NL262125A - - Google Patents
Info
- Publication number
- NL262125A NL262125A NL262125DA NL262125A NL 262125 A NL262125 A NL 262125A NL 262125D A NL262125D A NL 262125DA NL 262125 A NL262125 A NL 262125A
- Authority
- NL
- Netherlands
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
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
- F02K1/1261—Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a substantially axially movable structure
-
- 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
- F02K1/36—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto having an ejector
-
- 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)
- Jet Pumps And Other Pumps (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US19421A US3098352A (en) | 1960-04-01 | 1960-04-01 | Adjustable jet propulsion nozzle with secondary air flow control |
CH37161A CH391385A (de) | 1961-01-12 | 1961-01-12 | Einstellbare Schubdüse |
Publications (1)
Publication Number | Publication Date |
---|---|
NL262125A true NL262125A (zh) |
Family
ID=25684374
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NL262125D NL262125A (zh) | 1960-04-01 |
Country Status (5)
Country | Link |
---|---|
US (1) | US3098352A (zh) |
CH (1) | CH412474A (zh) |
FR (1) | FR1280852A (zh) |
GB (1) | GB907526A (zh) |
NL (1) | NL262125A (zh) |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB985192A (en) * | 1960-05-13 | 1965-03-03 | Bristol Siddeley Engines Ltd | Improvements in aircraft propulsion power plants |
US3229457A (en) * | 1962-10-15 | 1966-01-18 | James R Rowe | Variable area ratio rocket nozzle |
DE1262682B (de) * | 1963-08-22 | 1968-03-07 | Rolls Royce | Mantelstromgasturbinentriebwerk |
US3258913A (en) * | 1963-09-20 | 1966-07-05 | Boeing Co | Method and apparatus for varying the area of an air flow device |
GB1008322A (en) * | 1964-08-04 | 1965-10-27 | Rolls Royce | Gas turbine engine |
GB1068746A (en) * | 1964-11-27 | 1967-05-10 | Rolls Royce | Jet propulsion engine |
US3662957A (en) * | 1970-10-28 | 1972-05-16 | United Aircraft Corp | Low friction track bearing assembly |
US3897001A (en) * | 1974-06-12 | 1975-07-29 | Gen Electric | Nozzle and auxiliary inlet arrangement for gas turbine engine |
US4074523A (en) * | 1976-12-08 | 1978-02-21 | The United States Of America As Represented By The Secretary Of The Air Force | Pressure actuated collapsible curtain liners for a gas turbine engine nozzle |
US4587806A (en) * | 1981-05-11 | 1986-05-13 | United Technologies Corporation | Area two-dimensional converging/diverging nozzle |
FR2608680B1 (fr) * | 1986-12-17 | 1989-03-17 | Snecma | Tuyere bidimensionnelle reglable, notamment pour reacteur d'avion |
FR2637017B1 (fr) * | 1988-09-28 | 1990-11-30 | Snecma | Structure de tuyere pour propulseur combine turbo-stato-fusee |
FR2670177B1 (fr) * | 1990-12-05 | 1993-01-22 | Snecma | Joint d'etancheite entre l'arriere du fuselage d'un avion et les volets exterieurs de son turboreacteur. |
US5351888A (en) * | 1993-05-14 | 1994-10-04 | General Electric Company | Multi-axis vectorable exhaust nozzle |
US5431344A (en) * | 1993-11-12 | 1995-07-11 | United Technologies Corporation | Sliding throat gas turbine engine nozzle |
FR2715192B1 (fr) * | 1994-01-20 | 1996-02-16 | Snecma | Tuyère d'éjection de turboréacteur. |
FR2790791B1 (fr) * | 1999-03-10 | 2001-04-13 | Snecma | Tuyere d'ejection de turboreacteur axisymetrique et a orientation globale |
US8572986B2 (en) * | 2009-07-27 | 2013-11-05 | United Technologies Corporation | Retainer for suspended thermal protection elements in a gas turbine engine |
US9371800B2 (en) * | 2011-03-01 | 2016-06-21 | Grollo Aerospace | Engine for use in an aerial vehicle |
US9581109B1 (en) * | 2013-04-11 | 2017-02-28 | Geoffrey P. Pinto | Axially translating and radially tilting fan nozzle segments with combined actuation and position sensing |
USD868627S1 (en) | 2018-04-27 | 2019-12-03 | Jetoptera, Inc. | Flying car |
US10464668B2 (en) | 2015-09-02 | 2019-11-05 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
ES2844127T3 (es) | 2015-09-02 | 2021-07-21 | Jetoptera Inc | Configuraciones de eyector y perfil aerodinámico |
GB2588653A (en) | 2019-10-31 | 2021-05-05 | Rolls Royce Plc | An exhaust nozzle |
GB2588652A (en) * | 2019-10-31 | 2021-05-05 | Rolls Royce Plc | An exhaust nozzle |
GB2588651A (en) | 2019-10-31 | 2021-05-05 | Rolls Royce Plc | An exhaust nozzle |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2729937A (en) * | 1951-03-20 | 1956-01-10 | United Aircraft Corp | Retractable flameholders for afterburners |
US2770944A (en) * | 1952-04-26 | 1956-11-20 | United Aircraft Corp | Variable area reaction nozzle movable from convergent to convergent-di-vergent form |
GB733383A (en) * | 1953-02-05 | 1955-07-13 | British Thomson Houston Co Ltd | Improvements in and relating to fuel-reaction-chambers |
FR1006139A (fr) * | 1954-11-25 | 1952-04-21 | Cem Comp Electro Mec | Procédé et dispositif de réglage des turbo-réacteurs |
US2910828A (en) * | 1956-08-24 | 1959-11-03 | United Aircraft Company | Convergent-divergent variable area propulsion nozzle |
GB872195A (en) * | 1957-05-21 | 1961-07-05 | English Electric Co Ltd | Improvements in and relating to jet propulsion nozzles |
US3049873A (en) * | 1958-02-04 | 1962-08-21 | Westinghouse Electric Corp | Exhaust nozzle having a flow area of variable convergency and divergency |
US2984068A (en) * | 1958-06-30 | 1961-05-16 | Orenda Engines Ltd | Propulsive nozzle system for reaction propulsion units |
-
0
- NL NL262125D patent/NL262125A/xx unknown
-
1960
- 1960-04-01 US US19421A patent/US3098352A/en not_active Expired - Lifetime
-
1961
- 1961-01-04 FR FR848733A patent/FR1280852A/fr not_active Expired
- 1961-02-13 GB GB5246/61A patent/GB907526A/en not_active Expired
- 1961-03-30 CH CH381961A patent/CH412474A/de unknown
Also Published As
Publication number | Publication date |
---|---|
US3098352A (en) | 1963-07-23 |
CH412474A (de) | 1966-04-30 |
GB907526A (en) | 1962-10-03 |
FR1280852A (fr) | 1962-01-08 |