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AIRCRAFT MAINTENANCE ENGINEERING: BRAYTON CYCLE OF OPERATION
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Interested in Avionics, Visit, http:/ avionics0.blogspot.com. Saturday, July 30, 2011. BRAYTON CYCLE OF OPERATION. Figure 1.2. Typical Free-Power Turboshaft Engine. Subscribe to: Post Comments (Atom). TURBINE AIR INLET SECTION. ADVANTAGES OF TURBINE ENGINES. BRAYTON CYCLE OF OPERATION. Subscribe in a reader. Awesome Inc. template. Powered by Blogger.
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AIRCRAFT MAINTENANCE ENGINEERING: AME M-10 QUESTIONS
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Interested in Avionics, Visit, http:/ avionics0.blogspot.com. 1 State of registry means. A) country responsible for design of aircraft. B) country on whose register the aircraft is entered. C) country where the owners are based. 2 Contacting state means. A) country that leases aircraft on contract. B) any state that is party tot e convention on international civil aviation. C) country where federal aviation regulation apply. 3 Certificate of release to service of aircrafts is raised when. C) until aircra...
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AIRCRAFT MAINTENANCE ENGINEERING: June 2011
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Interested in Avionics, Visit, http:/ avionics0.blogspot.com. Thursday, June 9, 2011. Thermal expansion valve(ATA 21). A thermal expansion valve. Subscribe to: Posts (Atom). Subscribe in a reader. Awesome Inc. template. Powered by Blogger.
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AIRCRAFT MAINTENANCE ENGINEERING: AME M-8 QUESTIONS
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Interested in Avionics, Visit, http:/ avionics0.blogspot.com. The earth’s atmosphere can be said to consists of four concentric gaseous layers. The order stating from the earth surface is:. Tropopause, stratosphere, Mesophere and Thermosphere. Tropopause, Mesophere, Stratosphere and Tropopause. Stratosphere, Tropopause, Mesophere and Thermosphere. Troposphere, Stratosphere Mesophere and Thermosphere. In the stratosphere Temperature. Decreases at a steady rate. Increase at a steady rate. Remain constant i...
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AIRCRAFT MAINTENANCE ENGINEERING: July 2011
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Interested in Avionics, Visit, http:/ avionics0.blogspot.com. Saturday, July 30, 2011. Figure 1.29. Exhaust Diffuser Section. Figure 1.30. Divergent Exhaust Duct. Figure 1.21. Axial-flow Turbine Rotor. Figure 1.22. Radial Inflow Turbine. Figure 1.23. Impulse-Reaction Turbine Blade. Single-rotor turbine. Some gas turbine engines use a single-rotor turbine, with the power developed by one rotor. This arrangement is used on engines where low weight and compactness are necessary. A single-rotor, ...Multiple-...
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AIRCRAFT MAINTENANCE ENGINEERING: AME M-2 QUESTIONS
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Interested in Avionics, Visit, http:/ avionics0.blogspot.com. 1 What describes the physical nature of a gas? A) Definite volume and shape. B) Incompressible , takes the shape of the container. C) Compressible, takes the shape of the container. 2 What is true on Hydrogen Atom? A) It has one neutron. B) It has one proton. C) It has two nucleons. 3 If the symbol of a given atom is , then number of Protons it has is,. 4 If the symbol of a given atom is , , then it’s number of neutrons are,. C) Change in state.
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AIRCRAFT MAINTENANCE ENGINEERING: TURBINE AIR INLET SECTION
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Interested in Avionics, Visit, http:/ avionics0.blogspot.com. Saturday, July 30, 2011. TURBINE AIR INLET SECTION. Subscribe to: Post Comments (Atom). TURBINE AIR INLET SECTION. ADVANTAGES OF TURBINE ENGINES. BRAYTON CYCLE OF OPERATION. Subscribe in a reader. Awesome Inc. template. Powered by Blogger.
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AIRCRAFT MAINTENANCE ENGINEERING: AME M-3 QUESTIONS
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Interested in Avionics, Visit, http:/ avionics0.blogspot.com. 1A DC shunt generator without a voltage regulator,if the load increases the generator output voltage will. 2The out from an AC generator is taken. 3What is the cause of generator brush arching. 4Whwn AC generators are operating in parallel the. AAmphere and frequency both are equa;. BFrequency and voltage both are equal*. CAmphere and voltage are equal. 6The pole piece or shoe used in DC generator are parts of. CThe load on the generator*.
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AIRCRAFT MAINTENANCE ENGINEERING: COMPRESSOR SECTION
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Interested in Avionics, Visit, http:/ avionics0.blogspot.com. Saturday, July 30, 2011. Ram air pressure - free stream air pressure provided by the forward motion of the engine. Centrifugal-flow compressor. Figure 1.12 shows the basic components of a centrifugal-flow compressor: rotor, stator, and compressor manifold. Figure 1.12. Typical Single-stage Centrifugal Compressor. Figure 1.13. Axial-flow Compressor. Figure 1.14. Compressor Efficiencies and Pressure Ratios. Subscribe to: Post Comments (Atom).
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AIRCRAFT MAINTENANCE ENGINEERING: February 2011
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Interested in Avionics, Visit, http:/ avionics0.blogspot.com. Wednesday, February 23, 2011. In aviation, self-sealing fuel tank. Is a fuel tank technology in wide use since World War II that prevents fuel tanks primarily on aircraft from leaking fuel and igniting after being damaged by enemy fire. In additions to fighter aircraft some military patrol vehicles and armoured limousines for VIP use also feature self-sealing fuel tanks. Monday, February 14, 2011. Available width at airport gates). Airbus A310...
