BE530004A - - Google Patents
Info
- Publication number
- BE530004A BE530004A BE530004DA BE530004A BE 530004 A BE530004 A BE 530004A BE 530004D A BE530004D A BE 530004DA BE 530004 A BE530004 A BE 530004A
- Authority
- BE
- Belgium
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
- F02K1/78—Other construction of jet pipes
- F02K1/82—Jet pipe walls, e.g. liners
- F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/06—Fluid supply conduits to nozzles or the like
- F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
-
- 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
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/08—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone
-
- 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
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/09—Varying effective area of jet pipe or nozzle by axially moving an external member, e.g. a shroud
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- 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)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Supercharger (AREA)
- Exhaust Silencers (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US365005A US2811827A (en) | 1953-06-30 | 1953-06-30 | Balanced jet nozzle and cooling means therefor |
Publications (1)
Publication Number | Publication Date |
---|---|
BE530004A true BE530004A (fr) |
Family
ID=23437091
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE530004D BE530004A (fr) | 1953-06-30 |
Country Status (4)
Country | Link |
---|---|
US (1) | US2811827A (fr) |
BE (1) | BE530004A (fr) |
FR (1) | FR1104307A (fr) |
GB (1) | GB756783A (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE977738C (de) * | 1957-12-11 | 1969-03-27 | Josef Schaberger & Co G M B H | Verfahren zum Betreiben eines Strahlantriebes, insbesondere fuer Raketen |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2952124A (en) * | 1957-07-29 | 1960-09-13 | Boeing Co | Plug type noise suppressor and thrust reverser |
US3094072A (en) * | 1957-12-09 | 1963-06-18 | Arthur R Parilla | Aircraft, missiles, missile weapons systems, and space ships |
US4044555A (en) * | 1958-09-30 | 1977-08-30 | Hayes International Corporation | Rear section of jet power plant installations |
US3237864A (en) * | 1962-12-03 | 1966-03-01 | Gen Electric | Low drag variable plug jet exhaust nozzle |
US3192712A (en) * | 1962-12-31 | 1965-07-06 | Gen Electric | Load balancing arrangement for annular variable area jet exhaust nozzle |
US3504860A (en) * | 1964-07-07 | 1970-04-07 | Us Navy | Adjustable spike nozzle for thrust motors |
GB1026068A (en) * | 1964-11-09 | 1966-04-14 | Rolls Royce | Jet nozzle |
US3210934A (en) * | 1964-11-30 | 1965-10-12 | Gen Motors Corp | Jet engine exhaust |
GB1035015A (en) * | 1965-05-11 | 1966-07-06 | Rolls Royce | Improvements in or relating to jet propulsion power plant |
DE4225603C1 (de) * | 1992-08-03 | 1993-11-25 | Deutsche Aerospace | Schubdüse für ein Hyperschall-Kombinationstriebwerk mit gekühltem Zentralkörper |
US6584766B1 (en) * | 2000-03-24 | 2003-07-01 | General Electric Co. | Methods and apparatus for minimizing thermal stresses in a centerbody |
FR2920194B1 (fr) * | 2007-08-23 | 2014-02-21 | Airbus France | Cone d'ejection des gaz pour turboreacteur d'aeronef equipe d'un dispositif de generation de turbulences de flux primaire limitant le bruit de jet |
CN110657044B (zh) * | 2019-08-30 | 2020-09-25 | 中国科学院工程热物理研究所 | 一种电驱式加力燃烧室与可调面积尾喷管一体化结构 |
CN113266425B (zh) * | 2021-05-31 | 2022-11-01 | 张龙 | 一种封闭固定式环形涡喷蒸汽轮 |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2510506A (en) * | 1944-07-15 | 1950-06-06 | Jarvis C Marble | Turbojet power plant with controllable primary and secondary outlets |
NL70849C (fr) * | 1945-05-14 | |||
US2570629A (en) * | 1945-10-05 | 1951-10-09 | Anxionnaz | Adjustable pipe for the intake of air and expansion of the driving gases in reactionjet propellers for projectiles and vehicles |
US2540594A (en) * | 1946-08-23 | 1951-02-06 | Lockheed Aircraft Corp | Ram jet engine having variable area inlets |
US2573982A (en) * | 1946-12-14 | 1951-11-06 | Homestead Valve Mfg Co | Nozzle |
BE637917A (fr) * | 1947-06-05 | |||
US2641104A (en) * | 1950-04-18 | 1953-06-09 | United Aircraft Corp | Tail cone having radially adjustable wall |
US2630673A (en) * | 1950-09-27 | 1953-03-10 | Gen Electric | Cooling means for variable area nozzles |
-
0
- BE BE530004D patent/BE530004A/xx unknown
-
1953
- 1953-06-30 US US365005A patent/US2811827A/en not_active Expired - Lifetime
-
1954
- 1954-05-03 GB GB12763/54A patent/GB756783A/en not_active Expired
- 1954-06-22 FR FR1104307D patent/FR1104307A/fr not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE977738C (de) * | 1957-12-11 | 1969-03-27 | Josef Schaberger & Co G M B H | Verfahren zum Betreiben eines Strahlantriebes, insbesondere fuer Raketen |
Also Published As
Publication number | Publication date |
---|---|
US2811827A (en) | 1957-11-05 |
GB756783A (en) | 1956-09-12 |
FR1104307A (fr) | 1955-11-18 |