AU2003299459A1 - Integrated bypass turbojet engines for aircraft and other vehicles - Google Patents
Integrated bypass turbojet engines for aircraft and other vehicles Download PDFInfo
- Publication number
- AU2003299459A1 AU2003299459A1 AU2003299459A AU2003299459A AU2003299459A1 AU 2003299459 A1 AU2003299459 A1 AU 2003299459A1 AU 2003299459 A AU2003299459 A AU 2003299459A AU 2003299459 A AU2003299459 A AU 2003299459A AU 2003299459 A1 AU2003299459 A1 AU 2003299459A1
- Authority
- AU
- Australia
- Prior art keywords
- air
- turbine
- blades
- turbojet
- compressor
- 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.)
- Abandoned
Links
- 238000002485 combustion reaction Methods 0.000 claims description 107
- 239000007789 gas Substances 0.000 claims description 60
- 239000000446 fuel Substances 0.000 claims description 59
- 239000000567 combustion gas Substances 0.000 claims description 41
- 230000002093 peripheral effect Effects 0.000 claims description 23
- 238000001816 cooling Methods 0.000 claims description 12
- 239000000203 mixture Substances 0.000 claims description 12
- 230000009977 dual effect Effects 0.000 claims description 6
- 230000002441 reversible effect Effects 0.000 claims description 5
- 238000002347 injection Methods 0.000 claims description 4
- 239000007924 injection Substances 0.000 claims description 4
- 238000002156 mixing Methods 0.000 claims description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 3
- 235000008694 Humulus lupulus Nutrition 0.000 claims 1
- 244000025221 Humulus lupulus Species 0.000 claims 1
- 238000007599 discharging Methods 0.000 claims 1
- 238000007906 compression Methods 0.000 description 28
- 230000006835 compression Effects 0.000 description 27
- 239000007858 starting material Substances 0.000 description 13
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 9
- 239000001301 oxygen Substances 0.000 description 9
- 229910052760 oxygen Inorganic materials 0.000 description 9
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 7
- 230000000694 effects Effects 0.000 description 6
- 230000007246 mechanism Effects 0.000 description 5
- 238000006243 chemical reaction Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- 230000006870 function Effects 0.000 description 4
- 230000009467 reduction Effects 0.000 description 4
- 230000009471 action Effects 0.000 description 3
- 230000008901 benefit Effects 0.000 description 3
- 239000003949 liquefied natural gas Substances 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000037361 pathway Effects 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000036961 partial effect Effects 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 230000003321 amplification Effects 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 125000004435 hydrogen atom Chemical class [H]* 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 239000005433 ionosphere Substances 0.000 description 1
- 230000000670 limiting effect Effects 0.000 description 1
- 238000003199 nucleic acid amplification method Methods 0.000 description 1
- 238000011017 operating method Methods 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 230000002829 reductive effect Effects 0.000 description 1
- 230000001172 regenerating effect Effects 0.000 description 1
- 230000008929 regeneration Effects 0.000 description 1
- 238000011069 regeneration method Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 230000000153 supplemental effect Effects 0.000 description 1
- 230000008016 vaporization Effects 0.000 description 1
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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/045—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
- B64C29/0075—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors the motors being tiltable relative to the fuselage
-
- 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
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/022—Blade-carrying members, e.g. rotors with concentric rows of axial blades
-
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
- F02C3/073—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages the compressor and turbine stages being concentric
-
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/08—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/077—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type the plant being of the multiple flow type, i.e. having three or more flows
-
- 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
- Y02T50/40—Weight reduction
-
- 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 (13)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US37261802P | 2002-04-15 | 2002-04-15 | |
| US60/372,618 | 2002-04-15 | ||
| US37473702P | 2002-04-23 | 2002-04-23 | |
| US60/374,737 | 2002-04-23 | ||
| US40546002P | 2002-08-23 | 2002-08-23 | |
| US60/405,460 | 2002-08-23 | ||
| US10/292,892 US6733436B2 (en) | 2002-07-09 | 2002-11-12 | Detachable combination instrument for health-care and treatment |
| US10,292,892 | 2002-11-12 | ||
| US10/337,032 US20030192304A1 (en) | 2002-04-15 | 2003-01-06 | Integrated bypass turbojet engines for aircraft and other vehicles |
| US10/337,032 | 2003-01-06 | ||
| US10/383,462 US6966174B2 (en) | 2002-04-15 | 2003-03-06 | Integrated bypass turbojet engines for air craft and other vehicles |
| US10/383,462 | 2003-03-06 | ||
| PCT/US2003/010855 WO2004092567A2 (en) | 2002-04-15 | 2003-04-09 | Integrated bypass turbojet engines for aircraft and other vehicles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| AU2003299459A1 true AU2003299459A1 (en) | 2004-11-04 |
Family
ID=33304243
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AU2003299459A Abandoned AU2003299459A1 (en) | 2002-04-15 | 2003-04-09 | Integrated bypass turbojet engines for aircraft and other vehicles |
Country Status (4)
| Country | Link |
|---|---|
| EP (1) | EP1534945A4 (de) |
| AU (1) | AU2003299459A1 (de) |
| CA (1) | CA2484580A1 (de) |
| WO (1) | WO2004092567A2 (de) |
Families Citing this family (48)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2006060009A1 (en) | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Turbine blade engine comprising turbine clusters and radial attachment lock arrangement therefor |
| EP1825112B1 (de) | 2004-12-01 | 2013-10-23 | United Technologies Corporation | Freigetragene tipturbinentriebwerk |
| US7921636B2 (en) | 2004-12-01 | 2011-04-12 | United Technologies Corporation | Tip turbine engine and corresponding operating method |
| WO2006060000A1 (en) * | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method |
| US9845727B2 (en) | 2004-12-01 | 2017-12-19 | United Technologies Corporation | Tip turbine engine composite tailcone |
| EP1828568B1 (de) | 2004-12-01 | 2011-03-23 | United Technologies Corporation | Gebläse-turbinen-rotoranordnung für einen spitzenturbinenmotor |
| US8033092B2 (en) | 2004-12-01 | 2011-10-11 | United Technologies Corporation | Tip turbine engine integral fan, combustor, and turbine case |
| US8757959B2 (en) | 2004-12-01 | 2014-06-24 | United Technologies Corporation | Tip turbine engine comprising a nonrotable compartment |
| WO2006060004A1 (en) * | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Combustor for turbine engine |
| WO2006059994A1 (en) * | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Seal assembly for a fan-turbine rotor of a tip turbine engine |
| WO2006059985A1 (en) * | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Axial compressor for tip turbine engine |
| EP1841959B1 (de) | 2004-12-01 | 2012-05-09 | United Technologies Corporation | Ausgewuchtete turbinenrotorlüfterschaufel für einen spitzenturbinenmotor |
| WO2006059989A1 (en) | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Tip turbine engine support structure |
| EP1825117B1 (de) | 2004-12-01 | 2012-06-13 | United Technologies Corporation | Turbinentriebwerk mit von einem differentialgetriebe angetriebenem fan und verdichter |
| WO2006059986A1 (en) | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Tip turbine engine and operating method with reverse core airflow |
| US7854112B2 (en) | 2004-12-01 | 2010-12-21 | United Technologies Corporation | Vectoring transition duct for turbine engine |
| WO2006059993A1 (en) | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Tip turbine engine with multiple fan and turbine stages |
| DE602004019710D1 (de) | 2004-12-01 | 2009-04-09 | United Technologies Corp | Fernbetätigung für eine verstellbare stufe eines verdichters für einen turbinenmotor |
| US8061968B2 (en) | 2004-12-01 | 2011-11-22 | United Technologies Corporation | Counter-rotating compressor case and assembly method for tip turbine engine |
| WO2006112807A2 (en) * | 2004-12-01 | 2006-10-26 | United Technologies Corporation | Turbine engine and method for starting a turbine engine |
| US7883315B2 (en) | 2004-12-01 | 2011-02-08 | United Technologies Corporation | Seal assembly for a fan rotor of a tip turbine engine |
| DE602004028297D1 (de) | 2004-12-01 | 2010-09-02 | United Technologies Corp | Umfangsbrennkammer für spitzenturbinenmotor |
| WO2006060014A1 (en) | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Starter generator system for a tip turbine engine |
| US7631480B2 (en) * | 2004-12-01 | 2009-12-15 | United Technologies Corporation | Modular tip turbine engine |
| US7959406B2 (en) | 2004-12-01 | 2011-06-14 | United Technologies Corporation | Close coupled gearbox assembly for a tip turbine engine |
| US8083030B2 (en) | 2004-12-01 | 2011-12-27 | United Technologies Corporation | Gearbox lubrication supply system for a tip engine |
| EP1834067B1 (de) | 2004-12-01 | 2008-11-26 | United Technologies Corporation | Gebläseschaufelanordnung für ein tip-turbinentriebwerk und montageverfahren |
| EP1819907A2 (de) | 2004-12-01 | 2007-08-22 | United Technologies Corporation | Fanschaufel mit integralem diffusorabschnitt und spitzenturbinenschaufelabschnitt für einen spitzenturbinenmotor |
| DE602004027766D1 (de) | 2004-12-01 | 2010-07-29 | United Technologies Corp | Hydraulische dichtung für ein getriebe eines spitzenturbinenmotors |
| EP1828545A2 (de) | 2004-12-01 | 2007-09-05 | United Technologies Corporation | Ringförmiger turbinenringrotor |
| WO2006059968A1 (en) * | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Counter-rotating gearbox for tip turbine engine |
| EP1825116A2 (de) | 2004-12-01 | 2007-08-29 | United Technologies Corporation | Ejektor-kühlung des aussengehäuses eines tip-turbinen-triebwerks |
| EP1825128B1 (de) | 2004-12-01 | 2011-03-02 | United Technologies Corporation | Regenerative Kühlung einer Leit- und Laufschaufel für ein Tipturbinentriebwerk |
| US8468795B2 (en) | 2004-12-01 | 2013-06-25 | United Technologies Corporation | Diffuser aspiration for a tip turbine engine |
| US8365511B2 (en) | 2004-12-01 | 2013-02-05 | United Technologies Corporation | Tip turbine engine integral case, vane, mount and mixer |
| US8641367B2 (en) | 2004-12-01 | 2014-02-04 | United Technologies Corporation | Plurality of individually controlled inlet guide vanes in a turbofan engine and corresponding controlling method |
| US7976272B2 (en) | 2004-12-01 | 2011-07-12 | United Technologies Corporation | Inflatable bleed valve for a turbine engine |
| US8087885B2 (en) | 2004-12-01 | 2012-01-03 | United Technologies Corporation | Stacked annular components for turbine engines |
| WO2006059987A1 (en) * | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Particle separator for tip turbine engine |
| US9109537B2 (en) | 2004-12-04 | 2015-08-18 | United Technologies Corporation | Tip turbine single plane mount |
| US7201558B2 (en) * | 2005-05-05 | 2007-04-10 | United Technologies Corporation | Seal arrangement for a fan-turbine rotor assembly |
| US20130019585A1 (en) * | 2007-05-11 | 2013-01-24 | Brian Merry | Variable fan inlet guide vane for turbine engine |
| US8967945B2 (en) | 2007-05-22 | 2015-03-03 | United Technologies Corporation | Individual inlet guide vane control for tip turbine engine |
| CN107813947A (zh) * | 2017-11-27 | 2018-03-20 | 大连理工大学 | 一种利用排气续航的混合动力无人飞行器 |
| US10989408B2 (en) | 2018-09-13 | 2021-04-27 | Raytheon Technologies Corporation | Additive integral combustor expansion spring |
| CN111332477B (zh) * | 2020-02-21 | 2022-09-20 | 中国电子科技集团公司第二十九研究所 | 一种逆升压涡轮旁路控制装置及方法 |
| US11549463B2 (en) * | 2021-02-22 | 2023-01-10 | General Electric Company | Compact low-pressure compressor |
| CN116677498B (zh) * | 2023-08-03 | 2023-10-17 | 中国航发四川燃气涡轮研究院 | 基于氢能的新型高超声速组合发动机 |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2404767A (en) * | 1941-10-28 | 1946-07-23 | Armstrong Siddeley Motors Ltd | Jet propulsion plant |
| US2611241A (en) * | 1946-03-19 | 1952-09-23 | Packard Motor Car Co | Power plant comprising a toroidal combustion chamber and an axial flow gas turbine with blade cooling passages therein forming a centrifugal air compressor |
| US2694291A (en) * | 1948-02-07 | 1954-11-16 | Henning C Rosengart | Rotor and combustion chamber arrangement for gas turbines |
| US3112610A (en) * | 1961-02-27 | 1963-12-03 | Joseph J Jerger | Constant pressure shrouded propeller |
| US3283509A (en) * | 1963-02-21 | 1966-11-08 | Messerschmitt Boelkow Blohm | Lifting engine for vtol aircraft |
| US3606210A (en) * | 1969-11-06 | 1971-09-20 | Ralph E Busby | Engine mounting for vtol aircraft and the like |
| FR2076450A5 (de) * | 1970-01-15 | 1971-10-15 | Snecma | |
| US3603082A (en) * | 1970-02-18 | 1971-09-07 | Curtiss Wright Corp | Combustor for gas turbine having a compressor and turbine passages in a single rotor element |
| GB1361036A (en) * | 1971-11-05 | 1974-07-24 | Hansford R J | Gas turbine ducted fan propulsion unit |
| US3899886A (en) * | 1973-11-19 | 1975-08-19 | Gen Motors Corp | Gas turbine engine control |
| US4860537A (en) * | 1986-08-29 | 1989-08-29 | Brandt, Inc. | High bypass ratio counterrotating gearless front fan engine |
-
2003
- 2003-04-09 WO PCT/US2003/010855 patent/WO2004092567A2/en not_active Application Discontinuation
- 2003-04-09 EP EP03799749A patent/EP1534945A4/de not_active Withdrawn
- 2003-04-09 CA CA002484580A patent/CA2484580A1/en not_active Abandoned
- 2003-04-09 AU AU2003299459A patent/AU2003299459A1/en not_active Abandoned
Also Published As
| Publication number | Publication date |
|---|---|
| WO2004092567A2 (en) | 2004-10-28 |
| EP1534945A2 (de) | 2005-06-01 |
| CA2484580A1 (en) | 2004-10-28 |
| WO2004092567A3 (en) | 2005-04-07 |
| EP1534945A4 (de) | 2006-08-30 |
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