FR1288602A - Propulseur à réaction - Google Patents
Propulseur à réactionInfo
- Publication number
- FR1288602A FR1288602A FR860986A FR860986A FR1288602A FR 1288602 A FR1288602 A FR 1288602A FR 860986 A FR860986 A FR 860986A FR 860986 A FR860986 A FR 860986A FR 1288602 A FR1288602 A FR 1288602A
- Authority
- FR
- France
- Prior art keywords
- jet thruster
- thruster
- jet
- Prior art date
- 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.)
- Expired
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
- 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
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/075—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type controlling flow ratio between flows
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR860986A FR1288602A (fr) | 1960-05-06 | 1961-05-05 | Propulseur à réaction |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3130543X | 1960-05-06 | ||
| FR860986A FR1288602A (fr) | 1960-05-06 | 1961-05-05 | Propulseur à réaction |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| FR1288602A true FR1288602A (fr) | 1962-03-24 |
Family
ID=26190414
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR860986A Expired FR1288602A (fr) | 1960-05-06 | 1961-05-05 | Propulseur à réaction |
Country Status (1)
| Country | Link |
|---|---|
| FR (1) | FR1288602A (fr) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1225445B (de) * | 1964-02-05 | 1966-09-22 | Rolls Royce | Nebenschluss-Gasturbinenstrahltriebwerk |
| DE1287366B (de) * | 1963-07-15 | 1969-01-16 | Rolls Royce | Mantelstrom-Gasturbinenstrahltriebwerk |
| FR2669680A1 (fr) * | 1986-06-21 | 1992-05-29 | British Aerospace | Prefectionnements apportes a des moteurs a turbine a gaz ou les concernants. |
-
1961
- 1961-05-05 FR FR860986A patent/FR1288602A/fr not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1287366B (de) * | 1963-07-15 | 1969-01-16 | Rolls Royce | Mantelstrom-Gasturbinenstrahltriebwerk |
| DE1225445B (de) * | 1964-02-05 | 1966-09-22 | Rolls Royce | Nebenschluss-Gasturbinenstrahltriebwerk |
| FR2669680A1 (fr) * | 1986-06-21 | 1992-05-29 | British Aerospace | Prefectionnements apportes a des moteurs a turbine a gaz ou les concernants. |
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