GB890547A - Improvements in variable throat supersonic diffuser - Google Patents

Improvements in variable throat supersonic diffuser

Info

Publication number
GB890547A
GB890547A GB1310460A GB1310460A GB890547A GB 890547 A GB890547 A GB 890547A GB 1310460 A GB1310460 A GB 1310460A GB 1310460 A GB1310460 A GB 1310460A GB 890547 A GB890547 A GB 890547A
Authority
GB
United Kingdom
Prior art keywords
supersonic diffuser
variable throat
boundary layer
supersonic
throat
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
GB1310460A
Inventor
Ivan Hans Edelfelt
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.)
General Electric Co
Original Assignee
General Electric Co
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
Priority to US55325155 priority Critical patent/US3011307A/en
Application filed by General Electric Co filed Critical General Electric Co
Priority to GB1310460A priority patent/GB890547A/en
Publication of GB890547A publication Critical patent/GB890547A/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
    • F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry

Abstract

890,547. Boundary layer control. GENERAL ELECTRIC CO. April 12, 1960, No. 13104/60. Class 4. [Also in Group XXVI] A supersonic diffuser inlet for a jet propulsion engine having a pivoted flap 20 whereby the throat area 28 may be varied, has a duct 18 through which the boundary layer may be bled from the passage 15.
GB1310460A 1955-12-15 1960-04-12 Improvements in variable throat supersonic diffuser Expired GB890547A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US55325155 US3011307A (en) 1955-12-15 1955-12-15 Variable throat supersonic diffuser
GB1310460A GB890547A (en) 1960-04-12 1960-04-12 Improvements in variable throat supersonic diffuser

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1310460A GB890547A (en) 1960-04-12 1960-04-12 Improvements in variable throat supersonic diffuser

Publications (1)

Publication Number Publication Date
GB890547A true GB890547A (en) 1962-03-07

Family

ID=10016906

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1310460A Expired GB890547A (en) 1955-12-15 1960-04-12 Improvements in variable throat supersonic diffuser

Country Status (1)

Country Link
GB (1) GB890547A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2148809A (en) * 1978-03-14 1985-06-05 Rolls Royce Self-propelled missile
GB2192940A (en) * 1986-07-25 1988-01-27 Rolls Royce Plc Aircraft gas turbine engine air intake
GB2192941A (en) * 1986-07-25 1988-01-27 Rolls Royce Plc Aircraft gas turbine engine air intake
DE3627910A1 (en) * 1986-08-16 1988-02-18 Messerschmitt Boelkow Blohm Aircraft having devices which are arranged in a separate equipment bay and are to be cooled

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2148809A (en) * 1978-03-14 1985-06-05 Rolls Royce Self-propelled missile
GB2192940A (en) * 1986-07-25 1988-01-27 Rolls Royce Plc Aircraft gas turbine engine air intake
GB2192941A (en) * 1986-07-25 1988-01-27 Rolls Royce Plc Aircraft gas turbine engine air intake
US4782657A (en) * 1986-07-25 1988-11-08 Rolls-Royce Plc Variable area aircraft air intake
US4782659A (en) * 1986-07-25 1988-11-08 Rolls-Royce Plc Variable area aircraft air intake
GB2192941B (en) * 1986-07-25 1990-10-03 Rolls Royce Plc A variable area aircraft air intake
GB2192940B (en) * 1986-07-25 1990-10-31 Rolls Royce Plc A variable area aircraft air intake
DE3627910A1 (en) * 1986-08-16 1988-02-18 Messerschmitt Boelkow Blohm Aircraft having devices which are arranged in a separate equipment bay and are to be cooled

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