Integrated power unit control apparatus and method

Power plants – Combustion products used as motive fluid

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60 3927, 60727, 60 39142, F02C 950

Patent

active

050604694

ABSTRACT:
The invention relates to secondary power system apparatus and method for use aboard aircraft in place of conventional auxiliary power units (APU's) and emergency power units (EPU's). The invention integrated power unit (IPU) performs the function of both on APU and an EPU, while avoiding the use of hazardous monofuels. The IPU includes a turbine engine operable on pressurized ambient air, or on pressurized stored air, along with jet engine fuel. The structure of a combustion chamber for the engine which is able to use pressurized air from two separate sources; of a control able to selectively operate the engine as an EPU, as an APU, and to effect operating transition from EPU to APU; and of a complete secondary power system with the IPU are all disclosed.

REFERENCES:
patent: 2643511 (1953-06-01), Briggs
patent: 2711073 (1955-06-01), Atkinson
patent: 2873577 (1959-02-01), Kenney et al.
patent: 3866058 (1975-02-01), Lenssen
patent: 4777793 (1988-10-01), Weigand et al.
patent: 4815277 (1989-03-01), Vershure, Jr. et al.

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