JPS5514263B1 - - Google Patents
Info
- Publication number
- JPS5514263B1 JPS5514263B1 JP723962A JP396272A JPS5514263B1 JP S5514263 B1 JPS5514263 B1 JP S5514263B1 JP 723962 A JP723962 A JP 723962A JP 396272 A JP396272 A JP 396272A JP S5514263 B1 JPS5514263 B1 JP S5514263B1
- Authority
- JP
- Japan
- 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.)
- Pending
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
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)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10357771A | 1971-01-04 | 1971-01-04 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS5514263B1 true JPS5514263B1 (ja) | 1980-04-15 |
Family
ID=22295922
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP723962A Pending JPS5514263B1 (ja) | 1971-01-04 | 1971-12-28 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US3699682A (ja) |
| JP (1) | JPS5514263B1 (ja) |
| CA (1) | CA932968A (ja) |
| FR (1) | FR2121563B1 (ja) |
| GB (1) | GB1316029A (ja) |
Families Citing this family (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3981451A (en) * | 1975-11-17 | 1976-09-21 | Rohr Industries, Inc. | Fan cascade thrust reverser |
| US4410150A (en) * | 1980-03-03 | 1983-10-18 | General Electric Company | Drag-reducing nacelle |
| FR2486153B1 (fr) * | 1980-07-04 | 1985-10-04 | Hurel Dubois Avions | Inverseur de poussee pour moteur a reaction, destine notamment a equiper un aeronef |
| FR2506843B1 (fr) * | 1981-05-29 | 1987-04-24 | Hurel Dubois Avions | Dispositif d'inversion de poussee pour turboreacteur d'avion |
| FR2730763B1 (fr) * | 1995-02-21 | 1997-03-14 | Hispano Suiza Sa | Inverseur de poussee a volets aval pour turboreacteur |
| FR2752017B1 (fr) * | 1996-08-01 | 1998-10-16 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a portes formant ecopes |
| FR2754565B1 (fr) * | 1996-10-10 | 1999-01-08 | Hispano Suiza Sa | Inverseur de poussee a portes a debit de fuite controle |
| FR2760789B1 (fr) * | 1997-03-13 | 2001-09-07 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a portes a structure externe autoraidie |
| US7797944B2 (en) | 2006-10-20 | 2010-09-21 | United Technologies Corporation | Gas turbine engine having slim-line nacelle |
| US7870721B2 (en) | 2006-11-10 | 2011-01-18 | United Technologies Corporation | Gas turbine engine providing simulated boundary layer thickness increase |
| US8408491B2 (en) * | 2007-04-24 | 2013-04-02 | United Technologies Corporation | Nacelle assembly having inlet airfoil for a gas turbine engine |
| US8205430B2 (en) * | 2007-05-16 | 2012-06-26 | United Technologies Corporation | Variable geometry nacelle assembly for a gas turbine engine |
| US8402739B2 (en) * | 2007-06-28 | 2013-03-26 | United Technologies Corporation | Variable shape inlet section for a nacelle assembly of a gas turbine engine |
| US9004399B2 (en) | 2007-11-13 | 2015-04-14 | United Technologies Corporation | Nacelle flow assembly |
| US8192147B2 (en) * | 2007-12-14 | 2012-06-05 | United Technologies Corporation | Nacelle assembly having inlet bleed |
| US8186942B2 (en) * | 2007-12-14 | 2012-05-29 | United Technologies Corporation | Nacelle assembly with turbulators |
| DE102011008917A1 (de) * | 2011-01-19 | 2012-07-19 | Rolls-Royce Deutschland Ltd & Co Kg | Fluggasturbinenschubumkehrvorrichtung |
| US9016040B2 (en) * | 2012-11-30 | 2015-04-28 | General Electric Company | Thrust reverser system with translating-rotating cascade and method of operation |
| US9581108B2 (en) | 2013-02-22 | 2017-02-28 | United Technologies Corporation | Pivot thrust reverser with multi-point actuation |
| US9694912B2 (en) | 2013-02-22 | 2017-07-04 | United Technologies Corporation | ATR guide pins for sliding nacelle |
| FR3092145A1 (fr) * | 2019-01-24 | 2020-07-31 | Airbus Operations | Turboreacteur double flux comportant une serie de lames rotatives pour obturer la veine du flux secondaire |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB745720A (en) * | 1952-07-08 | 1956-02-29 | Rolls Royce | Improvements in or relating to aircraft reaction propulsion units and installations |
| BE556200A (ja) * | 1956-03-29 | |||
| US3024601A (en) * | 1960-04-12 | 1962-03-13 | Gen Electric | Thrust spoiler and reingestion control |
| US3279182A (en) * | 1965-06-07 | 1966-10-18 | Gen Electric | Thrust reverser |
| US3344604A (en) * | 1965-12-14 | 1967-10-03 | Gen Dynamics Corp | Apparatus for selectively reversing the thrust of front fan jet engines |
| US3601992A (en) * | 1970-06-10 | 1971-08-31 | Rohr Corp | Thrust reversing apparatus |
-
1971
- 1971-01-04 US US103577A patent/US3699682A/en not_active Expired - Lifetime
- 1971-12-13 GB GB5787171A patent/GB1316029A/en not_active Expired
- 1971-12-14 CA CA130137A patent/CA932968A/en not_active Expired
- 1971-12-28 JP JP723962A patent/JPS5514263B1/ja active Pending
-
1972
- 1972-01-04 FR FR7200127A patent/FR2121563B1/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| US3699682A (en) | 1972-10-24 |
| FR2121563B1 (ja) | 1977-06-24 |
| CA932968A (en) | 1973-09-04 |
| FR2121563A1 (ja) | 1972-08-25 |
| GB1316029A (en) | 1973-05-09 |
| DE2200521A1 (de) | 1972-07-20 |
| DE2200521B2 (de) | 1976-08-19 |