NL6605188A - - Google Patents
Info
- Publication number
- NL6605188A NL6605188A NL6605188A NL6605188A NL6605188A NL 6605188 A NL6605188 A NL 6605188A NL 6605188 A NL6605188 A NL 6605188A NL 6605188 A NL6605188 A NL 6605188A NL 6605188 A NL6605188 A NL 6605188A
- 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
- F02K1/004—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 by using one or more swivable nozzles rotating about their own axis
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US44903465A | 1965-04-19 | 1965-04-19 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| NL6605188A true NL6605188A (en:Method) | 1966-10-20 |
Family
ID=23782608
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NL6605188A NL6605188A (en:Method) | 1965-04-19 | 1966-04-19 |
Country Status (7)
| Country | Link |
|---|---|
| BE (1) | BE679612A (en:Method) |
| CH (1) | CH456357A (en:Method) |
| DE (1) | DE1481554A1 (en:Method) |
| FR (1) | FR1506309A (en:Method) |
| GB (1) | GB1132157A (en:Method) |
| NL (1) | NL6605188A (en:Method) |
| SE (1) | SE313741B (en:Method) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4478377A (en) * | 1980-12-22 | 1984-10-23 | British Aerospace Public Limited Company | Aircraft |
| GB2188887B (en) * | 1986-04-08 | 1989-11-29 | Rolls Royce Plc | Aircraft with stowable vectorable nozzle and ejector thrust augmentation |
| GB8812978D0 (en) * | 1988-06-01 | 1988-11-16 | British Aerospace | Nozzle assembly for aircraft |
| CN104875898A (zh) * | 2015-06-23 | 2015-09-02 | 中国航空工业集团公司西安飞机设计研究所 | 一种飞机用尾部喷管组件及具有其的飞机 |
| CN111237083B (zh) * | 2018-11-28 | 2022-01-11 | 海鹰航空通用装备有限责任公司 | 组合喷管结构及具有其的飞机 |
-
1966
- 1966-04-14 DE DE19661481554 patent/DE1481554A1/de active Pending
- 1966-04-15 BE BE679612D patent/BE679612A/xx unknown
- 1966-04-18 FR FR58029A patent/FR1506309A/fr not_active Expired
- 1966-04-18 SE SE523966A patent/SE313741B/xx unknown
- 1966-04-19 NL NL6605188A patent/NL6605188A/xx unknown
- 1966-04-19 CH CH562166A patent/CH456357A/de unknown
- 1966-04-19 GB GB1710266A patent/GB1132157A/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| FR1506309A (fr) | 1967-12-22 |
| DE1481554A1 (de) | 1970-01-22 |
| BE679612A (en:Method) | 1966-09-16 |
| CH456357A (de) | 1968-07-15 |
| SE313741B (en:Method) | 1969-08-18 |
| GB1132157A (en) | 1968-10-30 |