← Back to Patent Explorer
US4292802A Expired / Lapsed US ⏱️ 0.0 years remaining

Method and apparatus for increasing compressor inlet pressure

Assignee: General Electric Co
•
Filing: 1978-12-27
•
Granted: 1981-10-06
•
Expires: 1998-12-27
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract A plurality of blocker door vanes are disposed in the bypass duct to selectively close off the bypass flow and increase the flow and pressure of the air flowing into the compressor. In this way, the compressor inlet pressure can be increased sufficiently to allow air starts without starter torque assist. The vanes may also be closed down during ground idle to reduce the thrust and increase the compressor bleed pressure and both the pressure and the temperature of the air to the combustor. Provision is made for the controlling of the blocker door vanes as a function of core speed.

Inventors

  • 👤 Barton H. Snow

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-06 02:44
CPC Classifications
F; F02; F02K; F02K3/00; F02K3/02; F02K3/04; F02K3/075; Y; Y02; Y02T; Y02T50/00; Y02T50/60

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 54 words
A method of facilitating air starts in a turbofan engine of the type having a core, a fan, and a bypass duct, comprising the steps of: (a) blocking the flow of air in the bypass duct; and (b) increasing the inlet pressure to the compressor to a level which will allow an air start.
Claim 2
Independent Claim 54 words
A method of facilitating air starts in a turbofan engine of the type having a core, a fan, and a bypass duct, comprising the steps of: (a) blocking the flow of air in the bypass duct; and (b) increasing the inlet pressure to the compressor to a level which will allow an air start.
Claim 3
Dependent Claim 27 words
A method, as set forth in claim 1, wherein the step of blocking is accomplished by closing a plurality of circumferentially spaced vanes in the bypass duct.
Claim 4
Dependent Claim 18 words
A method, as set forth in claim 1, wherein substantially all airflow in the bypass duct is blocked.
Claim 5
Dependent Claim 16 words
A method, as set forth in claim 1, and including the step of starting the engine.
Claim 6
Dependent Claim 27 words
A method, as set forth in claim 4, and including the step of opening the bypass duct to the flow of air after the engine is started.

References Cited (Backward Citations)

US2873576A Cited
US3060680A Cited
US3514952A Cited
US3472027A Cited
US3908362A Cited
US3779665A Cited
US4080785A Cited
US4043121A Cited
US4069661A Cited
US4175384A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1984-10-05 1985-04-06 1985-10-06 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1988-10-05 1989-04-06 1989-10-06 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1992-10-05 1993-04-06 1993-10-06 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag