FR1291561A - Obturateur à papillons pour tri-réacteurs - Google Patents
Obturateur à papillons pour tri-réacteursInfo
- Publication number
- FR1291561A FR1291561A FR846375A FR846375A FR1291561A FR 1291561 A FR1291561 A FR 1291561A FR 846375 A FR846375 A FR 846375A FR 846375 A FR846375 A FR 846375A FR 1291561 A FR1291561 A FR 1291561A
- Authority
- FR
- France
- Prior art keywords
- reactors
- tri
- butterfly shutter
- butterfly
- shutter
- 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
- 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
-
- 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
- F02K3/062—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 with aft fan
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR846375A FR1291561A (fr) | 1960-12-02 | 1960-12-02 | Obturateur à papillons pour tri-réacteurs |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR846375A FR1291561A (fr) | 1960-12-02 | 1960-12-02 | Obturateur à papillons pour tri-réacteurs |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1291561A true FR1291561A (fr) | 1962-04-27 |
Family
ID=8744369
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR846375A Expired FR1291561A (fr) | 1960-12-02 | 1960-12-02 | Obturateur à papillons pour tri-réacteurs |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1291561A (fr) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1294222B (de) * | 1964-04-23 | 1969-04-30 | Bristol Siddeley Engines Ltd | Senkrecht startendes und landendes Flugzeug |
EP0076794A1 (fr) * | 1981-04-22 | 1983-04-20 | Boeing Co | Reacteur supersonique et procede de fonctionnement. |
FR2550821A1 (fr) * | 1983-08-18 | 1985-02-22 | Snecma | Dispositif variateur du flux secondaire d'un turboreacteur multiflux |
-
1960
- 1960-12-02 FR FR846375A patent/FR1291561A/fr not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1294222B (de) * | 1964-04-23 | 1969-04-30 | Bristol Siddeley Engines Ltd | Senkrecht startendes und landendes Flugzeug |
EP0076794A1 (fr) * | 1981-04-22 | 1983-04-20 | Boeing Co | Reacteur supersonique et procede de fonctionnement. |
EP0076794A4 (fr) * | 1981-04-22 | 1983-08-17 | Boeing Co | Reacteur supersonique et procede de fonctionnement. |
FR2550821A1 (fr) * | 1983-08-18 | 1985-02-22 | Snecma | Dispositif variateur du flux secondaire d'un turboreacteur multiflux |
EP0135430A1 (fr) * | 1983-08-18 | 1985-03-27 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." | Dispositif variateur du flux secondaire d'un turboréacteur multiflux |
US4638631A (en) * | 1983-08-18 | 1987-01-27 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." | Multiflow turbo jet engine secondary flow adjusting device |
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