JPWO2019167319A1 - ロケットエンジン用ターボポンプ - Google Patents
ロケットエンジン用ターボポンプ Download PDFInfo
- Publication number
- JPWO2019167319A1 JPWO2019167319A1 JP2020502794A JP2020502794A JPWO2019167319A1 JP WO2019167319 A1 JPWO2019167319 A1 JP WO2019167319A1 JP 2020502794 A JP2020502794 A JP 2020502794A JP 2020502794 A JP2020502794 A JP 2020502794A JP WO2019167319 A1 JPWO2019167319 A1 JP WO2019167319A1
- Authority
- JP
- Japan
- Prior art keywords
- nozzle
- spindle
- nozzles
- outlet
- rows
- 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.)
- Granted
Links
- 238000002347 injection Methods 0.000 description 25
- 239000007924 injection Substances 0.000 description 25
- 239000007789 gas Substances 0.000 description 19
- 239000003380 propellant Substances 0.000 description 15
- 239000000411 inducer Substances 0.000 description 14
- 239000012530 fluid Substances 0.000 description 11
- 238000002485 combustion reaction Methods 0.000 description 4
- 239000007788 liquid Substances 0.000 description 4
- 230000002093 peripheral effect Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 239000001257 hydrogen Substances 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000010363 phase shift Effects 0.000 description 2
- 238000005086 pumping Methods 0.000 description 2
- 239000000567 combustion gas Substances 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000005284 excitation Effects 0.000 description 1
- 239000003350 kerosene Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 239000007800 oxidant agent Substances 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
Images
Classifications
-
- 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
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/44—Feeding propellants
- F02K9/46—Feeding propellants using pumps
- F02K9/48—Feeding propellants using pumps driven by a gas turbine fed by propellant combustion gases or fed by vaporized propellants or other gases
-
- 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
- F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
- F01D15/08—Adaptations for driving, or combinations with, pumps
-
- 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
- F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
- F01D1/02—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
- F01D1/026—Impact turbines with buckets, i.e. impulse turbines, e.g. Pelton turbines
-
- 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
- F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
- F01D1/18—Non-positive-displacement machines or engines, e.g. steam turbines without stationary working-fluid guiding means
- F01D1/20—Non-positive-displacement machines or engines, e.g. steam turbines without stationary working-fluid guiding means traversed by the working-fluid substantially axially
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D13/00—Pumping installations or systems
- F04D13/02—Units comprising pumps and their driving means
- F04D13/04—Units comprising pumps and their driving means the pump being fluid driven
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
- F05D2240/128—Nozzles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/10—Two-dimensional
- F05D2250/14—Two-dimensional elliptical
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/30—Arrangement of components
- F05D2250/31—Arrangement of components according to the direction of their main axis or their axis of rotation
- F05D2250/314—Arrangement of components according to the direction of their main axis or their axis of rotation the axes being inclined in relation to each other
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/30—Arrangement of components
- F05D2250/36—Arrangement of components in inner-outer relationship, e.g. shaft-bearing arrangements
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Description
前記主軸の一端側に取り付けられたインペラを含むポンプ部と、前記主軸の他端側に取り付けられたディスク、前記ディスクの外周に設けられた複数の動翼、及び、前記動翼が成す翼列の入口面に向けて傾斜して設けられ、軸対称な断面を有する複数のノズルを含むタービン部と、を備え、前記複数のノズルは、前記主軸と直交する平面において前記主軸の周方向に沿った、第1の列および前記第1の列よりも径方向外側の第2の列に配置されることを要旨とする。
Claims (6)
- 回転可能に支持された主軸と、
前記主軸の一端側に取り付けられたインペラを含むポンプ部と、
前記主軸の他端側に取り付けられたディスク、前記ディスクの外周に設けられた複数の動翼、及び、前記動翼が成す翼列の入口面に向けて傾斜して設けられ、軸対称な断面を有する複数のノズルを含むタービン部と、
を備え、
前記複数のノズルは、前記主軸と直交する平面において前記主軸の周方向に沿った少なくとも2列に配置されるロケットエンジン用ターボポンプ。 - 各前記ノズルは、当該ノズルの中心軸に沿った当該ノズルの出口の前記入口面への投影面が前記入口面内に納まるように配列している請求項1に記載のロケットエンジン用ターボポンプ。
- 前記2列のうちの一方の列のノズルの出口と前記2列のうちの他方の列のノズルの出口は、前記主軸の周りで互いに異なる位相に位置する請求項1または2に記載のロケットエンジン用ターボポンプ。
- 前記2列のうちの一方の列のノズルの出口と前記2列のうちの他方の列のノズルの出口は、互いに異なる断面積を有する請求項1から3のうちの何れか一項に記載のロケットエンジン用ターボポンプ。
- 前記2列のうちの一方の列のノズルを第1ノズルとし、前記2列のうちの他方の列のノズルを第2ノズルとし、前記第1ノズルの出口をその中心軸に沿って前記入口面に投影した楕円を第1の楕円とし、前記第2ノズルの出口をその中心軸に沿って前記入口面に投影した楕円を第2の楕円とした場合、前記第1の楕円の長軸と、前記第2の楕円の長軸は、前記入口面内において互いに反対、あるいは同じ向きに、角度を変えて傾斜している請求項1から4のうちの何れか一項に記載のロケットエンジン用ターボポンプ。
- 前記複数のノズルはそれぞれラバールノズルである請求項1から5のうちの何れか一項に記載のロケットエンジン用ターボポンプ。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2018032749 | 2018-02-27 | ||
JP2018032749 | 2018-02-27 | ||
PCT/JP2018/034838 WO2019167319A1 (ja) | 2018-02-27 | 2018-09-20 | ロケットエンジン用ターボポンプ |
Publications (2)
Publication Number | Publication Date |
---|---|
JPWO2019167319A1 true JPWO2019167319A1 (ja) | 2020-12-03 |
JP6841376B2 JP6841376B2 (ja) | 2021-03-10 |
Family
ID=67806076
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2020502794A Active JP6841376B2 (ja) | 2018-02-27 | 2018-09-20 | ロケットエンジン用ターボポンプ |
Country Status (4)
Country | Link |
---|---|
US (1) | US11466645B2 (ja) |
EP (1) | EP3760869B1 (ja) |
JP (1) | JP6841376B2 (ja) |
WO (1) | WO2019167319A1 (ja) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11795833B1 (en) * | 2022-12-21 | 2023-10-24 | Pipl Limited | Nozzle set |
CN116291960B (zh) * | 2023-04-23 | 2023-11-14 | 北京星河动力装备科技有限公司 | 集气结构、涡轮泵以及火箭发动机 |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2578443A (en) * | 1948-02-10 | 1951-12-11 | Joseph J Mascuch | Pressure gas generation control |
US3216191A (en) * | 1960-05-09 | 1965-11-09 | North American Aviation Inc | Thrust chamber and turbopump assembly |
JPS52118105A (en) * | 1976-03-29 | 1977-10-04 | Esu Souaa Jiyon | Profileeformed supersonic nozzle |
JPS5349607A (en) * | 1976-10-19 | 1978-05-06 | Mitsubishi Heavy Ind Ltd | Axial flow turbine |
JPS5422003A (en) * | 1977-07-18 | 1979-02-19 | Suchiyuaato Bagurii Chiyaarusu | Method of and device for generating directed high speed flow of compressive fluid |
JPS60167102U (ja) * | 1984-04-13 | 1985-11-06 | 三菱重工業株式会社 | ラジアルフロ−衝動タ−ビンのノズル構造 |
JPH08232603A (ja) * | 1994-12-27 | 1996-09-10 | Soc Europ Propulsion <Sep> | ターボ機械の入口段用の超音速分配器 |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1883868A (en) * | 1930-03-21 | 1932-10-25 | Westinghouse Electric & Mfg Co | Turbine nozzle block |
US1883668A (en) | 1931-10-23 | 1932-10-18 | Charles N Foreman | Refrigerator |
DE1164753B (de) * | 1959-12-12 | 1964-03-05 | Boelkow Entwicklungen Kg | Raketentriebwerk fuer fluessige Treibstoffe |
GB1020995A (en) | 1962-09-04 | 1966-02-23 | Snecma | Centrifugal pump |
US3286473A (en) * | 1963-06-26 | 1966-11-22 | North American Aviation Inc | Fixed injector and turbopump assembly |
US3968935A (en) * | 1973-05-21 | 1976-07-13 | Sohre John S | Contoured supersonic nozzle |
US4036020A (en) * | 1975-12-15 | 1977-07-19 | Charles Stuart Bagley | Method and apparatus for producing a directed, high-velocity stream of compressible fluid |
FR2698661B1 (fr) * | 1992-11-30 | 1995-02-17 | Europ Propulsion | Turbopompe compacte de forte puissance pour moteur-fusée. |
US6969028B2 (en) | 2003-01-22 | 2005-11-29 | The Boeing Company | Scarf nozzle for a jet engine and method of using the same |
JP2007023894A (ja) | 2005-07-15 | 2007-02-01 | Toyota Motor Corp | ターボ過給機 |
JP2013015034A (ja) | 2011-06-30 | 2013-01-24 | Mitsubishi Heavy Ind Ltd | 可変容量ラジアルタービンおよびそれを備えたターボチャージャ |
JP6045389B2 (ja) | 2013-02-18 | 2016-12-14 | 三菱重工業株式会社 | タービンノズル及びその製造方法 |
FR3008749B1 (fr) * | 2013-07-22 | 2015-08-28 | Snecma | Pompe centrifuge, en particulier pour l'alimentation de moteurs de fusee |
DE102013218887A1 (de) * | 2013-09-20 | 2015-03-26 | Mahle International Gmbh | Lavaldüse |
JP2016142209A (ja) | 2015-02-03 | 2016-08-08 | 三井造船株式会社 | Vpc発電に使用するノズル構造 |
-
2018
- 2018-09-20 WO PCT/JP2018/034838 patent/WO2019167319A1/ja unknown
- 2018-09-20 EP EP18907686.2A patent/EP3760869B1/en active Active
- 2018-09-20 JP JP2020502794A patent/JP6841376B2/ja active Active
-
2020
- 2020-04-22 US US16/854,962 patent/US11466645B2/en active Active
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2578443A (en) * | 1948-02-10 | 1951-12-11 | Joseph J Mascuch | Pressure gas generation control |
US3216191A (en) * | 1960-05-09 | 1965-11-09 | North American Aviation Inc | Thrust chamber and turbopump assembly |
JPS52118105A (en) * | 1976-03-29 | 1977-10-04 | Esu Souaa Jiyon | Profileeformed supersonic nozzle |
JPS5349607A (en) * | 1976-10-19 | 1978-05-06 | Mitsubishi Heavy Ind Ltd | Axial flow turbine |
JPS5422003A (en) * | 1977-07-18 | 1979-02-19 | Suchiyuaato Bagurii Chiyaarusu | Method of and device for generating directed high speed flow of compressive fluid |
JPS60167102U (ja) * | 1984-04-13 | 1985-11-06 | 三菱重工業株式会社 | ラジアルフロ−衝動タ−ビンのノズル構造 |
JPH08232603A (ja) * | 1994-12-27 | 1996-09-10 | Soc Europ Propulsion <Sep> | ターボ機械の入口段用の超音速分配器 |
Also Published As
Publication number | Publication date |
---|---|
US20200248650A1 (en) | 2020-08-06 |
JP6841376B2 (ja) | 2021-03-10 |
EP3760869B1 (en) | 2023-08-23 |
EP3760869A1 (en) | 2021-01-06 |
EP3760869A4 (en) | 2021-11-24 |
US11466645B2 (en) | 2022-10-11 |
WO2019167319A1 (ja) | 2019-09-06 |
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