US4080783A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Turbine engine lubrication system
Assignee: TDY Industries LLC
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Filing: 1976-07-28
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Granted: 1978-03-28
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Expires: 1996-07-28
Abstract
Abstract A bearing lubrication system for a turbine engine is provided which utilizes a fuel-air mist to both lubricate and cool the bearing assembly. An annular fuel-air distributor is positioned adjacent the bearing assembly and includes an inlet and several outlet ports directed towards the bearing assembly. A fuel port and a source of pressurized air are coupled to the inlet of the fuel-air distributor so that the pressurized air mixes the fuel into the air and projects a fuel-air mist through the distributor and onto the bearing assembly. A fuel metering device maintains the fuel-air ratio outside of its flammability range to prevent fires within the bearing cavity. Exhaust passageways from the bearing cavity are disposed adjacent the bearing outer race to provide additional cooling of the bearing assembly during the exhaustion of the fuel-air mist from the bearing cavity.
Inventors
- 👤 Glenn Hamburg
- 👤 Gytis Jasas
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-30 11:31
CPC Classifications
F; F01; F01D; F01D25/00; F01D25/18; F16; F16C; F16C33/00; F16C33/30; F16C33/66; F16C33/6637; F16C33/6659; F16C19/00; F16C19/22; F16C19/24; F16C19/26; F16C2360/00; F16C2360/23
Claims Analysis
Total Claims: 12
Claim 1
Independent Claim
144 words
A lubrication system for a turbine for lubricating a bearing assembly within a bearing cavity, said system comprising: a source of pressurized air; an annular distributor contained within the bearing cavity and having inlet means comprising an annular groove in the distributor, said distributor further having outlet means comprising a plurality of substantially axial passageways, each passageway being open at one end to said annular groove and open at its other end to the bearing cavity; first passage means for fluidly connecting said pressurized air source with said distributor inlet means so that a fluid flow through said distributor is obtained; a source of fuel, and second passage means for fluidly connecting said fuel source to said first passage means, whereby an air-fuel mixture forms the fluid flow through said distributor, wherein said air-fuel mixture impinges upon said bearing assembly to lubricate the same.
Claim 2
Dependent Claim
144 words
A lubrication system for a turbine for lubricating a bearing assembly within a bearing cavity, said system comprising: a source of pressurized air; an annular distributor contained within the bearing cavity and having inlet means comprising an annular groove in the distributor, said distributor further having outlet means comprising a plurality of substantially axial passageways, each passageway being open at one end to said annular groove and open at its other end to the bearing cavity; first passage means for fluidly connecting said pressurized air source with said distributor inlet means so that a fluid flow through said distributor is obtained; a source of fuel, and second passage means for fluidly connecting said fuel source to said first passage means, whereby an air-fuel mixture forms the fluid flow through said distributor, wherein said air-fuel mixture impinges upon said bearing assembly to lubricate the same.
Claim 3
Dependent Claim
40 words
The invention as defined in claim 1 and including fuel metering means operatively disposed in said second passage means for maintaining said air-fuel mixture at a high air to fuel ratio to thereby inhibit the ignition of said air-fuel mixture.
Claim 4
Dependent Claim
21 words
The invention as defined in claim 1 and including third passage means for exhausting said air-fuel mixture from said bearing cavity.
Claim 5
Dependent Claim
34 words
The invention as defined in claim 3 wherein said third passage means is disposed adjacent said bearing assembly to thereby cool said bearing assembly upon exhaustion of the fuel-air mixture from the bearing cavity.
Claim 6
Dependent Claim
56 words
The invention as defined in claim 4 wherein said bearing assembly includes an outer race and wherein said third passage means comprises a plurality of circumferentially spaced axial grooves adjacent the outer periphery of said outer race open on one end to said bearing cavity and at the other end to the exhaust from the turbine.
Claim 7
Dependent Claim
21 words
The invention as defined in claim 2 wherein said fuel metering means comprises a member having a restricted orifice formed therethrough.
Claim 8
Dependent Claim
166 words
A lubrication system for a turbine for lubricating a bearing assembly having an outer race and being positioned within a bearing cavity, said system comprising: a source of pressurized air; first passage means for fluidly connecting said pressurized air source to said bearing cavity; a source of fuel; second passage means for fluidly connecting said fuel source to said first passage means so that said fuel mixes with said air and forms an air-fuel mixture which is projected into said bearing cavity to thereby lubricate said bearing assembly; and third passage means for exhausting said air-fuel mixture from said bearing cavity, said third passage means further comprising a plurality of circumferentially spaced axial grooves adjacent the outer periphery of said outer race, each groove being open at one end to said bearing cavity and at the other end to an exhaust from said turbine, whereby the exhaustion of the air-fuel mixture from said bearing cavity and through said third passage means further cools said bearing assembly.
Claim 9
Dependent Claim
166 words
A lubrication system for a turbine for lubricating a bearing assembly having an outer race and being positioned within a bearing cavity, said system comprising: a source of pressurized air; first passage means for fluidly connecting said pressurized air source to said bearing cavity; a source of fuel; second passage means for fluidly connecting said fuel source to said first passage means so that said fuel mixes with said air and forms an air-fuel mixture which is projected into said bearing cavity to thereby lubricate said bearing assembly; and third passage means for exhausting said air-fuel mixture from said bearing cavity, said third passage means further comprising a plurality of circumferentially spaced axial grooves adjacent the outer periphery of said outer race, each groove being open at one end to said bearing cavity and at the other end to an exhaust from said turbine, whereby the exhaustion of the air-fuel mixture from said bearing cavity and through said third passage means further cools said bearing assembly.
Claim 10
Dependent Claim
44 words
The invention as defined in claim 7 wherein said first passage means includes an annular distributor contained within the bearing cavity and having an inlet means for receiving the air-fuel mixture and an outlet means for directing said air-fuel mixture toward said bearing assembly.
Claim 11
Dependent Claim
48 words
The invention as defined in claim 8 wherein said inlet means comprises an annular groove in said distributor and wherein said outlet means comprises a plurality of substantially axial passageways open at one end to said annular groove and open at their other end to said bearing cavity.
Claim 12
Dependent Claim
40 words
The invention as defined in claim 7 and including further means for injecting air into said third passage means to thereby produce a high air to fuel ratio in said mixture to thereby inhibit the ignition of said air-fuel mixture.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1981-03-27 | 1981-09-26 | 1982-03-28 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1985-03-27 | 1985-09-26 | 1986-03-28 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1989-03-27 | 1989-09-26 | 1990-03-28 | $7700.00 | Window Closed / Lapsed |