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 cascadeInfo
- 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
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)
Abstract
INVERSEUR DE POUSSEE POUR GROUPE PROPULSEUR A REACTION COMPORTANT UNE CARCASSE ANNULAIRE DE MOTEUR ET UN MOTEUR A REACTION ENFERME DANS CETTE CARCASSE, A SON EXTREMITE AVANT. IL COMPREND UNE CASCADE D'AILETTES 20 DANS LA PAROI DE LA CARCASSE, A SON EXTREMITE ARRIERE ET AU-DELA DE LA TUYERE D'ECHAPPEMENT 18 DU MOTEUR 10, UNE PORTE 20 RECOUVRANT NORMALEMENT LA CASCADE, DES GLISSIERES 26, UN COULISSEAU 28 POUVANT ALLER ET VENIR SUR CHACUNE DES GLISSIERES, DES MOYENS 24 DE MONTAGE PIVOTANT DE L'EXTREMITE AVANT DE LA PORTE SUR LES COULISSEAUX RESPECTIFS, DES BRAS 38 QUI SONT MONTES PIVOTANTS DANS LA CARCASSE ET DONT UNE EXTREMITE LIBRE EST MONTEE PIVOTANTE SUR L'EXTREMITE ARRIERE DE LA PORTE, ET DES ORGANES D'ACTIONNEMENT 40 POUR FAIRE TOURNER CES BRAS. AVIONS A DECOLLAGE ET ATTERRISSAGE COURTS.
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 (fr) | 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 (fr) |
JP (1) | JPS5475799A (fr) |
DE (1) | DE2823206A1 (fr) |
FR (1) | FR2410142A1 (fr) |
GB (1) | GB1570680A (fr) |
IT (1) | IT1104826B (fr) |
Cited By (2)
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)
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 |
US4798328A (en) * | 1987-05-22 | 1989-01-17 | United Technologies Corporation | Area controlled, thrust vectoring vane cascade with nutating control vane |
US4828173A (en) * | 1987-05-22 | 1989-05-09 | United Technologies Corporation | Area controlled, thrust vectoring vane cascade |
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 |
EP3039275B1 (fr) | 2013-08-28 | 2020-03-04 | United Technologies Corporation | Ensemble porte coulissante d'inverseur de poussée |
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 |
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 |
US9895840B2 (en) | 2014-05-15 | 2018-02-20 | The Boeing Company | Thermoformed cascades for jet engine thrust reversers |
US10018151B2 (en) * | 2015-01-14 | 2018-07-10 | The Boeing Company | Methods and apparatus to vary reverse thrust of aircraft engines |
US9874176B2 (en) | 2015-01-14 | 2018-01-23 | 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 |
US20170058828A1 (en) * | 2015-08-26 | 2017-03-02 | Rohr, Inc. | Cascade with varying vane trailing edge thickness |
US20170058829A1 (en) * | 2015-08-26 | 2017-03-02 | Rohr, Inc. | Low forward-turning casacde with high-forward-turning aft vane passages |
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)
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 (fr) * | 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 (fr) * | 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 |
US3981463A (en) * | 1974-03-21 | 1976-09-21 | Rohr Industries, Inc. | Overwing thrust reverser |
US3915415A (en) * | 1974-03-21 | 1975-10-28 | Rohr Industries Inc | Overwing thrust reverser |
US4030291A (en) * | 1976-01-02 | 1977-06-21 | General Electric Company | Thrust reverser for a gas turbofan engine |
-
1977
- 1977-11-25 US US05/854,554 patent/US4183478A/en not_active Expired - Lifetime
-
1978
- 1978-05-04 GB GB17804/78A patent/GB1570680A/en not_active Expired
- 1978-05-24 IT IT49517/78A patent/IT1104826B/it active
- 1978-05-25 DE DE19782823206 patent/DE2823206A1/de active Granted
- 1978-05-26 JP JP6344978A patent/JPS5475799A/ja active Pending
- 1978-05-26 FR FR7815823A patent/FR2410142A1/fr active Granted
Cited By (2)
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 |
---|---|
FR2410142B3 (fr) | 1981-02-13 |
IT7849517A0 (it) | 1978-05-24 |
GB1570680A (en) | 1980-07-02 |
IT1104826B (it) | 1985-10-28 |
JPS5475799A (en) | 1979-06-16 |
DE2823206A1 (de) | 1979-06-07 |
US4183478A (en) | 1980-01-15 |
DE2823206C2 (fr) | 1987-03-05 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR2410142A1 (fr) | Inverseur de poussee a portes en coquille de peigne et a ailettes en cascade | |
EP0696985B1 (fr) | Agencement de nacelle | |
US4407120A (en) | Thrust reverser geared linkage | |
FR2661213A1 (fr) | Moteur d'aviation a tres grand taux de dilution et du type dit contrafan avant. | |
US3067579A (en) | Gas turbine power plant | |
GB1516980A (en) | Mounting ducted fan gas turbine engines on 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 (fr) | ||
EP0913569A2 (fr) | Boitier pour une turbine à gaz | |
GB1318748A (en) | Gas turgine ducted fan engines for aircraft | |
EP1462642A1 (fr) | Dispositif d'inversion de poussée de turboréacteur à double flux | |
EP1026387A3 (fr) | Portes d'un inverseur de poussée avec forme adaptée à une tuyère ondulée | |
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 | |
FR2369429A1 (fr) | Melangeur hybride pour turbo-moteur dilue et moteur ainsi obtenu | |
US3059426A (en) | Thrust reverser utilizing aft end mechanical blockage | |
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 | |
GB1207907A (en) | Controllable air-intake arrangement for a turbo-ramjet unit | |
FR2759418A1 (fr) | Inverseur de poussee pour turbosoufflante a tres grand taux de dilution |