BE762094A - Circuit de carburant pour moteur d'aeronef - Google Patents
Circuit de carburant pour moteur d'aeronefInfo
- Publication number
- BE762094A BE762094A BE762094A BE762094A BE762094A BE 762094 A BE762094 A BE 762094A BE 762094 A BE762094 A BE 762094A BE 762094 A BE762094 A BE 762094A BE 762094 A BE762094 A BE 762094A
- Authority
- BE
- Belgium
- Prior art keywords
- fuel system
- aircraft engine
- engine fuel
- aircraft
- fuel
- Prior art date
Links
- 239000000446 fuel Substances 0.000 title 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
- B64D37/14—Filling or emptying
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Details Of Reciprocating Pumps (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US3007370A | 1970-04-20 | 1970-04-20 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE762094A true BE762094A (fr) | 1971-07-01 |
Family
ID=21852358
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE762094A BE762094A (fr) | 1970-04-20 | 1971-01-27 | Circuit de carburant pour moteur d'aeronef |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US3627239A (fr) |
| BE (1) | BE762094A (fr) |
| CA (1) | CA918936A (fr) |
| DE (1) | DE2107166A1 (fr) |
| FR (1) | FR2086184B1 (fr) |
| GB (1) | GB1332072A (fr) |
Families Citing this family (19)
| 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 |
| US4038817A (en) * | 1975-06-02 | 1977-08-02 | General Electric Company | Fuel jettison system |
| 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 |
| GB1559828A (en) * | 1975-09-12 | 1980-01-30 | Rolls Royce | Fuel system for gas turbine engines |
| US4339917A (en) * | 1979-06-13 | 1982-07-20 | The Garrett Corporation | Fuel delivery system and method |
| GB2208411B (en) * | 1987-06-25 | 1990-10-31 | Plessey Co Plc | Rotary pump system |
| US5558303A (en) * | 1994-12-27 | 1996-09-24 | Koethe; Terence L. | Method and apparatus for using hot fuels to de-ice aircraft |
| US7051979B2 (en) * | 2004-01-29 | 2006-05-30 | The Boeing Company | Auxiliary fuel tank systems for aircraft and methods for their manufacture and use |
| US7458543B2 (en) | 2005-06-10 | 2008-12-02 | The Boeing Company | Aerial refueling system |
| GB0518576D0 (en) * | 2005-09-12 | 2005-10-19 | Airbus Uk Ltd | Improvements in and relating to aircraft wings and fuel tanks |
| US7337795B2 (en) * | 2005-10-17 | 2008-03-04 | The Boeing Company | Fuel balancing system |
| GB0917879D0 (en) * | 2009-10-13 | 2009-11-25 | Airbus Uk Ltd | Aircraft fuel system |
| US8956130B2 (en) * | 2009-12-23 | 2015-02-17 | Pentair Flow Technologies, Llc | Redundant sump pump system |
| JP6044140B2 (ja) * | 2012-07-06 | 2016-12-14 | 株式会社Ihi | 航空機エンジンの燃料供給装置 |
| JP6131785B2 (ja) * | 2013-08-30 | 2017-05-24 | 株式会社Ihi | 航空機エンジンの燃料供給装置 |
| CN105620771A (zh) * | 2014-10-28 | 2016-06-01 | 中国航空工业集团公司西安飞机设计研究所 | 一种双发涡桨飞机供输油系统 |
| US11186383B2 (en) | 2019-04-02 | 2021-11-30 | Hamilton Sundstrand Corporation | Centrifugal fuel pump ice prevention |
| CN115743569B (zh) * | 2022-11-17 | 2025-06-13 | 中国直升机设计研究所 | 一种可进行预检的压力加油切断系统 |
-
1970
- 1970-04-20 US US30073A patent/US3627239A/en not_active Expired - Lifetime
-
1971
- 1971-01-12 GB GB143371A patent/GB1332072A/en not_active Expired
- 1971-01-27 BE BE762094A patent/BE762094A/fr unknown
- 1971-02-03 FR FR7103628A patent/FR2086184B1/fr not_active Expired
- 1971-02-10 CA CA104948A patent/CA918936A/en not_active Expired
- 1971-02-15 DE DE19712107166 patent/DE2107166A1/de active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| DE2107166A1 (de) | 1971-11-11 |
| FR2086184A1 (fr) | 1971-12-31 |
| US3627239A (en) | 1971-12-14 |
| CA918936A (en) | 1973-01-16 |
| GB1332072A (en) | 1973-10-03 |
| FR2086184B1 (fr) | 1973-11-23 |
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