BE682004A - - Google Patents
Info
- Publication number
- BE682004A BE682004A BE682004DA BE682004A BE 682004 A BE682004 A BE 682004A BE 682004D A BE682004D A BE 682004DA BE 682004 A BE682004 A BE 682004A
- Authority
- BE
- Belgium
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
- F02K1/64—Reversing fan flow
- F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
- F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed 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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US462793A US3262270A (en) | 1965-06-07 | 1965-06-07 | Thrust reverser |
Publications (1)
Publication Number | Publication Date |
---|---|
BE682004A true BE682004A (nl) | 1966-11-14 |
Family
ID=23837774
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE682004D BE682004A (nl) | 1965-06-07 | 1966-06-02 |
Country Status (4)
Country | Link |
---|---|
US (1) | US3262270A (nl) |
BE (1) | BE682004A (nl) |
DE (1) | DE1289434B (nl) |
GB (1) | GB1092015A (nl) |
Families Citing this family (38)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3344604A (en) * | 1965-12-14 | 1967-10-03 | Gen Dynamics Corp | Apparatus for selectively reversing the thrust of front fan jet engines |
US3398535A (en) * | 1966-05-25 | 1968-08-27 | Gen Electric | Engine supporting structure |
GB1127828A (en) * | 1966-06-29 | 1968-09-18 | Rolls Royce | Fan thrust reverser for jet propulsion plant |
US3500644A (en) * | 1968-04-10 | 1970-03-17 | Rohr Corp | Thrust reverser |
US3500645A (en) * | 1968-04-10 | 1970-03-17 | Rohr Corp | Thrust reverser |
US3500646A (en) * | 1968-04-19 | 1970-03-17 | Rohr Corp | Thrust reverser |
US3511055A (en) * | 1968-05-29 | 1970-05-12 | Rohr Corp | Thrust reverser |
GB1210623A (en) * | 1969-01-31 | 1970-10-28 | Rolls Royce | Improvements in or relating to fluid flow control valves |
US3541794A (en) * | 1969-04-23 | 1970-11-24 | Gen Electric | Bifurcated fan duct thrust reverser |
US3599432A (en) * | 1970-04-02 | 1971-08-17 | Rohr Corp | Thrust reversing apparatus for turbo-fan propulsion unit |
US3814324A (en) * | 1972-06-19 | 1974-06-04 | Gen Electric | Propulsion nozzle and actuator system employed therein |
US3779010A (en) * | 1972-08-17 | 1973-12-18 | Gen Electric | Combined thrust reversing and throat varying mechanism for a gas turbine engine |
US4030291A (en) * | 1976-01-02 | 1977-06-21 | General Electric Company | Thrust reverser for a gas turbofan engine |
US4216926A (en) * | 1978-06-30 | 1980-08-12 | Rohr Industries, Inc. | Linkage system for a turbo fan engine thrust reverser |
US4545199A (en) * | 1982-06-14 | 1985-10-08 | Rohr Industries, Inc. | Fan cascade reverser having dual blocker doors |
EP0109219A3 (en) * | 1982-11-12 | 1985-11-13 | LUCAS INDUSTRIES public limited company | Thrust reversing apparatus for a gas turbine engine |
US4533098A (en) * | 1983-06-20 | 1985-08-06 | General Electric Company | Thrust reverser attachment |
GB2182724B (en) * | 1985-10-08 | 1988-12-07 | Rolls Royce | Gas turbine engine thrust reverser |
FR2611233B1 (fr) * | 1987-02-19 | 1991-05-10 | Hurel Dubois Avions | Groupe moto-propulseur d'avion du type a ventilateur capote equipe d'un inverseur de poussee a portes |
DE3844188C1 (nl) * | 1988-12-29 | 1990-05-17 | Mtu Muenchen Gmbh | |
US5224341A (en) * | 1992-01-06 | 1993-07-06 | United Technologies Corporation | Separable fan strut for a gas turbofan powerplant |
US5239822A (en) * | 1992-01-14 | 1993-08-31 | The Boeing Company | Composite structure for thrust reverser torque box |
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 |
US7837141B2 (en) * | 2006-03-22 | 2010-11-23 | The Boeing Company | Reaction drive rotor/wing variable area nozzle |
FR2904372B1 (fr) * | 2006-07-26 | 2008-10-31 | Snecma Sa | Tuyere d'ejection des gaz pour turbomachine a double flux ayant une section d'ejection ou de col variable par deplacement du capot secondaire |
EP2578864B1 (en) * | 2007-08-08 | 2014-09-24 | Rohr, Inc. | Variable area fan nozzle with bypass flow |
FR2922958B1 (fr) * | 2007-10-25 | 2009-11-20 | Aircelle Sa | Inverseur de poussee a grilles |
JP5405083B2 (ja) * | 2008-10-31 | 2014-02-05 | ゼネラル・エレクトリック・カンパニイ | ガスタービンエンジン逆スラスト装置用のバッフルシール |
FR2946094B1 (fr) * | 2009-06-02 | 2014-04-18 | Aircelle Sa | Inverseur de poussee pour nacelle de turboreacteur double flux. |
FR2960918B1 (fr) * | 2010-06-08 | 2012-05-25 | Aircelle Sa | Grille de deviation du type autosupporte pour inverseur de poussee |
US9574519B2 (en) * | 2013-08-23 | 2017-02-21 | Rohr, Inc. | Multi surface blocker door system and apparatus |
US10612490B2 (en) | 2014-04-25 | 2020-04-07 | Rohr, Inc. | Drag link assembly including buried drag link fitting |
US20160305370A1 (en) * | 2015-04-16 | 2016-10-20 | Honeywell International Inc. | Translating cowl thrust reverser with door pivots aft of reverse flow path |
US10563614B2 (en) | 2016-08-17 | 2020-02-18 | Honeywell International Inc. | Composite translating cowl assembly for a thrust reverser system |
FR3058474B1 (fr) * | 2016-11-04 | 2020-10-23 | Airbus Operations Sas | Ensemble propulsif d'aeronef comprenant au moins un systeme de guidage d'un dispositif d'inversion de poussee supporte par un carter de soufflante |
FR3091855A1 (fr) | 2019-01-22 | 2020-07-24 | Airbus Operations | NACELLE D’UN TURBOREACTEUR COMPORTANT UN ensemble mobile ET UNe structure fixe renforcee |
FR3122905A1 (fr) * | 2021-05-14 | 2022-11-18 | Safran Nacelles | Ensemble propulsif d’aéronef comprenant un actionneur relié à un bras structural tel qu’une aube directrice de sortie |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2681548A (en) * | 1948-10-27 | 1954-06-22 | Peter G Kappus | Reversible thrust nozzle for jet engines |
GB777803A (en) * | 1953-01-15 | 1957-06-26 | Pye Ltd | Improvements in or relating to television receivers |
US3002342A (en) * | 1953-08-12 | 1961-10-03 | Schatzki Erich | Mechanism for controlling relatively high velocity flow of fluids longitudinally through and laterally from ambulant conduit means |
US2945346A (en) * | 1954-10-04 | 1960-07-19 | Republic Aviat Corp | Reverse thrust brake |
US2847823A (en) * | 1955-03-15 | 1958-08-19 | Curtiss Wright Corp | Reverse thrust nozzle construction |
US2841956A (en) * | 1956-02-20 | 1958-07-08 | William E Gunson | Combination variable area converging-diverging nozzle and thrust destroyer |
US3113428A (en) * | 1957-03-13 | 1963-12-10 | Rolls Royce | Silenced jet propulsion nozzle with thrust reversing means |
FR1286886A (fr) * | 1961-01-27 | 1962-03-09 | Nord Aviation | Dispositif d'inversion de poussée pour propulseurs comportant un turbo-réacteur àdouble flux |
NL247267A (nl) * | 1958-04-02 | |||
US3068646A (en) * | 1959-01-28 | 1962-12-18 | Rolls Royce | Improvements in by-pass type gas turbine engines |
US3036431A (en) * | 1959-09-08 | 1962-05-29 | Boeing Co | Thrust reverser for jet engines |
DE1127725B (de) * | 1960-01-12 | 1962-04-12 | Rolls Royce | Strahltriebwerk mit Mitteln zur Strahlumkehr |
-
1965
- 1965-06-07 US US462793A patent/US3262270A/en not_active Expired - Lifetime
-
1966
- 1966-04-20 GB GB17250/66A patent/GB1092015A/en not_active Expired
- 1966-06-02 BE BE682004D patent/BE682004A/xx unknown
- 1966-06-07 DE DEG47105A patent/DE1289434B/de active Pending
Also Published As
Publication number | Publication date |
---|---|
DE1289434B (de) | 1969-02-13 |
GB1092015A (en) | 1967-11-22 |
US3262270A (en) | 1966-07-26 |