FR1241003A - Jet engine for supersonic aircraft - Google Patents
Jet engine for supersonic aircraftInfo
- Publication number
- FR1241003A FR1241003A FR810926A FR810926A FR1241003A FR 1241003 A FR1241003 A FR 1241003A FR 810926 A FR810926 A FR 810926A FR 810926 A FR810926 A FR 810926A FR 1241003 A FR1241003 A FR 1241003A
- Authority
- FR
- France
- Prior art keywords
- jet engine
- supersonic aircraft
- supersonic
- aircraft
- 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
- 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
-
- 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
- F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
- F02K3/105—Heating the by-pass flow
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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 |
---|---|---|---|
FR810926A FR1241003A (en) | 1959-11-23 | 1959-11-23 | Jet engine for supersonic aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR810926A FR1241003A (en) | 1959-11-23 | 1959-11-23 | Jet engine for supersonic aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1241003A true FR1241003A (en) | 1960-09-09 |
Family
ID=8721635
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR810926A Expired FR1241003A (en) | 1959-11-23 | 1959-11-23 | Jet engine for supersonic aircraft |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1241003A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2006105138A (en) * | 2004-09-30 | 2006-04-20 | General Electric Co <Ge> | Method and apparatus for assembling gas turbine engine |
-
1959
- 1959-11-23 FR FR810926A patent/FR1241003A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2006105138A (en) * | 2004-09-30 | 2006-04-20 | General Electric Co <Ge> | Method and apparatus for assembling gas turbine engine |
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