Alejandro Sanchez Perez

US Patent:

20180215475, Aug 2, 2018

Filed:

Feb 1, 2017

Appl. No.:

15/421692

Inventors:

- Schenectady NY, US
Robert Gregory Carita - Needham MA, US
Thomas Edward Brinson - Mason OH, US
Matthew Robert Cerny - West Chester OH, US
David Vickery Parker - Middleton MA, US
Alejandro Yatzail Perez Valdez - Cincinnati OH, US

International Classification:

B64D 13/08
F02C 6/08

Abstract:

Systems and methods for integrated power and thermal management in a turbine-powered aircraft are provided. The systems may include rotationally-independent first and second auxiliary power unit shafts, a power turbine, a first compressor, a second compressor, a cooling turbine, and an electrical motor-generator. The power turbine may be rotatably disposed on the first auxiliary power unit shaft. The first compressor may be rotatably disposed on the first auxiliary power unit shaft. The second compressor may be rotatably disposed on the second auxiliary power unit shaft. The cooling turbine may be rotatably disposed on the second auxiliary power unit shaft. The electrical motor-generator may disposed on the first auxiliary power unit shaft to alternatively supply a motive force input to the first auxiliary power unit shaft and an electrical power output to the aircraft.