US 5,201,798 A · Multifunction integrated power unit and power transfer apparatus therefor

Abstract

A multifunction integrated power unit (MIPU) (10) for use aboard aircraft provides the functions both of an auxiliary power unit and of an emergency power unit while being smaller, lighter, and less expensive than the two units it replaces. Additionally, the integration of both functions in a single unit allows elimination of duplicated service devices and a further reduction in size, cost, and weight in the aircraft itself. The MIPU (10) includes two turbine engines (12, 22) operable under differing conditions, an integrating gear box (34) receiving power from the two engines (12, 22) selectively, and a plurality of accessory devices (36, 38) receiving shaft power from either of the two engines (12, 22) via the gear box (34). The gear box (34) includes a power transfer unit (PTU) apparatus (108) which selectively delivers shaft power from one of the engines (12, 22) to the accessory devices (36, 38).

Claims17

Dependent claims

A power transfer unit comprising an elongate tubular member, said tubular member externally defining first cooperating means for journaling said tubular member upon a housing, said tubular member further externally defining second cooperating means for rotatable shaft power distribution delivering torque from said tubular member to a shaft power consuming device, and a pair of oppositely disposed one-way overrunning clutches carried within said tubular member, each of said pair of clutches being disposed to transmit torque to said tubular member in one rotational direction and to allow said tubular member to overrun relative thereto in said one direction, when said tubular member is rotationally driven at a higher speed by the other of said pair of clutches, each one of said pair of clutches including means for receiving shaft power transmitted thereto.

A combined auxiliary and emergency power unit comprising:

a gear box;
energy producing equipment mechanically coupled to said gear box to be driven when said gear box is provided with a rotary power input;
first and second turbine wheels for producing said rotary power input;
first and second clutches respectively coupled to said first and second turbine wheels;
a rotary compressor connected to said first turbine wheel to be driven thereby and for providing a compressed air source;
a first combustor for receiving fuel and compressed air from said compressor and combusting the same;
a first nozzle connected to said first combustor and for directing products of combustion therefrom at said first turbine wheel to drive the same and thus cause auxiliary power unit operation when said first clutch is engaged;
a high pressure storage container for storing a compressed air-based oxidant;
a second combustor for receiving fuel and compressed oxidant from said storage container and combusting the same;
a second nozzle connected to said second combustor for receiving combustion gas therefrom and directing the same at said second turbine wheel to drive the same and thus cause emergency power unit operation when said second clutch is engaged;
and
a power transfer unit mounted in said gear box and including a tubular member, in which said first and second clutches are mounted for delivering said rotary power input thereto, and said tubular member externally defining a gear portion for delivering said rotary power input to said gear box.

9 more elements

Dependencies are inferred from the claim text.

Multifunction integrated power unit and power transfer apparatus therefor

Life of this patent

Multifunction integrated power unit and power transfer apparatus therefor

Life of this patent

Abstract

Claims17