FR2601077B1 - Structure d'ejection des gaz pour moteur a reaction notamment pour reacteur a double flux. - Google Patents

Structure d'ejection des gaz pour moteur a reaction notamment pour reacteur a double flux.

Info

Publication number
FR2601077B1
FR2601077B1 FR8609838A FR8609838A FR2601077B1 FR 2601077 B1 FR2601077 B1 FR 2601077B1 FR 8609838 A FR8609838 A FR 8609838A FR 8609838 A FR8609838 A FR 8609838A FR 2601077 B1 FR2601077 B1 FR 2601077B1
Authority
FR
France
Prior art keywords
flow reactor
gas ejection
double flow
ejection structure
reaction engine
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
FR8609838A
Other languages
English (en)
Other versions
FR2601077A1 (fr
Inventor
John Francis Kennedy
Alain Fournier
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.)
Societe de Construction des Avions Hurel Dubois
Original Assignee
Societe de Construction des Avions Hurel Dubois
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 Societe de Construction des Avions Hurel Dubois filed Critical Societe de Construction des Avions Hurel Dubois
Priority to FR8609838A priority Critical patent/FR2601077B1/fr
Publication of FR2601077A1 publication Critical patent/FR2601077A1/fr
Application granted granted Critical
Publication of FR2601077B1 publication Critical patent/FR2601077B1/fr
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers
    • 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
FR8609838A 1986-07-07 1986-07-07 Structure d'ejection des gaz pour moteur a reaction notamment pour reacteur a double flux. Expired FR2601077B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR8609838A FR2601077B1 (fr) 1986-07-07 1986-07-07 Structure d'ejection des gaz pour moteur a reaction notamment pour reacteur a double flux.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8609838A FR2601077B1 (fr) 1986-07-07 1986-07-07 Structure d'ejection des gaz pour moteur a reaction notamment pour reacteur a double flux.

Publications (2)

Publication Number Publication Date
FR2601077A1 FR2601077A1 (fr) 1988-01-08
FR2601077B1 true FR2601077B1 (fr) 1988-10-21

Family

ID=9337142

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8609838A Expired FR2601077B1 (fr) 1986-07-07 1986-07-07 Structure d'ejection des gaz pour moteur a reaction notamment pour reacteur a double flux.

Country Status (1)

Country Link
FR (1) FR2601077B1 (fr)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7735778B2 (en) 2007-11-16 2010-06-15 Pratt & Whitney Canada Corp. Pivoting fairings for a thrust reverser
US8015797B2 (en) 2006-09-21 2011-09-13 Jean-Pierre Lair Thrust reverser nozzle for a turbofan gas turbine engine
US8052085B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser for a turbofan gas turbine engine
US8052086B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser door
US8051639B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser
US8091827B2 (en) 2007-11-16 2012-01-10 The Nordam Group, Inc. Thrust reverser door
US8127530B2 (en) 2008-06-19 2012-03-06 The Nordam Group, Inc. Thrust reverser for a turbofan gas turbine engine
US8172175B2 (en) 2007-11-16 2012-05-08 The Nordam Group, Inc. Pivoting door thrust reverser for a turbofan gas turbine engine

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2638783B1 (fr) * 1988-11-10 1991-04-05 Astech Inverseur de poussee notamment pour moteur a reaction d'aeronef
US5176340A (en) * 1991-11-26 1993-01-05 Lair Jean Pierre Thrust reverser with a planar exit opening
FR2727468B1 (fr) 1994-11-30 1996-12-27 Hispano Suiza Sa Inverseur de poussee de turboreacteur a obstacles aval
FR2736390B1 (fr) * 1995-07-05 1997-08-08 Hispano Suiza Sa Inverseur de poussee de turboreacteur a une coquille
DE69514224T2 (de) 1995-09-13 2000-08-10 Hurel Dubois Avions Elektrohydraulische Schubumkehrvorrichtung mit zwei Klappen
FR2741114B1 (fr) * 1995-11-15 1997-12-05 Hispano Suiza Sa Inverseur de poussee de turboreacteur a obstacles aval tendant a l'equilibrage
DE69616739T2 (de) * 1996-02-08 2002-09-05 Hurel Dubois Avions Dichtungsanordnung für schwenkbare Schubumkehrklappe
FR2764000B1 (fr) 1997-06-03 1999-08-13 Hurel Dubois Avions Structure d'ejection equipee d'un inverseur de poussee a deux portes arriere et a section de sortie plane
FR2768773B1 (fr) * 1997-09-25 1999-11-05 Hispano Suiza Sa Inverseur de poussee de turboreacteur a coquilles internes
FR2811716B1 (fr) 2000-07-17 2002-10-04 Hurel Dubois Avions Perfectionnements aux arriere-corps de nacelle, a tuyere commune, de reacteur d'avion
US6938408B2 (en) 2001-04-26 2005-09-06 Propulsion Vectoring, L.P. Thrust vectoring and variable exhaust area for jet engine nozzle
US6487845B1 (en) 2001-06-08 2002-12-03 The Nordam Group, Inc. Pivot fairing thrust reverser
US8091335B2 (en) * 2008-02-14 2012-01-10 Spirit Aerosystems, Inc. Swept fan ramp for pivot door thrust reverser

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2680948A (en) * 1948-08-30 1954-06-15 Engineering & Res Corp Variable area tail pipe for jet engines
US2847823A (en) * 1955-03-15 1958-08-19 Curtiss Wright Corp Reverse thrust nozzle construction
FR1482538A (fr) * 1965-06-07 1967-05-26 Gen Electric Inverseur de poussée
GB1227044A (fr) * 1969-04-02 1971-03-31
US3647141A (en) * 1970-06-01 1972-03-07 Rohr Corp Thrust controlling apparatus
US4183478A (en) * 1977-11-25 1980-01-15 The Boeing Company Jet thrust reverser
FR2506843B1 (fr) * 1981-05-29 1987-04-24 Hurel Dubois Avions Dispositif d'inversion de poussee pour turboreacteur d'avion

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8015797B2 (en) 2006-09-21 2011-09-13 Jean-Pierre Lair Thrust reverser nozzle for a turbofan gas turbine engine
US7735778B2 (en) 2007-11-16 2010-06-15 Pratt & Whitney Canada Corp. Pivoting fairings for a thrust reverser
US8052085B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser for a turbofan gas turbine engine
US8052086B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser door
US8051639B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser
US8091827B2 (en) 2007-11-16 2012-01-10 The Nordam Group, Inc. Thrust reverser door
US8172175B2 (en) 2007-11-16 2012-05-08 The Nordam Group, Inc. Pivoting door thrust reverser for a turbofan gas turbine engine
US8127530B2 (en) 2008-06-19 2012-03-06 The Nordam Group, Inc. Thrust reverser for a turbofan gas turbine engine

Also Published As

Publication number Publication date
FR2601077A1 (fr) 1988-01-08

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