US4168803A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Air-ejector assisted fuel nozzle
Assignee: Parker Hannifin Corp
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Filing: 1977-08-31
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Granted: 1979-09-25
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Expires: 1997-08-31
Abstract
Abstract A nozzle for atomizing fuel for combustion in a gas turbine engine. During normal operation of the engine, the nozzle uses a portion of the air supplied to the combustion chamber by the engine compressor to atomize fuel flowing through the nozzle. During start-up and low power operation of the engine when flow of engine air through the nozzle would otherwise be of insufficient velocity to cause good atomization of the fuel, additional air from a separate external source is introduced at high velocity into the nozzle in the manner of an ejector. The additional air imparts high velocity to the engine air within the nozzle so that the air from both sources acts on the fuel at the nozzle discharge orifice at high velocity to effect good atomization and spray pattern of the fuel. The nozzle is designed in such a manner as to cause no significant restriction of engine air flow through the nozzle under high power operation of the engine when the external air source is shut off.
Inventors
- 👤 Harold C. Simmons
- 👤 Robert T. Mains
- 👤 Frank Menti, Jr.
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 05:22
CPC Classifications
F; F23; F23D; F23D11/00; F23D11/10; F23D11/106; F23D11/107; F02; F02C; F02C7/00; F02C7/22; F02C7/236; F02C7/2365; F02C7/26; F23D2900/00; F23D2900/11101
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
119 words
A fuel atomizing nozzle for gas turbine engines, said nozzle including a passage for fuel terminating in a discharge orifice, a first passage for air to be received from the engine and communicating with the fuel passage upstream of the orifice, a second passage for receiving high velocity fluid from a source separate of the engine, said second passage comprising a tubular conduit located centrally of a portion of the first passage and projecting into said first passage, said first passage being unobstructed except for said tubular conduit, whereby said high velocity fluid discharging from said tubular conduit into said portion of the first passage imparts high velocity to the air from the first passage flowing to said orifice.
Claim 2
Dependent Claim
119 words
A fuel atomizing nozzle for gas turbine engines, said nozzle including a passage for fuel terminating in a discharge orifice, a first passage for air to be received from the engine and communicating with the fuel passage upstream of the orifice, a second passage for receiving high velocity fluid from a source separate of the engine, said second passage comprising a tubular conduit located centrally of a portion of the first passage and projecting into said first passage, said first passage being unobstructed except for said tubular conduit, whereby said high velocity fluid discharging from said tubular conduit into said portion of the first passage imparts high velocity to the air from the first passage flowing to said orifice.
Claim 3
Dependent Claim
47 words
The nozzle of claim 1 in which said first passage has inlet and outlet ends and has a portion intermediate said ends of smaller diameter than the diameters at said ends, and said tubular conduit projects into said inlet end and terminates upstream of said intermediate portion.
Claim 4
Dependent Claim
51 words
The nozzle of claim 1 further including an annulus interposed between said fluid source and said second passage for communicating said fluid therebetween, said annulus causing swirling of said fluid passing therethrough and in said second passage resulting in the increased atomization of said fuel as it exits from said orifice.
Claim 5
Dependent Claim
24 words
The nozzle of claim 3 further including means in said tubular conduit for adjusting the volume and velocity of said fluid from said source.
Claim 6
Dependent Claim
175 words
A fuel atomizing nozzle for gas turbine engines, comprising a body member adapted for positioning in the air manifold of the gas turbine engine, said body member having a central, unobstructed, circular cross-section passage therein with an inlet and an outlet communicating respectively with the manifold and combustion chamber of the engine, an annular fuel passage in said body member having tangential swirl-producing orifices adapted to swirl fuel in said central passage near the outlet thereof to be acted upon by engine air passing through said central passage, an annular air passage in said body member communicating the engine air manifold and the combustion chamber, said air passage surrounding said central passage outlet and having swirl-producing means therein for swirling air passing therethrough into engagement with fuel from said central passage, and an auxiliary fluid orifice centrally located in said central passage near said inlet thereof and positioned to direct the flow of auxiliary fluid away from said inlet and toward said outlet of said central passage to assist the flow of engine air therethrough.
Claim 7
Dependent Claim
175 words
A fuel atomizing nozzle for gas turbine engines, comprising a body member adapted for positioning in the air manifold of the gas turbine engine, said body member having a central, unobstructed, circular cross-section passage therein with an inlet and an outlet communicating respectively with the manifold and combustion chamber of the engine, an annular fuel passage in said body member having tangential swirl-producing orifices adapted to swirl fuel in said central passage near the outlet thereof to be acted upon by engine air passing through said central passage, an annular air passage in said body member communicating the engine air manifold and the combustion chamber, said air passage surrounding said central passage outlet and having swirl-producing means therein for swirling air passing therethrough into engagement with fuel from said central passage, and an auxiliary fluid orifice centrally located in said central passage near said inlet thereof and positioned to direct the flow of auxiliary fluid away from said inlet and toward said outlet of said central passage to assist the flow of engine air therethrough.
Claim 8
Dependent Claim
19 words
The fuel nozzle as set forth in claim 5 further including means for imparting swirl to the auxiliary fluid.
Claim 9
Dependent Claim
35 words
The fuel nozzle as set forth in claim 6 further including means for imparting swirl to the engine air passing through said central passage prior to combination of such engine air with the auxiliary fluid.
Claim 10
Dependent Claim
27 words
The fuel nozzle as set forth in claim 7 wherein said auxiliary fluid orifice is the outlet of a tubular conduit positioned at said central passage inlet.
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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) | 1982-09-24 | 1983-03-26 | 1983-09-25 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1986-09-24 | 1987-03-26 | 1987-09-25 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1990-09-24 | 1991-03-26 | 1991-09-25 | $7700.00 | Window Closed / Lapsed |