GB1416464A - Jet propulsion engines - Google Patents

Jet propulsion engines

Info

Publication number
GB1416464A
GB1416464A GB1000273A GB1000273A GB1416464A GB 1416464 A GB1416464 A GB 1416464A GB 1000273 A GB1000273 A GB 1000273A GB 1000273 A GB1000273 A GB 1000273A GB 1416464 A GB1416464 A GB 1416464A
Authority
GB
United Kingdom
Prior art keywords
thrust
thrust reversal
zones
slots
reversal
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
GB1000273A
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Publication of GB1416464A publication Critical patent/GB1416464A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/42—Arrangement or adaptation of brakes
    • B64C25/423—Braking devices acting by reaction of gaseous medium
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB1000273A 1972-03-06 1973-03-01 Jet propulsion engines Expired GB1416464A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7207726A FR2174672B1 (de) 1972-03-06 1972-03-06

Publications (1)

Publication Number Publication Date
GB1416464A true GB1416464A (en) 1975-12-03

Family

ID=9094694

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1000273A Expired GB1416464A (en) 1972-03-06 1973-03-01 Jet propulsion engines

Country Status (3)

Country Link
DE (1) DE2310921C3 (de)
FR (1) FR2174672B1 (de)
GB (1) GB1416464A (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2117720A (en) * 1981-02-28 1983-10-19 Rolls Royce Gas turbine engine having a thrust spoiler
GB2295994A (en) * 1994-12-14 1996-06-19 Short Brothers Plc Drag device for engine nacelle

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1506588A (en) * 1975-10-11 1978-04-05 Rolls Royce Gas turbine engine power plants for aircraft
FR2661714B1 (fr) * 1990-05-03 1994-06-17 Snecma Dispositif d'alimentation en comburant d'une turbine a gaz.

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2117720A (en) * 1981-02-28 1983-10-19 Rolls Royce Gas turbine engine having a thrust spoiler
GB2295994A (en) * 1994-12-14 1996-06-19 Short Brothers Plc Drag device for engine nacelle
US5730393A (en) * 1994-12-14 1998-03-24 Short Brothers Plc Aircraft propulsive power unit
GB2295994B (en) * 1994-12-14 1998-10-14 Short Brothers Plc Aircraft propulsive power unit

Also Published As

Publication number Publication date
DE2310921A1 (de) 1973-09-20
DE2310921C3 (de) 1979-07-19
DE2310921B2 (de) 1978-11-23
FR2174672B1 (de) 1975-06-13
FR2174672A1 (de) 1973-10-19

Similar Documents

Publication Publication Date Title
GB1418905A (en) Gas turbine engines
GB1069033A (en) Improvements in or relating to gas turbine jet propulsion engines
GB1529886A (en) Aerofoil tip-vortex control
GB1328993A (en) Air intakes for gas turbine engines
GB1104764A (en) Improvements in thrust reverters for jet propulsion powerplants
GB907288A (en) Fluid intake for supersonic flow
GB1085619A (en) Gas turbine engine
GB1130268A (en) Improvements in or relating to gas turbine by-pass engines
GB1338892A (en) Silencer or muffler for the composite nozzle of an aircraft jet engine
FR2076030B1 (de)
GB1316029A (en) Turbofan engine thrust reversers
GB955518A (en) Thrust-reversal in turbo-jet devices
GB1270434A (en) Turbofan engines
GB1111219A (en) Gas turbine engine
GB1192548A (en) Air-Cushion Vehicles
GB1330904A (en) Gas turbine jet propulsion engines
GB1182687A (en) Improvements in or relating to Multiflow Jet Propulsion Engines
GB1138679A (en) Wall element for combustion chambers
GB1307867A (en) Device for attenuating noise emitted by the jet of a jet engine
GB1416464A (en) Jet propulsion engines
GB1139005A (en) Improvements in or relating to gas turbine by-pass engines
GB1321657A (en) Ducted fan gas turbine jet propulsion engine
GB1166396A (en) Improvements in Power Plant with Thrust Reverser.
US4183211A (en) Propulsion system for supersonic aircraft
GB1055607A (en) Supersonic intake for a jet engine

Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee