DE69632339D1 - Vorrichtung und verfahren zum steuern der bewegung eines fluiden mediums - Google Patents

Vorrichtung und verfahren zum steuern der bewegung eines fluiden mediums

Info

Publication number
DE69632339D1
DE69632339D1 DE69632339T DE69632339T DE69632339D1 DE 69632339 D1 DE69632339 D1 DE 69632339D1 DE 69632339 T DE69632339 T DE 69632339T DE 69632339 T DE69632339 T DE 69632339T DE 69632339 D1 DE69632339 D1 DE 69632339D1
Authority
DE
Germany
Prior art keywords
controlling
movement
fluid medium
fluid
medium
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
DE69632339T
Other languages
English (en)
Other versions
DE69632339T2 (de
Inventor
Avi Seifert
Israel Wygnanski
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.)
Ramot at Tel Aviv University Ltd
Original Assignee
Ramot at Tel Aviv University Ltd
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 Ramot at Tel Aviv University Ltd filed Critical Ramot at Tel Aviv University Ltd
Application granted granted Critical
Publication of DE69632339D1 publication Critical patent/DE69632339D1/de
Publication of DE69632339T2 publication Critical patent/DE69632339T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/90Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using deflectors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/82Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control by injection of a secondary fluid into the rocket exhaust gases
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60Steering arrangements
    • F42B10/66Steering by varying intensity or direction of thrust
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60Steering arrangements
    • F42B10/66Steering by varying intensity or direction of thrust
    • F42B10/665Steering by varying intensity or direction of thrust characterised by using a nozzle provided with at least a deflector mounted within the nozzle

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Nozzles (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DE69632339T 1996-01-03 1996-12-29 Vorrichtung und verfahren zum steuern der bewegung eines fluiden mediums Expired - Fee Related DE69632339T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
IL11666896A IL116668A (en) 1996-01-03 1996-01-03 Apparatus and method for controlling the motion of a solid body or fluid stream
IL11666896 1996-01-03
PCT/IL1996/000194 WO1997025623A2 (en) 1996-01-03 1996-12-29 Controlling motions of a solid body or fluid stream

Publications (2)

Publication Number Publication Date
DE69632339D1 true DE69632339D1 (de) 2004-06-03
DE69632339T2 DE69632339T2 (de) 2005-05-25

Family

ID=11068399

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69632339T Expired - Fee Related DE69632339T2 (de) 1996-01-03 1996-12-29 Vorrichtung und verfahren zum steuern der bewegung eines fluiden mediums

Country Status (6)

Country Link
US (1) US6250586B1 (de)
EP (1) EP0871582B1 (de)
AU (1) AU1107797A (de)
DE (1) DE69632339T2 (de)
IL (1) IL116668A (de)
WO (1) WO1997025623A2 (de)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6751530B2 (en) 2002-06-10 2004-06-15 Ramot At Tel Aviv University Ltd. Aerial vehicle controlled and propelled by oscillatory momentum generators and method of flying a vehicle
US8096104B2 (en) * 2007-05-31 2012-01-17 United Technologies Corporation Fluidic vectoring for exhaust nozzle

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1054415A (de) *
GB842971A (en) * 1955-08-12 1960-08-04 United Aircraft Corp Directional control means for supersonic vehicle
GB916692A (en) * 1958-06-19 1963-01-23 Snecma Improvements in jet control apparatus
US3299638A (en) * 1965-03-12 1967-01-24 Ltv Aerospace Corp Variable flow deflection means
GB1325021A (en) * 1969-11-22 1973-08-01 Mikuni Kogyo Kk Impulse signal producing device of the pneumatic pressure type
US3598318A (en) * 1970-04-10 1971-08-10 Boeing Co Movable acoustic splitter for nozzle area control and thrust reversal
US3747875A (en) * 1971-11-04 1973-07-24 Us Air Force V/stol aircraft-by-pass engine having a double, thrust diverter valve assembly
US3786993A (en) * 1972-05-22 1974-01-22 Imp Metal Ind Kynoch Ltd Control systems for rocket motors
IL52613A (en) * 1977-07-28 1980-11-30 Univ Ramot Method and apparatus for controlling the mixing of two fluids
DE2913350A1 (de) * 1979-04-03 1980-10-16 Messerschmitt Boelkow Blohm Strahltriebwerk fuer lenkflugkoerper
US4645140A (en) * 1983-08-18 1987-02-24 Rockwell International Corporation Nozzle system
FR2557926B1 (fr) * 1984-01-06 1986-04-11 Brandt Armements Propulseur a gaz pour projectile guide.
US4754927A (en) * 1986-12-08 1988-07-05 Colt Industries Inc. Control vanes for thrust vector control nozzle
US5209438A (en) * 1988-06-20 1993-05-11 Israel Wygnanski Method and apparatus for delaying the separation of flow from a solid surface
US4978071A (en) * 1989-04-11 1990-12-18 General Electric Company Nozzle with thrust vectoring in the yaw direction
US5154050A (en) * 1990-12-14 1992-10-13 Herup Eric J Thrust vector control using internal airfoils
US5706650A (en) * 1995-08-09 1998-01-13 United Technologies Corporation Vectoring nozzle using injected high pressure air

Also Published As

Publication number Publication date
DE69632339T2 (de) 2005-05-25
EP0871582A4 (de) 1999-03-24
IL116668A (en) 1998-12-06
WO1997025623A3 (en) 1997-09-04
WO1997025623A2 (en) 1997-07-17
US6250586B1 (en) 2001-06-26
AU1107797A (en) 1997-08-01
EP0871582A2 (de) 1998-10-21
IL116668A0 (en) 1996-10-31
EP0871582B1 (de) 2004-04-28

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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