DE3909050C1 - - Google Patents
Info
- Publication number
- DE3909050C1 DE3909050C1 DE3909050A DE3909050A DE3909050C1 DE 3909050 C1 DE3909050 C1 DE 3909050C1 DE 3909050 A DE3909050 A DE 3909050A DE 3909050 A DE3909050 A DE 3909050A DE 3909050 C1 DE3909050 C1 DE 3909050C1
- Authority
- DE
- Germany
- Prior art keywords
- turbine
- rocket
- engine
- turbo
- 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.)
- Expired - Lifetime
Links
- 239000007789 gas Substances 0.000 claims description 46
- 239000000446 fuel Substances 0.000 claims description 25
- 238000002485 combustion reaction Methods 0.000 claims description 24
- 239000003380 propellant Substances 0.000 claims description 15
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 claims description 7
- 239000001257 hydrogen Substances 0.000 claims description 3
- 229910052739 hydrogen Inorganic materials 0.000 claims description 3
- 125000004435 hydrogen atom Chemical class [H]* 0.000 claims description 3
- 239000007788 liquid Substances 0.000 claims description 2
- 238000011144 upstream manufacturing Methods 0.000 claims description 2
- 230000001419 dependent effect Effects 0.000 claims 1
- 239000003570 air Substances 0.000 description 36
- 238000010276 construction Methods 0.000 description 4
- 230000008878 coupling Effects 0.000 description 3
- 238000010168 coupling process Methods 0.000 description 3
- 238000005859 coupling reaction Methods 0.000 description 3
- 239000012080 ambient air Substances 0.000 description 2
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 2
- 239000007800 oxidant agent Substances 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 230000029058 respiratory gaseous exchange Effects 0.000 description 2
- 206010010219 Compulsions Diseases 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000005422 blasting Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 108090000623 proteins and genes Proteins 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000007306 turnover Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/401—Liquid propellant rocket engines
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/4005—Air-breathing propulsion
-
- 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
- F02C3/13—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having variable working fluid interconnections between turbines or compressors or stages of different rotors
-
- 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
- F02K3/072—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 with counter-rotating, e.g. fan rotors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
- F02K7/16—Composite ram-jet/turbo-jet engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
- F02K7/18—Composite ram-jet/rocket engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/74—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant
- F02K9/78—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with an air-breathing jet-propulsion plant
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/402—Propellant tanks; Feeding propellants
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3909050A DE3909050C1 (US06168776-20010102-C00041.png) | 1989-03-18 | 1989-03-18 | |
EP90102216A EP0388613B1 (de) | 1989-03-18 | 1990-02-05 | Kombinationsantrieb für Fluggeschwindigkeiten von Unter - bis Hyperschall |
DE9090102216T DE59000220D1 (de) | 1989-03-18 | 1990-02-05 | Kombinationsantrieb fuer fluggeschwindigkeiten von unter - bis hyperschall. |
JP2064473A JPH076455B2 (ja) | 1989-03-18 | 1990-03-16 | 組合せ式駆動装置 |
US07/494,990 US5014508A (en) | 1989-03-18 | 1990-03-16 | Combination propulsion system for a flying craft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3909050A DE3909050C1 (US06168776-20010102-C00041.png) | 1989-03-18 | 1989-03-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3909050C1 true DE3909050C1 (US06168776-20010102-C00041.png) | 1990-08-16 |
Family
ID=6376739
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE3909050A Expired - Lifetime DE3909050C1 (US06168776-20010102-C00041.png) | 1989-03-18 | 1989-03-18 | |
DE9090102216T Expired - Fee Related DE59000220D1 (de) | 1989-03-18 | 1990-02-05 | Kombinationsantrieb fuer fluggeschwindigkeiten von unter - bis hyperschall. |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE9090102216T Expired - Fee Related DE59000220D1 (de) | 1989-03-18 | 1990-02-05 | Kombinationsantrieb fuer fluggeschwindigkeiten von unter - bis hyperschall. |
Country Status (4)
Country | Link |
---|---|
US (1) | US5014508A (US06168776-20010102-C00041.png) |
EP (1) | EP0388613B1 (US06168776-20010102-C00041.png) |
JP (1) | JPH076455B2 (US06168776-20010102-C00041.png) |
DE (2) | DE3909050C1 (US06168776-20010102-C00041.png) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1998056658A1 (de) * | 1997-06-12 | 1998-12-17 | Kaehler Kai | Wiederverwendbares raumschiff |
WO2000034122A1 (de) | 1998-12-05 | 2000-06-15 | Fuersich Manfred | Verfahren zum transport einer nutzlast in den weltraum |
RU2554392C1 (ru) * | 2014-01-10 | 2015-06-27 | Николай Борисович Болотин | Водородный газотурбинный двигатель |
RU2561757C1 (ru) * | 2014-01-14 | 2015-09-10 | Николай Борисович Болотин | Трехкомпонентный воздушно-реактивный двигатель |
RU2561764C1 (ru) * | 2014-01-10 | 2015-09-10 | Николай Борисович Болотин | Водородный газотурбинный двигатель |
RU2561773C1 (ru) * | 2014-01-29 | 2015-09-10 | Николай Борисович Болотин | Двухтопливный воздушно-реактивный двигатель |
RU2591361C1 (ru) * | 2015-01-13 | 2016-07-20 | Николай Борисович Болотин | Двигательная установка гиперзвукового самолета |
RU2594091C1 (ru) * | 2015-01-12 | 2016-08-10 | Николай Борисович Болотин | Двигательная установка гиперзвукового самолета |
CN114427975A (zh) * | 2022-01-27 | 2022-05-03 | 中国航发沈阳发动机研究所 | 一种串联式组合动力模态转换验证方法 |
Families Citing this family (100)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5077968A (en) * | 1990-04-06 | 1992-01-07 | United Technologies Corporation | Vaneless contrarotating turbine |
FR2687433B1 (fr) * | 1992-02-14 | 1994-05-06 | Onera | Propulseur a composants inverses, a alimentation modulee. |
FR2701293B1 (fr) * | 1993-02-05 | 1995-04-28 | Europ Propulsion | Moteur combiné intégrant les modes éjecteur à air turbocomprimé refroidi ou liquéfié statoréacteur et super-statoréacteur. |
US6148609A (en) * | 1999-05-27 | 2000-11-21 | Provitola; Anthony Italo | Turbo-rocket thruster |
EP1172544A1 (fr) * | 2000-07-14 | 2002-01-16 | Techspace Aero S.A. | Moteur d'un lanceur spatial avec dispositif de collecte et séparation d'air |
EP1780387A3 (en) * | 2000-09-05 | 2007-07-18 | Sudarshan Paul Dev | Nested core gas turbine engine |
US6942451B1 (en) | 2003-06-03 | 2005-09-13 | Hamilton Sundstrand Corporation | Damping system for an expendable gas turbine engine |
US7194866B1 (en) | 2003-06-20 | 2007-03-27 | Hamilton Sundstrand Corporation | Static structure for an expendable gas turbine engine |
FR2858999B1 (fr) * | 2003-08-18 | 2005-11-11 | Snecma Moteurs | Turbomachine pour aeronef a emissions de bruit reduites |
US8438858B1 (en) | 2003-08-20 | 2013-05-14 | Hamilton Sundstrand Corporation | Rotational system for an expendable gas turbine engine |
EP1825117B1 (en) | 2004-12-01 | 2012-06-13 | United Technologies Corporation | Turbine engine with differential gear driven fan and compressor |
US20090148273A1 (en) * | 2004-12-01 | 2009-06-11 | Suciu Gabriel L | Compressor inlet guide vane for tip turbine engine and corresponding control method |
EP1834076B1 (en) | 2004-12-01 | 2011-04-06 | United Technologies Corporation | Turbine blade cluster for a fan-turbine rotor assembly and method of mounting such a cluster |
US8087885B2 (en) * | 2004-12-01 | 2012-01-03 | United Technologies Corporation | Stacked annular components for turbine engines |
US7845157B2 (en) | 2004-12-01 | 2010-12-07 | United Technologies Corporation | Axial compressor for tip turbine engine |
WO2006059979A1 (en) | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Tip turbine engine integral case, vane, mount, and mixer |
EP1828568B1 (en) | 2004-12-01 | 2011-03-23 | United Technologies Corporation | Fan-turbine rotor assembly for a tip turbine engine |
EP1831521B1 (en) | 2004-12-01 | 2008-08-20 | United Technologies Corporation | Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method |
EP1828545A2 (en) | 2004-12-01 | 2007-09-05 | United Technologies Corporation | Annular turbine ring rotor |
WO2006059990A1 (en) | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Regenerative turbine blade and vane cooling for a tip turbine engine |
WO2006059988A1 (en) | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Modular tip turbine engine |
EP1819907A2 (en) | 2004-12-01 | 2007-08-22 | United Technologies Corporation | Fan blade with integral diffuser section and tip turbine blade section for a tip turbine engine |
EP1825116A2 (en) * | 2004-12-01 | 2007-08-29 | United Technologies Corporation | Ejector cooling of outer case for tip turbine engine |
US9845727B2 (en) | 2004-12-01 | 2017-12-19 | United Technologies Corporation | Tip turbine engine composite tailcone |
DE602004019710D1 (de) | 2004-12-01 | 2009-04-09 | United Technologies Corp | Fernbetätigung für eine verstellbare stufe eines verdichters für einen turbinenmotor |
US7854112B2 (en) * | 2004-12-01 | 2010-12-21 | United Technologies Corporation | Vectoring transition duct for turbine engine |
US8096753B2 (en) | 2004-12-01 | 2012-01-17 | United Technologies Corporation | Tip turbine engine and operating method with reverse core airflow |
US7882695B2 (en) | 2004-12-01 | 2011-02-08 | United Technologies Corporation | Turbine blow down starter for turbine engine |
EP1834067B1 (en) | 2004-12-01 | 2008-11-26 | United Technologies Corporation | Fan blade assembly for a tip turbine engine and method of assembly |
EP1825177B1 (en) | 2004-12-01 | 2012-01-25 | United Technologies Corporation | Inflatable bleed valve for turbine engine and method of controlling bleed air |
WO2006059980A2 (en) * | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Diffuser aspiration for a tip turbine engine |
WO2006059981A1 (en) | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Hydraulic seal for a gearbox of a tip turbine engine |
US7937927B2 (en) | 2004-12-01 | 2011-05-10 | United Technologies Corporation | Counter-rotating gearbox for tip turbine engine |
US9003759B2 (en) | 2004-12-01 | 2015-04-14 | United Technologies Corporation | Particle separator for tip turbine engine |
DE602004019709D1 (de) * | 2004-12-01 | 2009-04-09 | United Technologies Corp | Tip-turbinentriebwerk und entsprechendes betriebsverfahren |
US8807936B2 (en) | 2004-12-01 | 2014-08-19 | United Technologies Corporation | Balanced turbine rotor fan blade for a tip turbine engine |
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US8033092B2 (en) | 2004-12-01 | 2011-10-11 | United Technologies Corporation | Tip turbine engine integral fan, combustor, and turbine case |
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US8083030B2 (en) | 2004-12-01 | 2011-12-27 | United Technologies Corporation | Gearbox lubrication supply system for a tip engine |
DE602004016059D1 (de) * | 2004-12-01 | 2008-10-02 | United Technologies Corp | Tip-turbinentriebwerk mit wärmetauscher |
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DE3617915C1 (de) * | 1986-05-28 | 1987-09-17 | Messerschmitt Boelkow Blohm | Kombinationsantrieb |
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- 1990-02-05 DE DE9090102216T patent/DE59000220D1/de not_active Expired - Fee Related
- 1990-03-16 JP JP2064473A patent/JPH076455B2/ja not_active Expired - Lifetime
- 1990-03-16 US US07/494,990 patent/US5014508A/en not_active Expired - Fee Related
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Cited By (9)
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WO1998056658A1 (de) * | 1997-06-12 | 1998-12-17 | Kaehler Kai | Wiederverwendbares raumschiff |
WO2000034122A1 (de) | 1998-12-05 | 2000-06-15 | Fuersich Manfred | Verfahren zum transport einer nutzlast in den weltraum |
RU2554392C1 (ru) * | 2014-01-10 | 2015-06-27 | Николай Борисович Болотин | Водородный газотурбинный двигатель |
RU2561764C1 (ru) * | 2014-01-10 | 2015-09-10 | Николай Борисович Болотин | Водородный газотурбинный двигатель |
RU2561757C1 (ru) * | 2014-01-14 | 2015-09-10 | Николай Борисович Болотин | Трехкомпонентный воздушно-реактивный двигатель |
RU2561773C1 (ru) * | 2014-01-29 | 2015-09-10 | Николай Борисович Болотин | Двухтопливный воздушно-реактивный двигатель |
RU2594091C1 (ru) * | 2015-01-12 | 2016-08-10 | Николай Борисович Болотин | Двигательная установка гиперзвукового самолета |
RU2591361C1 (ru) * | 2015-01-13 | 2016-07-20 | Николай Борисович Болотин | Двигательная установка гиперзвукового самолета |
CN114427975A (zh) * | 2022-01-27 | 2022-05-03 | 中国航发沈阳发动机研究所 | 一种串联式组合动力模态转换验证方法 |
Also Published As
Publication number | Publication date |
---|---|
JPH02283846A (ja) | 1990-11-21 |
DE59000220D1 (de) | 1992-09-03 |
EP0388613B1 (de) | 1992-07-29 |
EP0388613A1 (de) | 1990-09-26 |
US5014508A (en) | 1991-05-14 |
JPH076455B2 (ja) | 1995-01-30 |
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