1,173,841. Gas turbine engine fuel systems. ROLLS-ROYCE Ltd. March 21, 1967 [Jan.13, 1967], No.2075/67. Heading F1G. [Also in Division G3 ] An aircraft gas turbine engine fuel system comprises a metering device which controls the supply of fuel to engine burners, means for ...
Fuel control system for gas turbine engine A fuel control system for a gas turbine engine of the kind having at least one compressor (12, 14) and turbine spool (20, 22) and a free turbine (24), comprising a pneumatic fuel metering device (34) whose metering valve is controlled by......
1cars engine fuel injection and ignition system specialist training information model 4 热度: Aircraft gas turbine engine s control based on the fuel injection control 热度: A simulation of aircraft fuel management system 热度: 1. Titl e Aircraft reciprocating engine fuel syst em components repai ...
A fuel drain can assembly positioned between the fuel manifold and the fuel nozzles of a gas turbine engine which utilizes detachable connectors rotatable into locking engagement without special tooling.doi:US5259185 APeterson, Ivan H.USUS5259185 1992年6月5日 1993年11月9日 General Electric ...
The invention relates to a method for supplying fuel to a in an aircraft built-in aircraft gas turbine as well as a fuel supply system. In order in which these negative influences by air into the fuel lines to be avoided, is provided according to the invention that the fuel with an incr...
the compressor and fan of a double-flow turbojet engine., and the compressor and propeller of a turboprop engine. Aircraft gas turbines are also used to drive auxiliary equipment of engines and aircraft, such as starters, electrical generators, fuel pumps, and oxygen pumps in liquid-fuel rocket...
United States Patent US2519624 Note: If you have problems viewing the PDF, please make sure you have the latest version ofAdobe Acrobat. Back to full text
Aircraft engine fuel system and method of operating the same An aircraft engine fuel system 900 is disclosed having a gas turbine engine 101, a turbocharger 910, a compressor bleed air system 930 for providing compressor air (A) from the gas turbine engine 101 to the turbocharger 910, and ...
Design and part-load performance of a hybrid system based on a solid oxide fuel cell reactor and a micro gas turbine This paper addresses the design and off-design analysis of a hybrid system (HS) based on the coupling of a recuperated micro gas turbine (MGT) with a high ... P. ...
The fuel system of aircraft is always the weakest link in terms of security [34]. Because the flash point ofaviation fueloil is very low and the carrying amount increases constantly, there is often the danger that the fuel will catch fire and explode. In addition, the aircraft fuel tank ...