BE685448A - - Google Patents
Info
- Publication number
- BE685448A BE685448A BE685448DA BE685448A BE 685448 A BE685448 A BE 685448A BE 685448D A BE685448D A BE 685448DA BE 685448 A BE685448 A BE 685448A
- Authority
- BE
- Belgium
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
- F02C7/12—Cooling of plants
- F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
-
- 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
- F02C7/22—Fuel supply systems
- F02C7/236—Fuel delivery systems comprising two or more pumps
- F02C7/2365—Fuel delivery systems comprising two or more pumps comprising an air supply system for the atomisation of fuel
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
- F23R3/32—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices being tubular
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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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Feeding And Controlling Fuel (AREA)
- Fuel-Injection Apparatus (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US148935A US3307355A (en) | 1961-10-31 | 1961-10-31 | Augmentation system for reaction engine using liquid fuel for cooling |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE685448A true BE685448A (US07534539-20090519-C00280.png) | 1967-01-16 |
Family
ID=22528096
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE685448D BE685448A (US07534539-20090519-C00280.png) | 1961-10-31 | 1966-08-12 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US3307355A (US07534539-20090519-C00280.png) |
| BE (1) | BE685448A (US07534539-20090519-C00280.png) |
| CH (1) | CH444576A (US07534539-20090519-C00280.png) |
| GB (1) | GB1140272A (US07534539-20090519-C00280.png) |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3779007A (en) * | 1972-04-28 | 1973-12-18 | Gen Electric | Fuel delivery and control system for a gas turbine engine |
| US3916621A (en) * | 1972-08-18 | 1975-11-04 | Cosmo Carleton Amenta | Pulse-jet engine with variable volume combustion chamber |
| US4020632A (en) * | 1975-07-17 | 1977-05-03 | The United States Of America As Represented By The United States National Aeronautics And Space Administration Office Of General Counsel-Code Gp | Oil cooling system for a gas turbine engine |
| US4041697A (en) * | 1975-07-17 | 1977-08-16 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Oil cooling system for a gas turbine engine |
| US5099644A (en) * | 1990-04-04 | 1992-03-31 | General Electric Company | Lean staged combustion assembly |
| FR2697289B1 (fr) * | 1992-10-28 | 1994-12-09 | Snecma | Turboréacteur à double flux avec système de réchauffement d'air sur la tuyère primaire. |
| US5845481A (en) * | 1997-01-24 | 1998-12-08 | Westinghouse Electric Corporation | Combustion turbine with fuel heating system |
| US6105370A (en) * | 1998-08-18 | 2000-08-22 | Hamilton Sundstrand Corporation | Method and apparatus for rejecting waste heat from a system including a combustion engine |
| RU2197630C1 (ru) * | 2002-03-15 | 2003-01-27 | Федеральное государственное унитарное предприятие "Исследовательский Центр им. М.В. Келдыша" | Солнечный тепловой ракетный двигатель и способ его работы |
| US6935117B2 (en) * | 2003-10-23 | 2005-08-30 | United Technologies Corporation | Turbine engine fuel injector |
| GB2443429A (en) * | 2005-09-24 | 2008-05-07 | Siemens Ind Turbomachinery Ltd | Fuel Vaporisation Within a Burner Associated With a Combustion Chamber |
| CN105716120B (zh) * | 2016-02-22 | 2018-02-16 | 中国科学院工程热物理研究所 | 一种燃油冷却式蒸发管结构 |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US780493A (en) * | 1904-03-24 | 1905-01-24 | Nicholas P Carver | Mercury-feeder for stamper-batteries, &c. |
| US2955420A (en) * | 1955-09-12 | 1960-10-11 | Phillips Petroleum Co | Jet engine operation |
| US2907527A (en) * | 1956-04-10 | 1959-10-06 | Thompson Ramo Wooldridge Inc | Nozzle |
| US3000176A (en) * | 1957-04-05 | 1961-09-19 | United Aircraft Corp | Ducted fan engine |
| US3024606A (en) * | 1958-07-10 | 1962-03-13 | Curtiss Wright Corp | Liquid cooling system for jet engines |
| US3052095A (en) * | 1959-09-11 | 1962-09-04 | Gen Motors Corp | Liquid vapor fuel system |
-
1961
- 1961-10-31 US US148935A patent/US3307355A/en not_active Expired - Lifetime
-
1966
- 1966-08-03 GB GB34781/66A patent/GB1140272A/en not_active Expired
- 1966-08-12 BE BE685448D patent/BE685448A/xx unknown
- 1966-08-12 CH CH1166466A patent/CH444576A/de unknown
Also Published As
| Publication number | Publication date |
|---|---|
| US3307355A (en) | 1967-03-07 |
| GB1140272A (en) | 1969-01-15 |
| CH444576A (de) | 1967-09-30 |
