Patent US4351150A successfully refreshed from Google Patents.
US4351150A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Auxiliary air system for gas turbine engine
Assignee: General Electric Co
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Filing: 1980-02-25
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Granted: 1982-09-28
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Expires: 2000-02-25
Abstract
Abstract An auxiliary air system contained within the nacelle of a gas turbine engine having the functions of cooling engine components and measuring air inlet temperature. The system comprises an air ducting pipe, temperature sensors extending into the pipe, a structure to be cooled, such as an electronics module, preferably with a heat transfer chamber, an air flow inducer, and, if desired, means for directing air onto other engine components.
Inventors
- 👤 Wallace M. Schulze
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-30 13:44
CPC Classifications
F; F01; F01D; F01D17/00; F01D17/02; F01D17/08; F01D17/085; F02; F02C; F02C7/00; F02C7/04; F02C7/047; F05; F05D; F05D2260/00; F05D2260/60; F05D2260/601
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
142 words
An auxiliary air system contained within the engine nacelle between the engine core and the engine cowling of a gas turbine engine and comprising: (a) an air ducting pipe having one end communicating with an aperture in an external surface of said engine cowling, said aperture lying in a plane generally parallel to the airstream adjacent said aperture; (b) at least one environmental sensor arranged to sense the condition of air within said pipe; (c) a structure to be cooled connected to the other end of said air ducting pipe; (d) an air flow device in communication with said structure to be cooled and effective to move air from the exterior of said cowling through said structure to be cooled, and to said air flow device; and (e) means for directing air from said air flow device onto selected other engine components.
Claim 2
Dependent Claim
142 words
An auxiliary air system contained within the engine nacelle between the engine core and the engine cowling of a gas turbine engine and comprising: (a) an air ducting pipe having one end communicating with an aperture in an external surface of said engine cowling, said aperture lying in a plane generally parallel to the airstream adjacent said aperture; (b) at least one environmental sensor arranged to sense the condition of air within said pipe; (c) a structure to be cooled connected to the other end of said air ducting pipe; (d) an air flow device in communication with said structure to be cooled and effective to move air from the exterior of said cowling through said structure to be cooled, and to said air flow device; and (e) means for directing air from said air flow device onto selected other engine components.
Claim 3
Dependent Claim
29 words
An auxiliary air system according to claim 1, wherein said means for directing air from said air flow device onto selected other engine components comprises a second ducting pipe.
Claim 4
Dependent Claim
147 words
An auxiliary air system contained within the engine nacelle between the fan cowl and the fan casing of a turbofan engine comprising: (a) an air ducting pipe having one end communicating with an aperture in a surface of the engine cowling, said aperture lying in a plane generally parallel to the airstream adjacent said aperture; (b) at least one environmental sensor arranged to sense the condition of air within said pipe; (c) a structure to be cooled including a heat transfer chamber therein connected to the other end of said air ducting pipe; (d) an air flow device in communication with said heat transfer chamber and effective to move air from the exterior of said cowling, through said structure to be cooled, and to said air flow device; and (e) a second ducting pipe for directing air from said air flow device onto selected other engine components.
Claim 5
Dependent Claim
147 words
An auxiliary air system contained within the engine nacelle between the fan cowl and the fan casing of a turbofan engine comprising: (a) an air ducting pipe having one end communicating with an aperture in a surface of the engine cowling, said aperture lying in a plane generally parallel to the airstream adjacent said aperture; (b) at least one environmental sensor arranged to sense the condition of air within said pipe; (c) a structure to be cooled including a heat transfer chamber therein connected to the other end of said air ducting pipe; (d) an air flow device in communication with said heat transfer chamber and effective to move air from the exterior of said cowling, through said structure to be cooled, and to said air flow device; and (e) a second ducting pipe for directing air from said air flow device onto selected other engine components.
Claim 6
Dependent Claim
64 words
An auxiliary air system according to claim 3 wherein the portion of said engine cowling in which said aperture is disposed is positionable relative to said air ducting pipe and wherein the end of said air ducting pipe communicating with said aperture includes a flexible seal for, in at least one position of said engine cowling, aligning said air ducting pipe with said aperture.
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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) | 1985-09-27 | 1986-03-29 | 1986-09-28 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1989-09-27 | 1990-03-29 | 1990-09-28 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1993-09-27 | 1994-03-29 | 1994-09-28 | $7700.00 | Window Closed / Lapsed |