GB1165360A - Improvements relating to Aircraft Engine Vortex Inhibitors - Google Patents

Improvements relating to Aircraft Engine Vortex Inhibitors

Info

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
Application number
GB5828366A
Inventor
Ivor Macaulay Davidson
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
MINI OF TECHNOLOGY LONDON
Original Assignee
MINI OF TECHNOLOGY LONDON
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by MINI OF TECHNOLOGY LONDON filed Critical MINI OF TECHNOLOGY LONDON
Priority to GB5828366A priority Critical patent/GB1165360A/en
Publication of GB1165360A publication Critical patent/GB1165360A/en
Expired legal-status Critical Current

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.
GB5828366A 1966-12-30 1966-12-30 Improvements relating to Aircraft Engine Vortex Inhibitors Expired GB1165360A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (2)

* Cited by examiner, † Cited by third party
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