US5022228A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Over the shaft fuel pumping system
Assignee: Honeywell International Inc
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Filing: 1990-09-13
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Granted: 1991-06-11
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Expires: 2010-09-13
Abstract
Abstract A large flow of high pressure fuel is supplied to a gas turbine engine by mounting a small modified vortex pump over or around a main high speed shaft. The pump includes a plurality of short, stubby impeller blades rotating at a very high speed within a fuel filled annular chamber having an axial fuel inlet and a tangential fuel outlet. A pump booster and priming system ensures the pump fills with fuel during operation.
Inventors
- 👤 Jay N. Hoopes
- 👤 Christopher D. Eick
- 👤 John R. Williamson
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-30 21:36
CPC Classifications
F; F04; F04D; F04D5/00; F02; F02C; F02C7/00; F02C7/22; F04D13/00; F04D13/02; F04D13/04; F04D9/00; F04D9/004; F04D9/005; Y; Y02; Y02T; Y02T50/00; Y02T50/60
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
140 words
A high speed rotary liquid pump, adapted to be driven by a shaft in the core of a gas turbine engine, comprising a rotatable impeller having a plurality of straight blades extending radially from an annular hub, said hub having a central aperture of sufficient size to engage said shaft for rotation therewith; a pump housing surrounding said impeller and defining a generally annular pump cavity for receiving said rotatable impeller; said housing also defining an annular fluid inlet aperture leading axially into said cavity adjacent said hub, a shield member axially adjacent said aperture and disposed between fluid entering said aperture and said shaft, whereby circumferential swirl of said fluid due to contact with said shaft is minimized, and at least one fluid outlet passage extending tangentially from the periphery of said cavity adjacent the tips of said blades.
Claim 2
Dependent Claim
140 words
A high speed rotary liquid pump, adapted to be driven by a shaft in the core of a gas turbine engine, comprising a rotatable impeller having a plurality of straight blades extending radially from an annular hub, said hub having a central aperture of sufficient size to engage said shaft for rotation therewith; a pump housing surrounding said impeller and defining a generally annular pump cavity for receiving said rotatable impeller; said housing also defining an annular fluid inlet aperture leading axially into said cavity adjacent said hub, a shield member axially adjacent said aperture and disposed between fluid entering said aperture and said shaft, whereby circumferential swirl of said fluid due to contact with said shaft is minimized, and at least one fluid outlet passage extending tangentially from the periphery of said cavity adjacent the tips of said blades.
Claim 3
Dependent Claim
20 words
The pump of claim 1 further including at least one baffle bridging said annular inlet aperture in a radial direction.
Claim 4
Dependent Claim
18 words
The pump of claim 1 wherein said plurality of blades in from about eight to about twelve blades.
Claim 5
Dependent Claim
36 words
The pump of claim 1 wherein said fluid outlet passage has a first, generally tubular, throat section in fluid communication with said cavity, and a second, generally conically diverging, diffuser section downstream from said first section.
Claim 6
Dependent Claim
31 words
The pump of claim 1 wherein said impeller has a blade diameter which is less than twice the diameter of said shaft so that said pump is compact and light weight.
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) | 1994-06-10 | 1994-12-10 | 1995-06-11 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1998-06-10 | 1998-12-10 | 1999-06-11 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2002-06-10 | 2002-12-10 | 2003-06-11 | $7700.00 | Window Closed / Lapsed |