as supporting the aircraft's weight and absorbing landing shocks.
2) The basic types of landing gear including fixed, retractable, and types based on arrangement like single, double, and tandem.
3) Key components of landing gear like shock struts, torque links, and the various actuators, links, and mechanisms involved.
This document contains 46 multiple choice questions about propeller construction and operation. It covers topics like propeller blade design and construction materials, forces acting on propeller blades like centrifugal twisting moment, blade angle adjustments, and the purpose of features like propeller twist and feathering. The questions are multiple choice with explanations provided for the correct answers referring to sources like the Jeppesen textbook on aircraft propellers and controls.
The document discusses inspections required on certificated aircraft according to FAR regulations. It covers the following key points:
- Owners are responsible for maintaining airworthiness and complying with inspections and airworthiness directives.
- Inspections required include annual inspections, 100-hour inspections, and inspections selected from FAA-approved programs depending on the aircraft type and operation.
- Additional inspections include altimeter and static system inspections every 24 months and transponder inspections every 24 months if the aircraft is equipped with a transponder.
The document summarizes the evolution of aircraft structures from early designs using wooden ribs and fabric to modern aluminum and composite designs. It describes key structural components such as those that produce lift (wings, airfoils), control (elevators, ailerons, rudders), modify lift (flaps, slats), and hold other components. Early aircraft had open wooden frameworks and fabric coverings while later warplanes used metal tubing and stressed skin construction. Modern jets widely use semi-monocoque construction.
This document provides training material on helicopter structures for the Malaysian Institute of Aviation Technology. It discusses the firewall and landing gear systems. The firewall functions to contain fires and protect the airframe and pipelines. Modern firewalls are made of titanium or composite honeycomb materials. Skid type landing gear is simpler but restricts aircraft movement compared to wheel type gear used on larger helicopters. The document describes constructing, installing, and maintaining firewalls and skid landing gear.
Structural detailing of fuselage of aeroplane /aircraft.PriyankaKg4
This presentation is about the structural detailing of fuselage of aeroplane .The fuselage or body of the airplane, holds all the pieces together. The pilots sit in the cockpit at the front of the fuselage. Passengers and cargo are carried in the rear of the fuselage. Some aircraft carry fuel in the fuselage; others carry the fuel in the wings.
An airfoil is any surface such as a wing, propeller, or helicopter blade that generates lift when air flows over it. The airfoil is designed so that the airflow speeds up over the top surface, which decreases the air pressure and increases lift. The leading edge is the front part that air first meets, and the trailing edge is the back where the top and bottom airflow meet again. Spars, ribs, and stringers make up the basic wing framework, providing structure and shape. Early wings were wood but now aluminum and lightweight composite materials are most common.
This document summarizes an FAA presentation on aircraft modifications. It discusses the regulations regarding modifications, including parts 21, 43, 91, and 135. It explains that for an aircraft to be considered airworthy, it must conform to its type design and be in a condition for safe operation. The presentation also discusses major vs minor alterations, field approvals, instructions for continued airworthiness, and other key topics relating to modifying aircraft.
This document discusses aircraft flight control systems. It describes the primary, secondary, and auxiliary flight controls, including the elevator, aileron, and rudder control systems, as well as secondary controls like trim tabs and auxiliary controls like flaps. It also provides details on how the autopilot system works, noting that it uses sensors, a gyroscope, and actuators to automatically control the aircraft without pilot input. The autopilot takes over complete control of the aircraft from take-off to landing.
This document provides an overview of aircraft basics including:
- The main components of an aircraft including wings, empennage, landing gear, and power plants. Wings can be high-wing, mid-wing, or low-wing and include ailerons and flaps. The empennage includes vertical and horizontal stabilizers with rudders and elevators.
- The four main forces acting on an aircraft during flight: lift, thrust, weight, and drag. Bernoulli's equation is presented relating to lift.
- Primary flight controls including ailerons, elevators, rudders, and various tail configurations. Pitch, yaw, and V-tail are also explained.
- Secondary flight controls
Aircraft Maintenance Manuals for Engineer's by Engr. Malay Kanti BalaMalay Kanti Bala
Aircraft Maintenance Manual is an important document for the Aircraft Maintenance Personnel. For the airworthiness of any flight, we do an inspection, servicing, repair, removal, installation, etc activities by following the approved documents which in manual or AMM. Here the presentation will disclose and familiarise with different manuals
This document provides an overview of aircraft wings, including their:
- Historical development from ancient kites to the Wright brothers' fixed-wing aircraft.
- Construction, with internal structures like ribs, spars, stringers, and skin covering the framework. Wings also contain fuel tanks, flaps, and other devices.
- Functions, as wings generate lift through Bernoulli's principle and critical angle of attack. Wing design factors like aspect ratio and camber also affect lift.
- Types based on position (fixed or movable) and structure (cantilever or strut-braced). Stability devices like ailerons and flaps are also described.
- Unconventional designs that
This document discusses airfoil and rotor blade terminology. It defines symmetrical and nonsymmetrical airfoils and their characteristics. It also defines the angles of incidence, attack, and describes how collective and cyclic feathering changes these angles to control the helicopter. Flapping, lead, and lag are also summarized as important motions of the rotor blades that help control the aircraft.
The document discusses the UH-1H helicopter flight control system. It appears to be a presentation about the topic given by Abdullah ÇELIK, who has an M.Sc. in Mechanical Engineering. The presentation provides a high-level overview of the UH-1H helicopter flight control system and thanks the audience for their attention.
The document discusses the flight control system of a UH-1H helicopter. It contains a diagram showing the collective lever, cyclic lever, and pedals used to control the helicopter during flight. The document concludes by thanking the audience for their attention.
This document provides an overview of how to use an E6-B flight computer or "whiz wheel" to solve common flight calculations. It begins with conversions between units like gallons to pounds, nautical to statute miles, and Celsius to Fahrenheit. It then covers time, speed, distance and fuel problems. Next, it discusses calculating density altitude and true airspeed given altitude and temperature. Finally, it addresses wind calculations including finding groundspeed and wind correction angle. The overall aim is to teach pilots how to perform essential flight calculations and navigate safely using the E6-B slide rule.
The document discusses the major flight controls of a helicopter - collective pitch control, cyclic pitch control, and antitorque pedals. The collective pitch control adjusts the pitch of all main rotor blades simultaneously to control altitude. The cyclic pitch control tilts the main rotor disk to control horizontal movement. The antitorque pedals control the pitch of the tail rotor blades to counteract torque from the main rotor. Throttle or a governor system maintains a constant main rotor RPM as collective pitch is adjusted.
A helicopter has horizontal rotors that generate lift to propel the aircraft vertically. The main rotor provides lift and is mounted horizontally, while the tail rotor counters torque and is mounted vertically or near-vertically. There are different rotor system types including single, tandem, and intermeshing rotors. The main rotor system consists of blades attached to a hub on a mast. Flight is controlled through cyclic, collective, antitorque pedals, and throttle inputs which vary blade pitch collectively or individually to control lift, thrust, yaw, and power.
Helicopters are aircraft that use rotary wings to fly and hover. The document discusses helicopters and their use of chaff and flare countermeasures to avoid detection. It was written by Abdullah ÇELİK, a mechanical engineer, and thanks the reader for their attention on the topic of helicopters.
ATMS Helicopter Training Management Systeminsidersatms
ATMS (Advanced Training Management System) designed for commercial and military helicopter services and manufacturing companies. ATMS is used to manage the currency and training requirements for the helicopter maintenance, non-flying instructor, pilot, supply, support services, and technical crew member groups. Specifically, ATMS is used to build helicopter aircrew and maintenance training curriculums, track and manage qualifications, and streamline their training processes for their helicopter aircrew to ensure increased safety and compliance. MyATMS provides helicopter flight instructors and trainees with immediate access to training schedules, qualifications, launching e-learning content and provide reporting and analysis capabilities.
Hydroswing® Helicopter Hangar Facility Door Systems/Hydraulic DoorsMarshal Parker
The document discusses Hydroswing, a company that manufactures hydraulic single panel door systems for helicopter hangars. Their doors can be up to 145 feet wide and 45 feet tall, come in various styles, and are suitable for residential, commercial, and military helicopter facilities. The document provides contact information for Hydroswing locations around the world.
The document discusses the history and development of helicopters. It notes that the first helicopter was created in 1784 by two French inventors, Bienvenue and Launoy. The first helicopter to carry humans was developed by Paul Cornu in 1907. The helicopter design was further advanced in the 1920s by Juan de la Cieva, who is credited with coining the term "helicopter" that is still used today. The American government then ordered large numbers of helicopters in the late 1930s, building on Igor Sikorsky's design from 1939. Helicopters saw increasing development and usage during and after World War 2. They are now used for various purposes including in disaster relief situations like earthquakes and
The document is a presentation on flight data monitoring (FDM) given by Captain Mike Pilgrim to the IHST Accident Intervention Workshop on March 4th, 2013 in Las Vegas. It discusses the definition and purpose of FDM in improving helicopter safety by proactively identifying and addressing risks through analysis of digital flight data. It provides examples of how FDM can detect unsafe trends and incidents like overtorques on takeoff and potential for dynamic roll-overs.
The document discusses rotor flapping motion in helicopters. It covers three key topics:
1) The equation of rotor flapping motion and three origins of flapping motion: forward speed, controls, and angular velocity.
2) Factors that affect flapping motion, including hinge offset, hub moments, and whether the rotor is hinged or hingeless.
3) How the pilot controls the helicopter through inducing flapping motion by changing blade pitch via the controls.
The document discusses helicopter ground handling and marshalling signals. It provides learning objectives about gaining knowledge of internationally recognized helicopter marshalling signals and safety precautions for ground handling activities. It then defines ground handling, introduces marshalling and the roles of marshallers. The majority of the document details standard marshalling hand signals for helicopter operations on the ground to communicate with pilots. These signals include directions for taxiing, turns and stopping.
Helicopter doors, windows & windscreen. symmetrical checkBai Haqi
The document discusses helicopter doors, windows, windscreens and symmetry checks. It provides details on the construction, installation and maintenance of cockpit doors, cabin doors, windows and windscreens. It describes the different types of doors used on helicopters and their emergency escape mechanisms. The document also outlines how to perform airframe symmetry checks to ensure the fuselage and components are within dimensional limits after incidents like hard landings.
This document provides an overview of the components, systems, and instruments of the R22 helicopter. It describes the main components, which include the two main rotor blades, tail rotor, engine, drive system, landing gear, flight controls (cyclic, collective, throttle, pedals), and instruments. The flight controls section explains how each control affects the helicopter's movement and rotor RPM. The document then details several key components like the swash plate assembly, drive train, and clutch system.
This document provides instruction on helicopter ground handling, mooring, and jacking procedures for training at the Malaysian Institute of Aviation Technology. It discusses mooring helicopters to face the wind and retracting wheels when stationary. Jacking procedures are outlined, including using multiple personnel at designated jacking points and evenly distributing weight. Safety precautions for mooring, towing, and jacking helicopters are emphasized.
This document provides information about helicopter safety procedures for passengers. It outlines the types of helicopters used, prohibited items, check-in procedures, safety equipment, boarding and disembarking procedures, dangers of helicopters, and what to do during flight emergencies. Key safety equipment mentioned includes emergency breathing systems, life jackets, harnesses, and hearing protection. Passengers are instructed to follow crew instructions carefully and be aware of rotor blades, loose objects, and other hazards.
Top 10 airline cabin crew interview questions and answersjustingramke
In this file, you can ref interview materials for airline cabin crew such as types of interview questions, airline cabin crew situational interview, airline cabin crew behavioral interview…
1) FADEC systems use digital controls and computers to precisely regulate factors like fuel flow and engine speed, allowing consistent engine performance. HUMS monitors helicopter components for faults or reduced lifespan.
2) FADEC systems have wiring to sensors, actuators, and the aircraft to allow the electronic engine control unit to compute and relay control signals. HUMS includes onboard and ground equipment to analyze vibration and performance data.
3) FADEC and HUMS provide benefits like reduced maintenance, lower costs, increased safety and reliability compared to older mechanical controls. HUMS requires cooperation across organizations for its maintenance approach.
Disasters can be natural or man-made. Natural disasters include cyclones, earthquakes, tornados, volcanic eruptions, tsunamis, floods, wildfires, droughts, avalanches, and landslides. Man-made disasters involve human elements like negligence, intent, or technological failures and include nuclear bombings, acts of terrorism, and oil spills. The document then provides examples and details of some specific major natural and man-made disasters that have occurred throughout history.
Helikopter - bölüm 04 - helikopter sistemleri - emre akar
1. Helikopter Yapı ve Sistemleri
İstanbul Arel Üniversitesi – 2016
Emre Akar
2. İçindekiler
• Helikoptere Giriş
• Uçuş Aerodinamiği
• Uçuş Kumandaları
• Helikopter Yapısı ve Sistemleri
• Helikopter Uçuş Manueli
• Ağırlık ve Denge
• Helikopterlerde Performans
• Yer Prosedürleri ve Uçuş Öncesi Hazırlıklar
• Basit Uçuş Manevraları
• İleri Uçuş Manevraları
• Acil Durumlar ve Tehlikeler
• Helikopter Göstergeleri
• Gece Operasyonları
• Havacılıkta Efektif Karar Verme
Emre Akar, İstanbul Arel Üniversitesi - 2016 2
3. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 3
4. 04 – Helikopter Yapı Sistemleri
Sistemler
• Airframe yapı
• Gövde
• Ana rotor sistemi
• Swash plate
• Free wheeling unit
• Anti-tork sistemi
• Motor
• Dişli kutusu
• Yakıt sistemi
• Elektrik sistemi
• Hidrolik sistem
• SAS
• Anti-icing
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 4
5. 04 – Helikopter Yapı Sistemleri
Airframe Yapı
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 5
6. 04 – Helikopter Yapı Sistemleri
Airframe Yapı
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 6
7. 04 – Helikopter Yapı Sistemleri
Airframe Yapı
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 7
8. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 8
Airframe Yapı
9. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 9
Airframe Yapı
10. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 10
Airframe Yapı
11. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 11
Airframe Yapı
12. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 12
Airframe Yapı
13. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 13
Airframe Yapı
14. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 14
Airframe Yapı
15. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 15
Ana Rotor Sistemi
• Fully articulated rotor
• Semi-rigid rotor
• Rigid rotor
16. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 16
Ana Rotor Sistemi
• Fully articulated rotor
• Semi-rigid rotor
• Rigid rotor
17. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 17
Ana Rotor Sistemi
• Fully articulated rotor
• Semi-rigid rotor
• Rigid rotor
18. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 18
Ana Rotor Sistemi
• Fully articulated rotor
• Semi-rigid rotor
• Rigid rotor
19. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 19
Ana Rotor Sistemi
• Fully articulated rotor
• Semi-rigid rotor
• Rigid rotor
20. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 20
Ana Rotor Sistemi
• Fully articulated rotor
• Semi-rigid rotor
• Rigid rotor
21. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 21
Ana Rotor Sistemi
• Fully articulated rotor
• Semi-rigid rotor
• Rigid rotor
22. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 22
Ana Rotor Sistemi
• Fully articulated rotor
• Semi-rigid rotor
• Rigid rotor
23. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 23
Ana Rotor Sistemi
• Fully articulated rotor
• Semi-rigid rotor
• Rigid rotor
24. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 24
Ana Rotor Sistemi
• Fully articulated rotor
• Semi-rigid rotor
• Rigid rotor
25. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 25
Ana Rotor Sistemi
• Fully articulated rotor
• Semi-rigid rotor
• Rigid rotor
26. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 26
Ana Rotor Sistemi
• Fully articulated rotor
• Semi-rigid rotor
• Rigid rotor
27. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 27
Ana Rotor Sistemi
• Fully articulated rotor
• Semi-rigid rotor
• Rigid rotor
28. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 28
Ana Rotor Sistemi
• Fully articulated rotor
• Semi-rigid rotor
• Rigid rotor
29. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 29
Ana Rotor Sistemi
• Fully articulated rotor
• Semi-rigid rotor
• Rigid rotor
30. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 30
Swash Plate
31. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 31
Swash Plate
32. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 32
Swash Plate
33. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 33
Swash Plate
34. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 34
Swash Plate
35. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 35
Swash Plate
36. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 36
Freewheeling Unit
37. 04 – Helikopter Yapı Sistemleri
Rotor yerleşimlerine göre
• Geleneksel rotor
• Coaxial Rotor
• Intermeshing Rotor
• Tandem Rotor
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 37
38. 04 – Helikopter Yapı Sistemleri
Rotor yerleşimlerine göre
• Geleneksel rotor
• Coaxial Rotor
• Intermeshing Rotor
• Tandem Rotor
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 38
39. 04 – Helikopter Yapı Sistemleri
Rotor yerleşimlerine göre
• Geleneksel rotor
• Coaxial Rotor
• Intermeshing Rotor
• Tandem Rotor
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 39
40. 04 – Helikopter Yapı Sistemleri
Rotor yerleşimlerine göre
• Geleneksel rotor
• Coaxial Rotor
• Intermeshing Rotor
• Tandem Rotor
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 40
41. 04 – Helikopter Yapı Sistemleri
Rotor yerleşimlerine göre
• Geleneksel rotor
• Coaxial Rotor
• Intermeshing Rotor
• Tandem Rotor
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 41
42. 04 – Helikopter Yapı Sistemleri
Anti-Tork Sistemleri
• Geleneksel Kuyruk Rotoru
• Ducted Fan (Fenestron)
• Coaxial Rotor
• Intermeshing Rotor
• Tandem Rotor
• Notar
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 42
43. 04 – Helikopter Yapı Sistemleri
Anti-Tork Sistemleri
• Geleneksel Kuyruk Rotoru
• Ducted Fan (Fenestron)
• Coaxial Rotor
• Intermeshing Rotor
• Tandem Rotor
• Notar
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 43
44. 04 – Helikopter Yapı Sistemleri
Anti-Tork Sistemleri
• Geleneksel Kuyruk Rotoru
• Ducted Fan (Fenestron)
• Coaxial Rotor
• Intermeshing Rotor
• Tandem Rotor
• Notar
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 44
45. 04 – Helikopter Yapı Sistemleri
Anti-Tork Sistemleri
• Geleneksel Kuyruk Rotoru
• Ducted Fan (Fenestron)
• Coaxial Rotor
• Intermeshing Rotor
• Tandem Rotor
• Notar
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 45
46. 04 – Helikopter Yapı Sistemleri
Anti-Tork Sistemleri
• Geleneksel Kuyruk Rotoru
• Ducted Fan (Fenestron)
• Coaxial Rotor
• Intermeshing Rotor
• Tandem Rotor
• Notar
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 46
47. 04 – Helikopter Yapı Sistemleri
Anti-Tork Sistemleri
• Geleneksel Kuyruk Rotoru
• Ducted Fan (Fenestron)
• Coaxial Rotor
• Intermeshing Rotor
• Tandem Rotor
• Notar
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 47
48. 04 – Helikopter Yapı Sistemleri
Anti-Tork Sistemleri
• Geleneksel Kuyruk Rotoru
• Ducted Fan (Fenestron)
• Coaxial Rotor
• Intermeshing Rotor
• Tandem Rotor
• Notar
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 48
49. 04 – Helikopter Yapı Sistemleri
Anti-Tork Sistemleri
• Geleneksel Kuyruk Rotoru
• Ducted Fan (Fenestron)
• Coaxial Rotor
• Intermeshing Rotor
• Tandem Rotor
• Notar
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 49
50. 04 – Helikopter Yapı Sistemleri
Anti-Tork Sistemleri
• Geleneksel Kuyruk Rotoru
• Ducted Fan (Fenestron)
• Coaxial Rotor
• Intermeshing Rotor
• Tandem Rotor
• Notar
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 50
51. 04 – Helikopter Yapı Sistemleri
Anti-Tork Sistemleri
• Geleneksel Kuyruk Rotoru
• Ducted Fan (Fenestron)
• Coaxial Rotor
• Intermeshing Rotor
• Tandem Rotor
• Notar
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 51
52. 04 – Helikopter Yapı Sistemleri
Anti-Tork Sistemleri
• Geleneksel Kuyruk Rotoru
• Ducted Fan (Fenestron)
• Coaxial Rotor
• Intermeshing Rotor
• Tandem Rotor
• Notar
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 52
53. 04 – Helikopter Yapı Sistemleri
Anti-Tork Sistemleri
• Geleneksel Kuyruk Rotoru
• Ducted Fan (Fenestron)
• Coaxial Rotor
• Intermeshing Rotor
• Tandem Rotor
• Notar
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 53
54. 04 – Helikopter Yapı Sistemleri
Motor
• Pistonlu motor
• Türbin motor
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 54
55. 04 – Helikopter Yapı Sistemleri
Motor
• Pistonlu motor
• Türbin motor
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 55
56. 04 – Helikopter Yapı Sistemleri
Motor
• Pistonlu motor
• Türbin motor
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 56
57. 04 – Helikopter Yapı Sistemleri
Motor
• Pistonlu motor
• Türbin motor
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 57
59. 04 – Helikopter Yapı Sistemleri
Transmission
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 59
60. 04 – Helikopter Yapı Sistemleri
Transmission
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 60
61. 04 – Helikopter Yapı Sistemleri
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 61
Transmission
62. 04 – Helikopter Yapı Sistemleri
Clutch (Debriyaj)
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 62
63. 04 – Helikopter Yapı Sistemleri
Yakıt Sistemi
• Fuel Supply System
• Engine Fuel Control System
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 63
64. 04 – Helikopter Yapı Sistemleri
Elektrik Sistemi
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 64
70. 04 – Helikopter Yapı Sistemleri
SAS (Stability Augmentation
Systems)
• AFCS
• Autopilot
• IAS
• VHF
• VOR
• ILS
• GPS
• IFR
• FD
• Environmental Systems
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 70
71. 04 – Helikopter Yapı Sistemleri
Anti-icing Systems
• Engine
• Carburetor
• Airframe
• Deicing
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 71
72. 04 – Helikopter Yapı Sistemleri
Bölüm sonu…
İçindekiler SayfasıBölüm Başı
Emre Akar, İstanbul Arel Üniversitesi - 2016 72