NL255475A - - Google Patents
Info
- Publication number
- NL255475A NL255475A NL255475DA NL255475A NL 255475 A NL255475 A NL 255475A NL 255475D A NL255475D A NL 255475DA NL 255475 A NL255475 A NL 255475A
- 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
- F02K1/002—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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
- B64C29/0066—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors with horizontal jet and jet deflector
-
- 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)
- Aviation & Aerospace Engineering (AREA)
- Exhaust Silencers (AREA)
- Control Of Turbines (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US844328A US3019601A (en) | 1959-10-05 | 1959-10-05 | Pen-shaped nozzle with thrust deflector |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| NL255475A true NL255475A (xx) |
Family
ID=25292403
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NL255475D NL255475A (xx) | 1959-10-05 | ||
| NL121474D NL121474C (xx) | 1959-10-05 |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NL121474D NL121474C (xx) | 1959-10-05 |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US3019601A (xx) |
| BE (1) | BE595414A (xx) |
| CH (1) | CH399916A (xx) |
| DE (1) | DE1159769B (xx) |
| GB (1) | GB900040A (xx) |
| NL (2) | NL121474C (xx) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3080711A (en) * | 1960-01-06 | 1963-03-12 | James F Connors | Penshape exhaust nozzle for supersonic engine |
| GB918189A (en) * | 1960-07-01 | 1963-02-13 | Rolls Royce | Jet propulsion nozzle |
| US4000610A (en) * | 1975-04-28 | 1977-01-04 | General Electric Company | Flight maneuverable nozzle for gas turbine engines |
| US4000611A (en) * | 1975-07-01 | 1977-01-04 | General Electric Company | Variable area, load balancing nozzle |
| FR2537657A1 (fr) * | 1982-12-08 | 1984-06-15 | Snecma | Tuyere a section variable pour un turboreacteur et avion comportant un tel equipement |
| US6000635A (en) * | 1995-10-02 | 1999-12-14 | Lockheed Martin Corporation | Exhaust nozzle for a turbojet engine |
| EP0959000A1 (en) * | 1998-03-10 | 1999-11-24 | Manuel Munoz Saiz | Lift enhancing and drag reducing device for aircraft |
| US9181899B2 (en) * | 2008-08-27 | 2015-11-10 | General Electric Company | Variable slope exhaust nozzle |
| US9810178B2 (en) | 2015-08-05 | 2017-11-07 | General Electric Company | Exhaust nozzle with non-coplanar and/or non-axisymmetric shape |
| RU2668309C1 (ru) * | 2017-07-20 | 2018-09-28 | Публичное акционерное общество "ОДК - Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") | Выхлопное сопло турбореактивного двигателя летательного аппарата |
| CN110496713B (zh) * | 2019-09-20 | 2024-06-18 | 常熟华东汽车有限公司 | 除雪车用的矢量喷口结构 |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2734698A (en) * | 1956-02-14 | Aikplane control surface and jet | ||
| US2657575A (en) * | 1947-08-21 | 1953-11-03 | Harry J Allen | Asymmetric adjustable supersonic nozzle |
| BE498317A (xx) * | 1949-10-06 | |||
| US2840325A (en) * | 1951-12-05 | 1958-06-24 | Rolls Royce | Aircraft structure |
| US2758805A (en) * | 1952-03-18 | 1956-08-14 | Northrop Aircraft Inc | Blast deflector arrangement for jet propelled aircraft |
| US2866610A (en) * | 1956-04-10 | 1958-12-30 | John E M Taylor | Aircraft jet thrust control |
| US2951660A (en) * | 1956-06-25 | 1960-09-06 | James V Giliberty | Method and means for controlling the jet thrust of an aircraft |
| US2956759A (en) * | 1957-02-21 | 1960-10-18 | English Electric Co Ltd | Aircraft wings incorporating power installation for propulsion |
| US2944765A (en) * | 1958-09-01 | 1960-07-12 | Bristol Siddeley Engines Ltd | Jet-propelled aircraft |
-
0
- NL NL255475D patent/NL255475A/xx unknown
- NL NL121474D patent/NL121474C/xx active
-
1959
- 1959-10-05 US US844328A patent/US3019601A/en not_active Expired - Lifetime
-
1960
- 1960-08-25 GB GB29370/60A patent/GB900040A/en not_active Expired
- 1960-09-23 DE DEU7478A patent/DE1159769B/de active Pending
- 1960-09-26 BE BE595414A patent/BE595414A/fr unknown
- 1960-09-29 CH CH1095660A patent/CH399916A/de unknown
Also Published As
| Publication number | Publication date |
|---|---|
| NL121474C (xx) | |
| DE1159769B (de) | 1963-12-19 |
| US3019601A (en) | 1962-02-06 |
| CH399916A (de) | 1965-09-30 |
| GB900040A (en) | 1962-07-04 |
| BE595414A (fr) | 1961-03-27 |