FR2018120A1 - - Google Patents
Info
- Publication number
- FR2018120A1 FR2018120A1 FR6931064A FR6931064A FR2018120A1 FR 2018120 A1 FR2018120 A1 FR 2018120A1 FR 6931064 A FR6931064 A FR 6931064A FR 6931064 A FR6931064 A FR 6931064A FR 2018120 A1 FR2018120 A1 FR 2018120A1
- Authority
- FR
- France
- 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.)
- Withdrawn
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
- F02K1/58—Reversers mounted on the inner cone or the nozzle housing or the fuselage
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Turbines (AREA)
- Lift Valve (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4382468 | 1968-09-14 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2018120A1 true FR2018120A1 (fr) | 1970-05-29 |
Family
ID=10430458
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR6931064A Withdrawn FR2018120A1 (fr) | 1968-09-14 | 1969-09-12 |
Country Status (4)
Country | Link |
---|---|
US (1) | US3570247A (fr) |
DE (1) | DE1946592B2 (fr) |
FR (1) | FR2018120A1 (fr) |
GB (1) | GB1253071A (fr) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2123115B1 (fr) * | 1971-01-08 | 1975-01-17 | Serap | |
US3824946A (en) * | 1972-08-30 | 1974-07-23 | D Macardy | Water jet propulsion unit |
US3774868A (en) * | 1972-12-11 | 1973-11-27 | G Goetz | Integrated nozzle |
US3831376A (en) * | 1973-02-05 | 1974-08-27 | Boeing Co | Thrust reverser |
US4037405A (en) * | 1975-09-30 | 1977-07-26 | United Technologies Corporation | Two dimensional nozzle with rotating plug |
US4050631A (en) * | 1976-03-26 | 1977-09-27 | The Boeing Company | Jet engine nozzle for controlling the direction of thrust |
US4088270A (en) * | 1976-03-31 | 1978-05-09 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Two dimensional wedge/translating shroud nozzle |
US4147027A (en) * | 1976-04-06 | 1979-04-03 | Grumman Aerospace Corporation | Thrust reverser nozzle |
US4175385A (en) * | 1977-12-12 | 1979-11-27 | General Electric Company | Thrust reverser for an asymmetric aircraft exhaust nozzle |
US5699966A (en) * | 1980-03-31 | 1997-12-23 | General Electric Company | Exhaust nozzle of a gas turbine engine |
FR2622928A1 (fr) * | 1987-11-05 | 1989-05-12 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a portes,a section variable d'ejection |
FR2766522B1 (fr) * | 1997-07-24 | 1999-09-03 | Hispano Suiza Sa | Inverseur de poussee de turbosoufflante a obstacle a guidage axial lies au capot primaire |
SE515379C2 (sv) * | 1999-12-22 | 2001-07-23 | Saab Ab | Utloppsanordning för en jetmotor samt flygfarkost med en utloppsanordning |
US7568348B2 (en) * | 2005-11-28 | 2009-08-04 | Aerojet-General Corporation | Nozzle assembly for rocket and ramjet applications |
DE102008022289B4 (de) * | 2008-04-25 | 2010-07-29 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Flugkörper |
US9623976B2 (en) * | 2012-07-25 | 2017-04-18 | Rohr, Inc. | Nacelle for a high bypass ratio engine with multiple flow paths |
US10001080B2 (en) * | 2014-08-19 | 2018-06-19 | The Boeing Company | Thrust reverse variable area fan nozzle |
RU2758875C1 (ru) * | 2020-07-23 | 2021-11-02 | Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") | Выходное устройство плоского реактивного сопла |
RU2758867C1 (ru) * | 2020-07-23 | 2021-11-02 | Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") | Выходное устройство плоского реактивного сопла |
-
1968
- 1968-09-14 GB GB4382468A patent/GB1253071A/en not_active Expired
-
1969
- 1969-09-11 US US857029A patent/US3570247A/en not_active Expired - Lifetime
- 1969-09-12 FR FR6931064A patent/FR2018120A1/fr not_active Withdrawn
- 1969-09-15 DE DE19691946592 patent/DE1946592B2/de active Granted
Also Published As
Publication number | Publication date |
---|---|
DE1946592B2 (de) | 1977-02-24 |
US3570247A (en) | 1971-03-16 |
DE1946592A1 (de) | 1970-05-21 |
GB1253071A (fr) | 1971-11-10 |
Similar Documents
Legal Events
Date | Code | Title | Description |
---|---|---|---|
TP | Transmission of property | ||
TP | Transmission of property | ||
TP | Transmission of property | ||
ST | Notification of lapse |