US4170108A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Fuel injectors for gas turbine engines
Assignee: Rolls Royce PLC
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Filing: 1977-11-08
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Granted: 1979-10-09
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Expires: 1997-11-08
Abstract
Abstract A fuel injector for a gas turbine engine consists of a hollow body adapted to be supplied with compressed air and having a number of fuel orifices in the internal surface of the body. An annular member is located inside the body adjacent to the orifices so as to define an annular gap between it and the internal surface of the hollow body. The gap receives fuel from the orifices and has a radial width of 0.015 to 0.020 inches.
Inventors
- 👤 John A. Mobsby
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-26 05:36
CPC Classifications
F; F23; F23R; F23R3/00; F23R3/28; F23D; F23D11/00; F23D11/10; F23D11/106; F23D11/107
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
192 words
A fuel injector for a gas turbine engine comprising a hollow central body, an outer body which at least partly surrounds the central body and defines a flow passage therewith, said flow passage and the interior of the central body being adapted to receive a supply of compressed air, a plurality of orifices in the internal surface of said central body, each said orifice communicating with a flow duct in said central body, said flow duct being adapted to supply fuel to each of said orifices, an elongate annular member located adjacent said plurality of orifices so as to define an annular gap between it and said internal surface of said central body, which gap is adapted to receive a flow of fuel through said orifices, the minimum flow area of the gap being larger than the total flow area of said orifices so that the gap does not provide a flow controlling orifice for the fuel flow and the radial width of the gap having a value of 0.015 to 0.02 inches whereby it deforms the separate flows from said orifices into a substantially single annular flow of generally uniform thickness.
Claim 2
Dependent Claim
192 words
A fuel injector for a gas turbine engine comprising a hollow central body, an outer body which at least partly surrounds the central body and defines a flow passage therewith, said flow passage and the interior of the central body being adapted to receive a supply of compressed air, a plurality of orifices in the internal surface of said central body, each said orifice communicating with a flow duct in said central body, said flow duct being adapted to supply fuel to each of said orifices, an elongate annular member located adjacent said plurality of orifices so as to define an annular gap between it and said internal surface of said central body, which gap is adapted to receive a flow of fuel through said orifices, the minimum flow area of the gap being larger than the total flow area of said orifices so that the gap does not provide a flow controlling orifice for the fuel flow and the radial width of the gap having a value of 0.015 to 0.02 inches whereby it deforms the separate flows from said orifices into a substantially single annular flow of generally uniform thickness.
Claim 3
Dependent Claim
18 words
A fuel injector according to claim 1 wherein the radial width of the gap is substantially 0.016 inches.
Claim 4
Dependent Claim
29 words
A fuel injector as claimed in claim 1 and in which said fuel orifices are arranged to be the flow-controlling orifices in the said flow path through said injector.
Claim 5
Dependent Claim
39 words
A fuel injector as claimed in claim 3 in which said fuel orifices lie with their center lines in a plane perpendicular to said injector axis and make an acute angle with said internal surface of said central body.
Claim 6
Dependent Claim
17 words
A fuel injector as claimed in claim 4 in which said fuel orifices are of rectangular cross-section.
Claim 7
Dependent Claim
22 words
A fuel injector as claimed in claim 4 in which said interior of said hollow central body is of substantially cylindrical shape.
Claim 8
Dependent Claim
26 words
A fuel injector as claimed in claim 4 in which part of said interior of said hollow central body converges in the direction of the flow.
Claim 9
Dependent Claim
26 words
A fuel injector as claimed in claim 3 in which said annular member extends only part way to the downstream end of said hollow central body.
Claim 10
Dependent Claim
22 words
A fuel injector as claimed in claim 1 comprising an air deflector member, said deflector member being within said hollow central body.
References Cited (Backward Citations)
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1982-10-08 | 1983-04-09 | 1983-10-09 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1986-10-08 | 1987-04-09 | 1987-10-09 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1990-10-08 | 1991-04-09 | 1991-10-09 | $7700.00 | Window Closed / Lapsed |