DE68905156D1 - Kompakte hochdruckturbopumpe zur versorgung eines raketenmotors mit treibstoff. - Google Patents

Kompakte hochdruckturbopumpe zur versorgung eines raketenmotors mit treibstoff.

Info

Publication number
DE68905156D1
DE68905156D1 DE8989403401T DE68905156T DE68905156D1 DE 68905156 D1 DE68905156 D1 DE 68905156D1 DE 8989403401 T DE8989403401 T DE 8989403401T DE 68905156 T DE68905156 T DE 68905156T DE 68905156 D1 DE68905156 D1 DE 68905156D1
Authority
DE
Germany
Prior art keywords
fuel
pump
supply
high pressure
rocket engine
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 - Fee Related
Application number
DE8989403401T
Other languages
English (en)
Other versions
DE68905156T2 (de
Inventor
Claude Mechin
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Societe Europeenne de Propulsion SEP SA
Original Assignee
Societe Europeenne de Propulsion SEP SA
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Societe Europeenne de Propulsion SEP SA filed Critical Societe Europeenne de Propulsion SEP SA
Publication of DE68905156D1 publication Critical patent/DE68905156D1/de
Application granted granted Critical
Publication of DE68905156T2 publication Critical patent/DE68905156T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/005—Selecting particular materials
    • 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
    • F05D2250/00—Geometry
    • F05D2250/60—Structure; Surface texture

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
DE89403401T 1988-12-12 1989-12-08 Kompakte Hochdruckturbopumpe zur Versorgung eines Raketenmotors mit Treibstoff. Expired - Fee Related DE68905156T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8816340A FR2640323B1 (fr) 1988-12-12 1988-12-12 Ensemble structural compact d'alimentation d'un moteur-fusee en ergols a haute pression

Publications (2)

Publication Number Publication Date
DE68905156D1 true DE68905156D1 (de) 1993-04-08
DE68905156T2 DE68905156T2 (de) 1993-09-30

Family

ID=9372849

Family Applications (1)

Application Number Title Priority Date Filing Date
DE89403401T Expired - Fee Related DE68905156T2 (de) 1988-12-12 1989-12-08 Kompakte Hochdruckturbopumpe zur Versorgung eines Raketenmotors mit Treibstoff.

Country Status (5)

Country Link
US (1) US5074762A (de)
EP (1) EP0374020B1 (de)
JP (1) JP2750182B2 (de)
DE (1) DE68905156T2 (de)
FR (1) FR2640323B1 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2671142B1 (fr) * 1990-12-31 1993-04-23 Europ Propulsion Turbopompe a gavage integre en flux derive.
FR2671141B1 (fr) * 1990-12-31 1993-08-20 Europ Propulsion Turbopompe a gavage integre en flux unique.
FR2671143B1 (fr) * 1990-12-31 1993-04-23 Europ Propulsion Turbopompe a gavage integre en flux axial.
FR2698666B1 (fr) * 1992-11-30 1995-02-17 Europ Propulsion Pompe centrifuge hautement performante à rouet ouvert.
FR2698667B1 (fr) * 1992-11-30 1995-02-17 Europ Propulsion Pompe centrifuge à rouet ouvert.
US5444973A (en) * 1993-12-13 1995-08-29 United Technologies Corporation Pressure-fed rocket booster system
US6848163B2 (en) * 2001-08-31 2005-02-01 The Boeing Company Nanophase composite duct assembly
US7931441B1 (en) 2008-03-18 2011-04-26 Florida Turbine Technologies, Inc. Inducer with tip shroud and turbine blades
US7828511B1 (en) 2008-03-18 2010-11-09 Florida Turbine Technologies, Inc. Axial tip turbine driven pump
US9206820B2 (en) 2012-06-11 2015-12-08 Aerojet Rocketdyne, Inc. Inducer with cavitation instability controls to reduce vibrations and radial loads
CN114941586B (zh) * 2022-05-31 2024-09-10 西安航天动力研究所 双介质驱动的预增压泵及低温液体火箭发动机的起动方法

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2707919A (en) * 1950-12-27 1955-05-10 Kellogg M W Co Turbo-pump sets
CH313449A (de) * 1952-02-21 1956-04-15 Bercovitz Bernard Pumpenaggregat mit Druckluft-Turbinenantrieb
US3091921A (en) * 1957-06-24 1963-06-04 Thiokol Chemical Corp Turborocket powerplant including turbine bypassing means for a portion of the propellant
FR2040548A5 (de) * 1969-04-03 1971-01-22 Bringer Henri
US3991248A (en) * 1972-03-28 1976-11-09 Ducommun Incorporated Fiber reinforced composite product
SE406624B (sv) * 1977-07-12 1979-02-19 Stal Laval Turbin Ab Turbomaskin
DE3003470C2 (de) * 1980-01-31 1982-02-25 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Turbinenleitschaufelaufhängung für Gasturbinenstrahltriebwerke
US4790052A (en) * 1983-12-28 1988-12-13 Societe Europeenne De Propulsion Process for manufacturing homogeneously needled three-dimensional structures of fibrous material
FR2567874B1 (fr) * 1984-07-20 1987-01-02 Europ Propulsion Procede de fabrication d'un materiau composite a renfort fibreux refractaire et matrice ceramique, et structure telle qu'obtenue par ce procede

Also Published As

Publication number Publication date
DE68905156T2 (de) 1993-09-30
FR2640323B1 (fr) 1991-04-05
EP0374020A1 (de) 1990-06-20
JPH02256859A (ja) 1990-10-17
FR2640323A1 (fr) 1990-06-15
EP0374020B1 (de) 1993-03-03
US5074762A (en) 1991-12-24
JP2750182B2 (ja) 1998-05-13

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee