FR2410142A1 - Inverseur de poussee a portes en coquille de peigne et a ailettes en cascade - Google Patents

Inverseur de poussee a portes en coquille de peigne et a ailettes en cascade

Info

Publication number
FR2410142A1
FR2410142A1 FR7815823A FR7815823A FR2410142A1 FR 2410142 A1 FR2410142 A1 FR 2410142A1 FR 7815823 A FR7815823 A FR 7815823A FR 7815823 A FR7815823 A FR 7815823A FR 2410142 A1 FR2410142 A1 FR 2410142A1
Authority
FR
France
Prior art keywords
cascade
fins
door
slides
thrust inverter
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.)
Granted
Application number
FR7815823A
Other languages
English (en)
French (fr)
Other versions
FR2410142B3 (US20100056889A1-20100304-C00004.png
Inventor
Peter Klaus Christoph Rudolph
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.)
Boeing Co
Original Assignee
Boeing 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
Application filed by Boeing Co filed Critical Boeing Co
Publication of FR2410142A1 publication Critical patent/FR2410142A1/fr
Application granted granted Critical
Publication of FR2410142B3 publication Critical patent/FR2410142B3/fr
Granted 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Component Parts Of Construction Machinery (AREA)
  • Power-Operated Mechanisms For Wings (AREA)
FR7815823A 1977-11-25 1978-05-26 Inverseur de poussee a portes en coquille de peigne et a ailettes en cascade Granted FR2410142A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/854,554 US4183478A (en) 1977-11-25 1977-11-25 Jet thrust reverser

Publications (2)

Publication Number Publication Date
FR2410142A1 true FR2410142A1 (fr) 1979-06-22
FR2410142B3 FR2410142B3 (US20100056889A1-20100304-C00004.png) 1981-02-13

Family

ID=25319019

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7815823A Granted FR2410142A1 (fr) 1977-11-25 1978-05-26 Inverseur de poussee a portes en coquille de peigne et a ailettes en cascade

Country Status (6)

Country Link
US (1) US4183478A (US20100056889A1-20100304-C00004.png)
JP (1) JPS5475799A (US20100056889A1-20100304-C00004.png)
DE (1) DE2823206A1 (US20100056889A1-20100304-C00004.png)
FR (1) FR2410142A1 (US20100056889A1-20100304-C00004.png)
GB (1) GB1570680A (US20100056889A1-20100304-C00004.png)
IT (1) IT1104826B (US20100056889A1-20100304-C00004.png)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2481748A1 (fr) * 1980-04-30 1981-11-06 Rolls Royce Deflecteur de poussee pour moteur d'aviation
FR2601077A1 (fr) * 1986-07-07 1988-01-08 Hurel Dubois Avions Structure d'ejection des gaz pour moteur a reaction notamment pour reacteur a double flux.

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4753392A (en) * 1984-11-02 1988-06-28 United Technologies Corporation Two dimensional gas turbine engine exhaust nozzle
US4790495A (en) * 1984-12-06 1988-12-13 Grumman Aerospace Corporation Cascade thrust reverser
US4760960A (en) * 1987-05-22 1988-08-02 United Technologies Corporation Linkage for area controlled, thrust vectoring vane cascade
US4828173A (en) * 1987-05-22 1989-05-09 United Technologies Corporation Area controlled, thrust vectoring vane cascade
US4798328A (en) * 1987-05-22 1989-01-17 United Technologies Corporation Area controlled, thrust vectoring vane cascade with nutating control vane
US4922711A (en) * 1988-06-10 1990-05-08 The Boeing Company Thrust reversing system for high bypass fan engines
US5197694A (en) * 1990-04-27 1993-03-30 General Electric Company Overwing thrust reverser
US5058828A (en) * 1990-07-30 1991-10-22 General Electric Company Overwing thrust reverser
FR2712929B1 (fr) * 1993-11-24 1995-12-29 Hispano Suiza Sa Inverseur de poussée de turboréacteur à double flux.
US5987880A (en) * 1997-07-08 1999-11-23 Mcdonnell Douglas Corporation Supersonic engine, multi-port thrust reversing system
FR2768773B1 (fr) * 1997-09-25 1999-11-05 Hispano Suiza Sa Inverseur de poussee de turboreacteur a coquilles internes
US7124981B2 (en) 2003-03-04 2006-10-24 The Boeing Company Thrust reverser utilizing integrated structural bypass duct
GB0608985D0 (en) * 2006-05-06 2006-06-14 Rolls Royce Plc Aeroengine thrust reverser
US8201390B2 (en) * 2007-12-12 2012-06-19 Spirit Aerosystems, Inc. Partial cascade thrust reverser
US8959889B2 (en) 2008-11-26 2015-02-24 The Boeing Company Method of varying a fan duct nozzle throat area of a gas turbine engine
US8127532B2 (en) * 2008-11-26 2012-03-06 The Boeing Company Pivoting fan nozzle nacelle
US10006404B2 (en) * 2012-02-28 2018-06-26 United Technologies Corporation Gas turbine engine thrust reverser system
US10221809B2 (en) 2013-08-28 2019-03-05 United Technologies Corporation Thrust reverser sliding door assembly
RU2570743C2 (ru) * 2014-04-17 2015-12-10 Открытое Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" Способ управления летательным аппаратом, снабженным двигательной установкой с реактивными соплами
RU2570745C2 (ru) * 2014-04-17 2015-12-10 Открытое Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" Способ управления летательным аппаратом, снабженным двигательной установкой с реактивными соплами
US9895840B2 (en) 2014-05-15 2018-02-20 The Boeing Company Thermoformed cascades for jet engine thrust reversers
US9874176B2 (en) 2015-01-14 2018-01-23 The Boeing Company Methods and apparatus to vary reverse thrust of aircraft engines
US10018151B2 (en) * 2015-01-14 2018-07-10 The Boeing Company Methods and apparatus to vary reverse thrust of aircraft engines
US20160305370A1 (en) * 2015-04-16 2016-10-20 Honeywell International Inc. Translating cowl thrust reverser with door pivots aft of reverse flow path
US20170009704A1 (en) * 2015-07-06 2017-01-12 Rohr, Inc. Thrust reverser staggered translating sleeve
US20170058829A1 (en) * 2015-08-26 2017-03-02 Rohr, Inc. Low forward-turning casacde with high-forward-turning aft vane passages
US20170058828A1 (en) * 2015-08-26 2017-03-02 Rohr, Inc. Cascade with varying vane trailing edge thickness
US10648426B2 (en) 2016-01-14 2020-05-12 Honeywell International Inc. Single row vane assembly for a thrust reverser
US10451002B2 (en) 2016-01-22 2019-10-22 Honeywell International Inc. Translating cowl thrust reverser that prevents unintended door rotation
US10337454B2 (en) 2016-01-25 2019-07-02 Honeywell International Inc. Thrust reverser with asymmetric vane geometry
US10359051B2 (en) 2016-01-26 2019-07-23 Honeywell International Inc. Impeller shroud supports having mid-impeller bleed flow passages and gas turbine engines including the same
US10563614B2 (en) 2016-08-17 2020-02-18 Honeywell International Inc. Composite translating cowl assembly for a thrust reverser system
US10823112B2 (en) 2017-05-25 2020-11-03 The Boeing Company Method for manufacturing and assembly of a thrust reverser cascade
US11078871B2 (en) 2018-12-21 2021-08-03 Rohr, Inc. Thrust reverser system with cascades
US11491686B2 (en) 2019-07-22 2022-11-08 The Boeing Company Compression molded cascades with two piece mold

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2932164A (en) * 1955-08-03 1960-04-12 Lockheed Aircraft Corp Thrust reverser and control mechanism therefor
US3024604A (en) * 1958-03-31 1962-03-13 Rolls Royce Aircraft jet propulsion apparatus with thrust reversing means
GB913699A (US20100056889A1-20100304-C00004.png) * 1959-12-18
US3035411A (en) * 1960-02-26 1962-05-22 Gen Electric Thrust reverser actuating mechanism
FR1259348A (fr) * 1960-06-15 1961-04-21 Rolls Royce Perfectionnements aux moteurs à turbine à gaz
GB933612A (en) * 1961-02-13 1963-08-08 Rolls Royce Jet engine thrust reversers
GB978462A (en) * 1963-10-28 1964-12-23 Rolls Royce Gas turbine by-pass engine
GB1227044A (US20100056889A1-20100304-C00004.png) * 1969-04-02 1971-03-31
US3612399A (en) * 1969-12-05 1971-10-12 Rolls Royce Variable directionally silenced nozzle
US3791586A (en) * 1972-12-26 1974-02-12 Boeing Co Combination clamshell thrust reverser & variable nozzle area ramp
US3907224A (en) * 1973-06-01 1975-09-23 Boeing Co Variable ramp exhaust nozzle and clamshell reverser
US3863867A (en) * 1973-12-26 1975-02-04 Boeing Co Thrust control apparatus for a jet propulsion engine and actuating mechanism therefor
US3915415A (en) * 1974-03-21 1975-10-28 Rohr Industries Inc Overwing thrust reverser
US3981463A (en) * 1974-03-21 1976-09-21 Rohr Industries, Inc. Overwing thrust reverser
US4030291A (en) * 1976-01-02 1977-06-21 General Electric Company Thrust reverser for a gas turbofan engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2481748A1 (fr) * 1980-04-30 1981-11-06 Rolls Royce Deflecteur de poussee pour moteur d'aviation
FR2601077A1 (fr) * 1986-07-07 1988-01-08 Hurel Dubois Avions Structure d'ejection des gaz pour moteur a reaction notamment pour reacteur a double flux.

Also Published As

Publication number Publication date
IT1104826B (it) 1985-10-28
JPS5475799A (en) 1979-06-16
GB1570680A (en) 1980-07-02
FR2410142B3 (US20100056889A1-20100304-C00004.png) 1981-02-13
US4183478A (en) 1980-01-15
DE2823206C2 (US20100056889A1-20100304-C00004.png) 1987-03-05
DE2823206A1 (de) 1979-06-07
IT7849517A0 (it) 1978-05-24

Similar Documents

Publication Publication Date Title
FR2410142A1 (fr) Inverseur de poussee a portes en coquille de peigne et a ailettes en cascade
EP0696985B1 (en) Nacelle arrangement
EP0453360A1 (fr) Moteur d'aviation à trÀ¨s grand taux de dilution et du type dit contrafan avant
EP0756557B1 (en) An aircraft propulsive power unit
US4407120A (en) Thrust reverser geared linkage
US3067579A (en) Gas turbine power plant
US4600396A (en) Cowl latch for outboard motors
GB1516980A (en) Mounting ducted fan gas turbine engines on aircraft
US8951006B2 (en) Nacelle for the jet engine of an aircraft
CN109080836B (zh) 推力反向器系统和涡轮发动机及飞行器
US4129269A (en) Single-skin thrust reverser for aircraft jet engines
GB1304212A (US20100056889A1-20100304-C00004.png)
GB1318748A (en) Gas turgine ducted fan engines for aircraft
EP1462642A1 (en) Thrust reverser utilizing integrated structural bypass duct
EP1026387A3 (en) Contoured thrust reverser blocker doors matching lobed noise suppressor nozzle
RU2162536C2 (ru) Двухконтурный турбореактивный двигатель, связанный с устройством реверсирования тяги с обтекателем, установленным в канале газового потока
GB1130268A (en) Improvements in or relating to gas turbine by-pass engines
FR2926790A1 (fr) Systeme de guidage pour la maintenance d'une nacelle d'aeronef
GB1338892A (en) Silencer or muffler for the composite nozzle of an aircraft jet engine
FR2434273A1 (fr) Systeme de tuyere deployable telescopiquement, a cones emboites, pour un moteur-fusee
GB1316029A (en) Turbofan engine thrust reversers
FR2376301A1 (fr) Engin autopropulse a etages separables
GB1358078A (en) Thrust reverser for ducted fan jet propulsion engines
GB1276265A (en) Improvements in or relating to thrust deflectors for gas turbine ducted fan engines
GB1207907A (en) Controllable air-intake arrangement for a turbo-ramjet unit