FR2174672A1 - - Google Patents

Info

Publication number
FR2174672A1
FR2174672A1 FR7207726A FR7207726A FR2174672A1 FR 2174672 A1 FR2174672 A1 FR 2174672A1 FR 7207726 A FR7207726 A FR 7207726A FR 7207726 A FR7207726 A FR 7207726A FR 2174672 A1 FR2174672 A1 FR 2174672A1
Authority
FR
France
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.)
Granted
Application number
FR7207726A
Other languages
French (fr)
Other versions
FR2174672B1 (cs
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
Priority to FR7207726A priority Critical patent/FR2174672B1/fr
Priority to GB1000273A priority patent/GB1416464A/en
Priority to DE2310921A priority patent/DE2310921C3/de
Publication of FR2174672A1 publication Critical patent/FR2174672A1/fr
Priority to US05/528,480 priority patent/US3941313A/en
Application granted granted Critical
Publication of FR2174672B1 publication Critical patent/FR2174672B1/fr
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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Turbines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR7207726A 1972-03-06 1972-03-06 Expired FR2174672B1 (cs)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR7207726A FR2174672B1 (cs) 1972-03-06 1972-03-06
GB1000273A GB1416464A (en) 1972-03-06 1973-03-01 Jet propulsion engines
DE2310921A DE2310921C3 (de) 1972-03-06 1973-03-05 Schubumkehrvorrichtung, insbesondere für ein Luftfahrzeug, das mittels eines Strahltriebwerks angetrieben wird
US05/528,480 US3941313A (en) 1972-03-06 1974-11-29 Jet engine nacelle with drag augmenter auxiliary for thrust-reverser system

Applications Claiming Priority (1)

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

Publications (2)

Publication Number Publication Date
FR2174672A1 true FR2174672A1 (cs) 1973-10-19
FR2174672B1 FR2174672B1 (cs) 1975-06-13

Family

ID=9094694

Family Applications (1)

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

Country Status (3)

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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2327411A1 (fr) * 1975-10-11 1977-05-06 Rolls Royce Perfectionnements aux inverseurs de poussee pour turboreacteurs a soufflante canalisee
EP0455559A1 (fr) * 1990-05-03 1991-11-06 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Dispositif d'alimentation en comburant d'une turbine à gaz

Families Citing this family (3)

* 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
GB9425403D0 (en) * 1994-12-14 1995-02-15 Short Brothers Plc Aircraft propulsive power unit
FR3116043B1 (fr) * 2020-11-09 2023-04-28 Safran Aircraft Engines Entrée d’air de nacelle d’ensemble propulsif d’aéronef pour favoriser une phase d’inversion de poussée

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
NEANT *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2327411A1 (fr) * 1975-10-11 1977-05-06 Rolls Royce Perfectionnements aux inverseurs de poussee pour turboreacteurs a soufflante canalisee
EP0455559A1 (fr) * 1990-05-03 1991-11-06 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Dispositif d'alimentation en comburant d'une turbine à gaz
FR2661714A1 (fr) * 1990-05-03 1991-11-08 Snecma Dispositif d'alimentation en comburant d'une turbine a gaz.

Also Published As

Publication number Publication date
DE2310921B2 (de) 1978-11-23
DE2310921A1 (de) 1973-09-20
FR2174672B1 (cs) 1975-06-13
DE2310921C3 (de) 1979-07-19
GB1416464A (en) 1975-12-03

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Legal Events

Date Code Title Description
ST Notification of lapse