DK140996C - - Google Patents
Info
- Publication number
- DK140996C DK140996C DK513976A DK513976A DK140996C DK 140996 C DK140996 C DK 140996C DK 513976 A DK513976 A DK 513976A DK 513976 A DK513976 A DK 513976A DK 140996 C DK140996 C DK 140996C
- Authority
- DK
- Denmark
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
-
- 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
- F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
- F02K1/006—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector within one plane only
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Nozzles (AREA)
- Supercharger (AREA)
- Exhaust-Gas Circulating Devices (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US05/640,377 US3973731A (en) | 1975-12-12 | 1975-12-12 | Flap-type two-dimensional nozzle |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| DK513976A DK513976A (nl) | 1977-06-13 |
| DK140996B DK140996B (da) | 1979-12-17 |
| DK140996C true DK140996C (nl) | 1980-06-02 |
Family
ID=24568001
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DK513976AA DK140996B (da) | 1975-12-12 | 1976-11-16 | Flapkonstruktion for todimensional dyse. |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US3973731A (nl) |
| BE (1) | BE848916A (nl) |
| CA (1) | CA1066518A (nl) |
| DK (1) | DK140996B (nl) |
| IT (1) | IT1065153B (nl) |
| NL (1) | NL7612696A (nl) |
| NO (1) | NO145628C (nl) |
Families Citing this family (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4238928A (en) * | 1979-02-14 | 1980-12-16 | Stupica Vekoslav A | Hydraulic engine |
| US4361281A (en) * | 1980-07-07 | 1982-11-30 | General Electric Company | Exhaust nozzle |
| US4382551A (en) * | 1981-05-18 | 1983-05-10 | United Technologies Corporation | Flap-type nozzle with built-in reverser |
| US4422524A (en) * | 1982-03-22 | 1983-12-27 | Lockheed Corporation | Variable shape, fluid flow nozzle for sound suppression |
| FR2714422A1 (fr) * | 1983-01-13 | 1995-06-30 | Snecma | Tuyère convergente-divergente, en particulier pour turboréacteur. |
| US4605169A (en) * | 1983-12-27 | 1986-08-12 | United Technologies Corporation | Exhaust nozzle construction |
| US4591097A (en) * | 1984-05-16 | 1986-05-27 | The United States Of America As Represented By The Secretary Of The Air Force | Thrust reverser/exhaust nozzle assembly for a gas turbine engine |
| US4753392A (en) * | 1984-11-02 | 1988-06-28 | United Technologies Corporation | Two dimensional gas turbine engine exhaust nozzle |
| FR2622928A1 (fr) * | 1987-11-05 | 1989-05-12 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a portes,a section variable d'ejection |
| GB2277559A (en) * | 1993-04-30 | 1994-11-02 | Marconi Gec Ltd | Variable area convergent-divergent nozzle. |
| US8051639B2 (en) * | 2007-11-16 | 2011-11-08 | The Nordam Group, Inc. | Thrust reverser |
| RU2445486C1 (ru) * | 2010-11-26 | 2012-03-20 | Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн") | Плоское сопло турбореактивного двигателя |
| RU2445487C1 (ru) * | 2010-12-02 | 2012-03-20 | Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн") | Плоское сопло турбореактивного двигателя |
| RU2462609C1 (ru) * | 2011-02-18 | 2012-09-27 | Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн") | Плоское сопло турбореактивного двигателя |
| JP6183837B2 (ja) * | 2013-08-19 | 2017-08-23 | 国立研究開発法人宇宙航空研究開発機構 | 排気ノズル |
| WO2017218841A1 (en) | 2016-06-15 | 2017-12-21 | The Regents Of The University Of California | Two-dimensional supersonic nozzle thrust vectoring using staggered ramps |
| RU2674232C1 (ru) * | 2017-10-05 | 2018-12-05 | Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") | Плоское сопло турбореактивного авиационного двигателя |
| GB2592267A (en) * | 2020-02-24 | 2021-08-25 | Altair Uk Ltd | Pulse nozzle for filter cleaning systems |
| CN113969848B (zh) * | 2021-09-27 | 2022-10-25 | 太仓点石航空动力有限公司 | 满足飞行器全包线的二元机械推力矢量喷管及控制方法 |
| US11994087B2 (en) * | 2021-12-06 | 2024-05-28 | Rohr, Inc. | Variable area nozzle and method for operating same |
| US11867136B2 (en) | 2021-12-17 | 2024-01-09 | Rohr, Inc. | Variable area nozzle assembly and method for operating same |
| US11754018B2 (en) | 2021-12-17 | 2023-09-12 | Rohr, Inc. | Aircraft propulsion system exhaust nozzle with ejector passage(s) |
| US12065977B2 (en) | 2022-07-22 | 2024-08-20 | Rtx Corporation | Multi-duct exhaust system for gas turbine engine |
| US11867135B1 (en) | 2022-09-14 | 2024-01-09 | Rtx Corporation | Vectoring exhaust nozzle for an aircraft powerplant |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB996461A (en) * | 1962-09-03 | 1965-06-30 | Bristol Siddeley Engines Ltd | Improvements relating to jet propulsion power plants |
| US3511441A (en) * | 1964-10-01 | 1970-05-12 | United Aircraft Corp | Ejector with variable inner flap |
| US3386658A (en) * | 1965-12-08 | 1968-06-04 | Usa | Convergent-divergent jet exhaust nozzle for supersonic aircraft |
| US3454227A (en) * | 1966-08-19 | 1969-07-08 | United Aircraft Corp | Free floating articulate ejector nozzle |
| GB1395709A (en) * | 1971-07-06 | 1975-05-29 | Rolls Royce | Jet propulsion power plant |
-
1975
- 1975-12-12 US US05/640,377 patent/US3973731A/en not_active Expired - Lifetime
-
1976
- 1976-10-14 CA CA263,399A patent/CA1066518A/en not_active Expired
- 1976-11-16 DK DK513976AA patent/DK140996B/da unknown
- 1976-11-16 NL NL7612696A patent/NL7612696A/nl not_active Application Discontinuation
- 1976-11-30 BE BE172848A patent/BE848916A/xx not_active IP Right Cessation
- 1976-12-03 IT IT30082/76A patent/IT1065153B/it active
- 1976-12-06 NO NO764145A patent/NO145628C/no unknown
Also Published As
| Publication number | Publication date |
|---|---|
| IT1065153B (it) | 1985-02-25 |
| NL7612696A (nl) | 1977-06-14 |
| NO764145L (nl) | 1977-06-14 |
| BE848916A (fr) | 1977-03-16 |
| NO145628C (no) | 1982-04-28 |
| CA1066518A (en) | 1979-11-20 |
| DK513976A (nl) | 1977-06-13 |
| NO145628B (no) | 1982-01-18 |
| DK140996B (da) | 1979-12-17 |
| US3973731A (en) | 1976-08-10 |