BE693994A - - Google Patents
Info
- Publication number
- BE693994A BE693994A BE693994DA BE693994A BE 693994 A BE693994 A BE 693994A BE 693994D A BE693994D A BE 693994DA BE 693994 A BE693994 A BE 693994A
- Authority
- BE
- Belgium
Links
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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/16—Aircraft characterised by the type or position of power plants of jet type
- B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
-
- 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
- F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/60—Mounting; Assembling; Disassembling
- F04D29/64—Mounting; Assembling; Disassembling of axial pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/60—Mounting; Assembling; Disassembling
- F04D29/64—Mounting; Assembling; Disassembling of axial pumps
- F04D29/644—Mounting; Assembling; Disassembling of axial pumps especially adapted for elastic fluid pumps
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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)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US552755A US3398535A (en) | 1966-05-25 | 1966-05-25 | Engine supporting structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE693994A true BE693994A (US07488766-20090210-C00029.png) | 1967-07-17 |
Family
ID=24206666
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE693994D BE693994A (US07488766-20090210-C00029.png) | 1966-05-25 | 1967-02-13 |
Country Status (5)
Families Citing this family (36)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3494129A (en) * | 1968-03-06 | 1970-02-10 | Gen Electric | Fluid compressors and turbofan engines employing same |
| GB1294324A (en) * | 1969-05-03 | 1972-10-25 | Dowty Rotol Ltd | Engine installations |
| US3830058A (en) * | 1973-02-26 | 1974-08-20 | Avco Corp | Fan engine mounting |
| GB1533551A (en) * | 1974-11-08 | 1978-11-29 | Gen Electric | Gas turbofan engines |
| US4571936A (en) * | 1985-07-10 | 1986-02-25 | The United States Of America As Represented By The Secretary Of The Air Force | Length adjustable strut link with low aerodynamic drag |
| US4722184A (en) * | 1985-10-03 | 1988-02-02 | United Technologies Corporation | Annular stator structure for a rotary machine |
| US4820117A (en) * | 1987-07-09 | 1989-04-11 | United Technologies Corporation | Crossed I-beam structural strut |
| CA2021087A1 (en) * | 1989-09-07 | 1991-03-08 | Eugene J. Antuna | Ultra high bypass engine integrated fan/cowl and transportation/removal |
| US5161947A (en) * | 1991-05-08 | 1992-11-10 | United Technologies Corporation | Fan case strut for turbomachine |
| US5224341A (en) * | 1992-01-06 | 1993-07-06 | United Technologies Corporation | Separable fan strut for a gas turbofan powerplant |
| WO1992019854A1 (en) * | 1991-05-08 | 1992-11-12 | United Technologies Corporation | Separable fan strut for a gas turbofan powerplant |
| US5609467A (en) * | 1995-09-28 | 1997-03-11 | Cooper Cameron Corporation | Floating interturbine duct assembly for high temperature power turbine |
| JPH11247605A (ja) | 1997-12-26 | 1999-09-14 | United Technol Corp <Utc> | タ―ボマシ―ンコンポ―ネントの振動緩衝方法及び装置 |
| GB0328671D0 (en) * | 2003-12-11 | 2004-01-14 | Rolls Royce Plc | Aircraft engine mounting |
| US7124572B2 (en) * | 2004-09-14 | 2006-10-24 | Honeywell International, Inc. | Recuperator and turbine support adapter for recuperated gas turbine engines |
| GB0520850D0 (en) * | 2005-10-14 | 2005-11-23 | Rolls Royce Plc | Fan static structure |
| BRPI0708547B1 (pt) * | 2006-03-03 | 2018-02-06 | Dresser-Rand Company | Dispositivo de processamento de fluido multifásico |
| FR2925121B1 (fr) * | 2007-12-18 | 2014-07-04 | Snecma | Carter intermediaire pour turboreacteur d'aeronef a conception amelioree |
| FR2928181B1 (fr) * | 2008-02-28 | 2010-04-02 | Airbus France | Ensemble moteur pour aeronef comprenant un turboreacteur avec des structures de renfort reliant le carter de soufflante au carter central. |
| FR2928136B1 (fr) * | 2008-02-28 | 2010-04-02 | Airbus France | Ensemble moteur pour aeronef comprenant des attaches moteur deportees vers le bas sur le carter de soufflante. |
| FR2933130B1 (fr) * | 2008-06-25 | 2012-02-24 | Snecma | Carter structural pour turbomachine |
| GB2468485A (en) * | 2009-03-09 | 2010-09-15 | Aircelle Ltd | Turbine engine support arm |
| US8316523B2 (en) | 2009-10-01 | 2012-11-27 | Pratt & Whitney Canada Corp. | Method for centering engine structures |
| US8784050B2 (en) * | 2010-06-15 | 2014-07-22 | Rolls-Royce Corporation | Aggregate vane assembly |
| US20130084174A1 (en) * | 2011-10-03 | 2013-04-04 | United Technologies Corporation | Strut rods for structural guide vanes |
| FR2988777B1 (fr) * | 2012-03-29 | 2014-04-25 | Snecma Propulsion Solide | Integration de pieces d'arriere-corps de moteur aeronautique |
| US9163525B2 (en) * | 2012-06-27 | 2015-10-20 | United Technologies Corporation | Turbine wheel catcher |
| US10227895B2 (en) * | 2013-12-20 | 2019-03-12 | Pratt & Whitney Canada Corp. | Gas turbine case and reinforcement strut for same |
| US20160201516A1 (en) * | 2015-01-09 | 2016-07-14 | United Technologies Corporation | Gas turbine engine mid-turbine frame tie rod arrangement |
| GB201803571D0 (en) * | 2018-03-06 | 2018-04-18 | Rolls Royce Plc | Component |
| CN113443124B (zh) * | 2021-07-20 | 2022-08-19 | 北京理工大学 | 采用两级大小叶片的边界层吸入式推进器 |
| US11555420B1 (en) | 2021-08-20 | 2023-01-17 | Raytheon Technologies Corporation | Frame connection between fan case and core housing in a gas turbine engine |
| US11674415B2 (en) | 2021-08-20 | 2023-06-13 | Raytheon Technologies Corporation | Front section stiffness ratio |
| US11708772B2 (en) | 2021-11-12 | 2023-07-25 | Raytheon Technologies Corporation | Triangular-frame connection between fan case and core housing in a gas turbine engine |
| US11608796B1 (en) | 2021-11-12 | 2023-03-21 | Raytheon Technologies Corporation | Radial strut frame connection between fan case and core housing in a gas turbine engine |
| US11686220B2 (en) | 2021-11-12 | 2023-06-27 | Raytheon Technologies Corporation | H-frame connection between fan case and core housing in a gas turbine engine |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3070285A (en) * | 1959-11-26 | 1962-12-25 | Rolls Royce | Gas turbine engine |
| US3262270A (en) * | 1965-06-07 | 1966-07-26 | Gen Electric | Thrust reverser |
-
1966
- 1966-05-25 US US552755A patent/US3398535A/en not_active Expired - Lifetime
-
1967
- 1967-02-13 BE BE693994D patent/BE693994A/xx unknown
- 1967-02-17 DE DE19671626084 patent/DE1626084A1/de active Pending
- 1967-02-22 GB GB8365/67A patent/GB1151613A/en not_active Expired
- 1967-02-24 FR FR96362A patent/FR1516333A/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| FR1516333A (fr) | 1968-03-08 |
| DE1626084A1 (de) | 1971-05-13 |
| GB1151613A (en) | 1969-05-14 |
| US3398535A (en) | 1968-08-27 |
