GB1591994A - Supersonic air intake diffuser for air-breathing propulsion units - Google Patents

Supersonic air intake diffuser for air-breathing propulsion units Download PDF

Info

Publication number
GB1591994A
GB1591994A GB4645477A GB4645477A GB1591994A GB 1591994 A GB1591994 A GB 1591994A GB 4645477 A GB4645477 A GB 4645477A GB 4645477 A GB4645477 A GB 4645477A GB 1591994 A GB1591994 A GB 1591994A
Authority
GB
United Kingdom
Prior art keywords
diffuser
component
central body
chamber
brake
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
GB4645477A
Other languages
English (en)
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of GB1591994A publication Critical patent/GB1591994A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/042Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Aeration Devices For Treatment Of Activated Polluted Sludge (AREA)
GB4645477A 1976-11-16 1977-11-08 Supersonic air intake diffuser for air-breathing propulsion units Expired GB1591994A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19762652114 DE2652114A1 (de) 1976-11-16 1976-11-16 Ueberschalleinlaufdiffusor fuer ein luftatmendes flugtriebwerk, insbesondere staustrahltriebwerk

Publications (1)

Publication Number Publication Date
GB1591994A true GB1591994A (en) 1981-07-01

Family

ID=5993247

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4645477A Expired GB1591994A (en) 1976-11-16 1977-11-08 Supersonic air intake diffuser for air-breathing propulsion units

Country Status (3)

Country Link
DE (1) DE2652114A1 (enExample)
FR (1) FR2370865A1 (enExample)
GB (1) GB1591994A (enExample)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3011796C2 (de) * 1980-03-27 1982-11-11 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Überschall-Lufteinlauf für Strahltriebwerke, insbesondere für Staustrahltriebwerke zum Antrieb von Flugkörpern
DE3912392A1 (de) * 1989-04-14 1990-10-25 Mtu Muenchen Gmbh Turbinen-staustrahltriebwerk

Also Published As

Publication number Publication date
FR2370865A1 (fr) 1978-06-09
FR2370865B3 (enExample) 1980-08-14
DE2652114A1 (de) 1978-05-18

Similar Documents

Publication Publication Date Title
US8371104B2 (en) System and apparatus for vectoring nozzle exhaust plume from a nozzle
US3240200A (en) Sonobuoy launcher
US2411895A (en) Nozzle control
US3265331A (en) Supersonic inlet
US4291782A (en) Simplified method and apparatus for hot-shield jet noise suppression
US4093122A (en) Integrated divergent exhaust nozzle thrust reverser
US3380660A (en) Variable area exhaust deflector
US2831321A (en) Variable area exhaust nozzle
US2799990A (en) Supersonic jet deflection device
US5671722A (en) Projectile launcher
US3208383A (en) Ramjet vent
GB1591994A (en) Supersonic air intake diffuser for air-breathing propulsion units
US10378477B2 (en) Nozzle for jet engines
GB1272836A (en) Gas turbine engines
US12129795B2 (en) Air inlet duct for a nacelle of an aircraft propulsion assembly
US3678692A (en) Pulsation power unit
US2798743A (en) Flexible coupling device for connecting jet-engine-powered aircraft to ground mounted silencers
WO2021167667A3 (en) Aircraft engine nacelle cowling mechanism
US5148673A (en) Integrated turboramjet engine
US2841955A (en) Directional control for jets
GB878400A (en) Improvements in or relating to supersonic aircraft
US3354645A (en) Method and apparatus for producing a non-axial thrust vector
GB1117266A (en) Supersonic intake for a jet propulsion engine
US3086357A (en) Supersonic flow control device
US3837577A (en) Minimum drag variable area exhaust nozzle

Legal Events

Date Code Title Description
CSNS Application of which complete specification have been accepted and published, but patent is not sealed