GB1165360A - Improvements relating to Aircraft Engine Vortex Inhibitors - Google Patents
Improvements relating to Aircraft Engine Vortex InhibitorsInfo
- Publication number
- GB1165360A GB1165360A GB5828366A GB5828366A GB1165360A GB 1165360 A GB1165360 A GB 1165360A GB 5828366 A GB5828366 A GB 5828366A GB 5828366 A GB5828366 A GB 5828366A GB 1165360 A GB1165360 A GB 1165360A
- Authority
- GB
- United Kingdom
- Prior art keywords
- vortex
- inhibitors
- aircraft engine
- tube
- improvements relating
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/05—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
1,165,360. Boundary layer control. MINISTER OF TECHNOLOGY. 29 Nov., 1967 [30 Dec., 1966], No. 58283/66. Heading F2R. [Also in Division F1] To reduce the risk of ingesting debris from a ground surface 6 drawn upwardly by a vortex 5 into the air intake of a gas turbine engine mounted by a pylon 3 on an aircraft wing 2 provision is made to prevent the formation of the vortex by mounting on the lower face of the engine casing a tube 7, which is axially slotted at 8, 9, 10 and 11 so that air tapped from the compressor 12 and delivered through a conduit 13 will generate circulation round the tube to entrain the vortex, Two side.byside vortex inhibitors may be provided and arrangements are described for retracting the tubes into the engine casing.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5828366A GB1165360A (en) | 1966-12-30 | 1966-12-30 | Improvements relating to Aircraft Engine Vortex Inhibitors |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5828366A GB1165360A (en) | 1966-12-30 | 1966-12-30 | Improvements relating to Aircraft Engine Vortex Inhibitors |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1165360A true GB1165360A (en) | 1969-09-24 |
Family
ID=10481225
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5828366A Expired GB1165360A (en) | 1966-12-30 | 1966-12-30 | Improvements relating to Aircraft Engine Vortex Inhibitors |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1165360A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2350464A1 (en) * | 1976-05-03 | 1977-12-02 | Gen Electric | METHOD OF LIMITING THE INGESTION OF SOIL DEBRIS BY A GAS TURBINE ENGINE |
EP1413721A3 (en) * | 2002-10-25 | 2006-08-09 | The Boeing Company | Air inlet for an aircraft jet engine with an active system for the suppression of a ground vortex |
-
1966
- 1966-12-30 GB GB5828366A patent/GB1165360A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2350464A1 (en) * | 1976-05-03 | 1977-12-02 | Gen Electric | METHOD OF LIMITING THE INGESTION OF SOIL DEBRIS BY A GAS TURBINE ENGINE |
EP1413721A3 (en) * | 2002-10-25 | 2006-08-09 | The Boeing Company | Air inlet for an aircraft jet engine with an active system for the suppression of a ground vortex |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PLNP | Patent lapsed through nonpayment of renewal fees |