Gravity scavenged generator with integral engine oil tank

• US 8,893,856 B2
• Filed: 07/24/2008
• Issued: 11/25/2014
• Est. Priority Date: 07/24/2008
• Status: Expired due to Fees

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Frost, Cristopher
• Primary Examiner(s): LIU, HENRY Y
• Application Number:
  US12/179,357
• Publication Number:
  US 20100019505A1
• Time in Patent Office: 2,315 Days
• Field of Search: 184/6.11, 184/65, 184/6.12, 60/390.8, 608/02, 415/110
• US Class Current: 184/6.11
• CPC Class Codes: B64D 2041/002 Mounting arrangements for auxiliary power units (APU's)
• CPC Class Codes: F01D 25/18 Lubricating arrangements of machines or engines in general F01M
• CPC Class Codes: F02C 7/32 Arrangement, mounting, or driving, of auxiliaries
• CPC Class Codes: F05D 2260/602 Drainage
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A generator having an integral oil tank for an auxiliary power unit (APU) is provided. A gas turbine engine has a turbine shaft extending from an aft portion to a forward portion where it is in communication with a gear box mounted thereto. The gearbox advantageously has at least one oil gravity drain passage in flow communication with a lower portion thereof and is suitable for reducing the speed of the turbine shaft by gear reduction to power an oil cooled generator attached thereto. The oil cooled generator has at least one oil gravity drain passage therein. An engine oil tank is integral with and advantageously removable from the generator and is in flow communication with each oil gravity drain passage making is suitable for gravity scavenging oil from the generator and advantageously the gearbox.

Claims

1. An auxiliary power unit for an aircraft comprising:

a turbine internal combustion engine having a turbine main shaft and a forward bearing supporting the turbine shaft;

a gearbox with gears connected to be driven by the turbine main shaft, the gearbox including a lower portion;

an oil cooled generator including a rotor forward end, a rotor aft end, and a rotor shaft extending from the rotor aft end to the rotor forward end, the rotor shaft substantially parallel to the turbine main shaft, and connected to be driven by the gears, the oil cooled generator being mounted on the gearbox so that the gearbox is interposed between the generator and the engine, and said oil cooled generator having at least one generator oil gravity drain passage in flow communication with a lower portion thereof;

an oil pump connected to deliver oil to the generator, to the forward bearing, and to the gearbox;

an oil tank including a bottom wall and extending from a lower portion of said generator, the oil tank being in fluid communication with the oil pump and disposed to gravitationally scavenge the oil from said at least one generator oil gravity drain passage in said oil cooled generator;

a gearbox oil gravity drain passage fluidly connecting the engine forward bearing and lower portion of the gearbox with the oil tank to gravitationally scavenge oil into the oil tank from the engine forward bearing and the gearbox;

an oil tube adapted to carry oil from the oil tank to the oil pump; and

a screen disposed in the oil tank, wherein the screen is disposed between an open top end of the oil tank and an inlet of the oil tube, wherein the oil tube passes through an aperture in the screen

and wherein the rotor shaft is angled downwards towards the rotor forward end in relation to the oil tank bottom wall.

2. The auxiliary power unit of claim 1 wherein said oil tank has an attachment flange extending outward from a sidewall.

3. The auxiliary power unit of claim 1 wherein said lower portion of said generator has an open bell shape, a lower exterior perimeter of said open bell shaped lower portion has a flange outwardly extending therefrom.

4. The auxiliary power unit of claim 1 wherein said generator has an oil gravity drain passage in flow communication with the generator rotor forward end, and an oil gravity drain passage in flow communication with the generator rotor aft end.

5. The auxiliary power unit of claim 1 wherein the screen is disposed between said at least one generator oil gravity drain passage and a bottom wall of said oil tank, and the screen is disposed between the gearbox oil gravity drain passage and the bottom wall of the oil tank.

6. The auxiliary power unit of claim 1 wherein said oil tank is removably mounted to said generator.

7. The auxiliary power unit of claim 1 wherein said oil tank is comprised of fire resistant material.

8. The auxiliary power unit of claim 7 wherein said oil tank is comprised of steel.

9. The auxiliary power unit of claim 1 wherein a sidewall of said oil tank is cylindrical.

10. The auxiliary power unit of claim 1 wherein a bottom wall of said oil tank slopes toward a lower portion.

11. The auxiliary power unit of claim 10 wherein said oil tank bottom wall is conical.

12. The auxiliary power unit of claim 1 being installed in the tailcone of an aircraft in a horizontal or forward end angled down orientation, said auxiliary power unit forward end having said generator.

13. An auxiliary power unit comprising:

an oil cooled generator including a rotor forward end, a rotor aft end, and a rotor shaft extending from the rotor aft end to the rotor forward end; and

an oil tank including a bottom wall,

said oil tank extending from a lower portion of said generator wherein the rotor shaft is angled downwards towards the rotor forward end in relation to the oil tank bottom wall,

said generator receiving power from a gearbox of said auxiliary power unit,

said generator having oil gravity drain passages in flow communication with each end of a generator rotor,

said oil gravity drain passages being in flow communication with said oil tank,

the gearbox being axially displaced from the oil tank, and

the gearbox having a lower portion with a gearbox lower wall, and a gearbox-gravity drain passage through the gearbox lower wall in flow communication with the oil tank, the gearbox lower wall separating the gearbox from the oil tank.

14. The auxiliary power unit of claim 13 wherein said oil tank is removable from said generator.

15. The auxiliary power unit of claim 13 wherein said generator and oil tank assembly has a screen therein above a bottom wall of said oil tank and below said oil gravity drain passages in said generator.

16. The auxiliary power unit of claim 13 wherein said oil tank has a sidewall extending downward from said generator to a bottom wall, said bottom wall sloping to a lower portion having an oil tank drain plug.