FR1075248A - Improvements to thermopropulsive nozzles - Google Patents
Improvements to thermopropulsive nozzlesInfo
- Publication number
- FR1075248A FR1075248A FR1075248DA FR1075248A FR 1075248 A FR1075248 A FR 1075248A FR 1075248D A FR1075248D A FR 1075248DA FR 1075248 A FR1075248 A FR 1075248A
- Authority
- FR
- France
- Prior art keywords
- thermopropulsive
- nozzles
- thermopropulsive nozzles
- 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
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/08—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being continuous
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
-
- 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)
- Physics & Mathematics (AREA)
- Geometry (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1075248T | 1952-12-31 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1075248A true FR1075248A (en) | 1954-10-14 |
Family
ID=9607034
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1075248D Expired FR1075248A (en) | 1952-12-31 | 1952-12-31 | Improvements to thermopropulsive nozzles |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE1069952C2 (en) |
FR (1) | FR1075248A (en) |
GB (1) | GB777570A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2997229A (en) * | 1959-10-06 | 1961-08-22 | Means for removing moisture from a surface | |
US2997843A (en) * | 1958-04-23 | 1961-08-29 | Bendix Corp | Inlet control system for supersonic aircraft |
US3011307A (en) * | 1955-12-15 | 1961-12-05 | Gen Electric | Variable throat supersonic diffuser |
US3030770A (en) * | 1957-07-30 | 1962-04-24 | United Aircraft Corp | Variable supersonic inlet |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1086491B (en) * | 1958-03-29 | 1960-08-04 | Bmw Triebwerkbau Ges M B H | Control device for jet engines with supersonic flight speed, especially ramjet engines |
DE1121414B (en) * | 1958-07-24 | 1962-01-04 | Ernst Heinkel Flugzeugbau G M | Device for controlling additional air in a jet engine |
DE1228859B (en) * | 1963-03-29 | 1966-11-17 | Ver Flugtechnische Werke Ges M | Supersonic inlet for jet engines of missiles surrounded by a jacket pipe |
CN113153531B (en) * | 2021-05-28 | 2022-09-27 | 西北工业大学 | Variable overflow groove adjusting mechanism, scramjet engine and hypersonic aircraft |
-
1952
- 1952-12-31 FR FR1075248D patent/FR1075248A/en not_active Expired
-
1953
- 1953-12-19 DE DE1953L0017493 patent/DE1069952C2/en not_active Expired
- 1953-12-31 GB GB36361/53A patent/GB777570A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3011307A (en) * | 1955-12-15 | 1961-12-05 | Gen Electric | Variable throat supersonic diffuser |
US3030770A (en) * | 1957-07-30 | 1962-04-24 | United Aircraft Corp | Variable supersonic inlet |
US2997843A (en) * | 1958-04-23 | 1961-08-29 | Bendix Corp | Inlet control system for supersonic aircraft |
US2997229A (en) * | 1959-10-06 | 1961-08-22 | Means for removing moisture from a surface |
Also Published As
Publication number | Publication date |
---|---|
GB777570A (en) | 1957-06-26 |
DE1069952C2 (en) | 1960-05-12 |
DE1069952B (en) | 1959-11-26 |
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