Device and method for supplying non-propulsive power for an aircraft
A technology for propulsion power and aircraft, applied in auxiliary power equipment, mechanical equipment, air handling equipment, etc., can solve problems such as low electric drive energy efficiency, and achieve the effect of improving efficiency
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[0056] The invention is described with respect to an aircraft including one or more main engines for moving the aircraft. The aircraft further comprises a passenger cabin which must be regulated for pressure and / or temperature. refer to figure 2 An apparatus 10 for providing non-propulsion power is described.
[0057] The device 10 for providing non-propulsion power comprises an Environmental Control System 1, known to those skilled in the art by the term ECS, and an Auxiliary Power Unit 4, known to those skilled in the art by the term APU. According to the invention, the ECS 1 and APU 4 are coupled such that the APU 4 provides power to the ECS unit 1 and thus reduces the take-off power obtained from the main engines of the aircraft.
[0058] ECS 1
[0059] like figure 2 As shown in , the ECS 1 includes a turbine 12 and a load compressor 11, the turbine 12 is used to transfer the conditioned air A reg Distributed into the aircraft nacelle 2 , the load compressor 11 is...
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