IL226044B - Steering system and method - Google Patents

Steering system and method

Info

Publication number
IL226044B
IL226044B IL226044A IL22604413A IL226044B IL 226044 B IL226044 B IL 226044B IL 226044 A IL226044 A IL 226044A IL 22604413 A IL22604413 A IL 22604413A IL 226044 B IL226044 B IL 226044B
Authority
IL
Israel
Prior art keywords
longitudinal axis
steering system
fluid
respect
exhaust outlet
Prior art date
Application number
IL226044A
Other languages
Hebrew (he)
Inventor
Tsabari Moshe
Bar Anan Doron
Original Assignee
Israel Aerospace Ind Ltd
Tsabari Moshe
Bar Anan Doron
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 Israel Aerospace Ind Ltd, Tsabari Moshe, Bar Anan Doron filed Critical Israel Aerospace Ind Ltd
Priority to IL226044A priority Critical patent/IL226044B/en
Priority to PCT/IL2014/050382 priority patent/WO2014178045A1/en
Publication of IL226044B publication Critical patent/IL226044B/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means 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
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/668—Injection of a fluid, e.g. a propellant, into the gas shear in a nozzle or in the boundary layer at the outer surface of a missile, e.g. to create a shock wave in a supersonic flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B19/00—Marine torpedoes, e.g. launched by surface vessels or submarines; Sea mines having self-propulsion means
    • F42B19/01—Steering control
    • F42B19/06—Directional control

Abstract

A steering system (100) is provided for a body (10) configured for moving through a fluid medium. The steering system has a longitudinal axis (B) and includes a fluid deflector apparatus (200), a mounting arrangement (400), and a control system (600). The fluid deflector apparatus (200) defines at least a part of an external casing (299) of the steering system (100), and includes a ram inlet (210), an exhaust outlet (230) defined on the external casing and laterally disposed with respect to the longitudinal axis, and an internal fluid passageway (270) extending between the ram inlet and the exhaust outlet. The internal fluid passageway is immovably positioned with respect to at least the exhaust outlet. The mounting arrangement is configured for rotatably mounting the fluid deflector apparatus with respect to the body about the longitudinal axis. The control system is configured for selectively providing and maintaining a desired angular disposition of the fluid deflector about the longitudinal axis.
IL226044A 2013-04-29 2013-04-29 Steering system and method IL226044B (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
IL226044A IL226044B (en) 2013-04-29 2013-04-29 Steering system and method
PCT/IL2014/050382 WO2014178045A1 (en) 2013-04-29 2014-04-24 Steering system and method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IL226044A IL226044B (en) 2013-04-29 2013-04-29 Steering system and method

Publications (1)

Publication Number Publication Date
IL226044B true IL226044B (en) 2018-10-31

Family

ID=50928161

Family Applications (1)

Application Number Title Priority Date Filing Date
IL226044A IL226044B (en) 2013-04-29 2013-04-29 Steering system and method

Country Status (2)

Country Link
IL (1) IL226044B (en)
WO (1) WO2014178045A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115294807B (en) * 2022-09-28 2022-12-27 四川腾盾科技有限公司 Control method for intelligent selection of exit of contact crossing for large unmanned aerial vehicle

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4193567A (en) 1962-07-17 1980-03-18 Novatronics, Inc. Guidance devices
US3208383A (en) 1963-07-18 1965-09-28 Roland W Larson Ramjet vent
US3325121A (en) 1964-07-30 1967-06-13 Honeywell Inc Airborne vehicle with vortex valve controlled by linear accelerometer to compensate for variations in aerodynamic drag
FR2244978B1 (en) 1973-09-21 1976-10-01 Europ Propulsion
DE2616209A1 (en) 1976-04-13 1977-11-03 Dynamit Nobel Ag SHORT BULLET FOR EXERCISE AMMUNITION
US4537371A (en) 1982-08-30 1985-08-27 Ltv Aerospace And Defense Company Small caliber guided projectile
EP0135500B1 (en) 1983-01-19 1989-05-17 FORD AEROSPACE & COMMUNICATIONS CORPORATION Ram air steering system for a guided missile
DE3429798C1 (en) 1984-08-13 1985-12-12 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Device for correcting the trajectory of a projectile
US4685639A (en) 1985-12-23 1987-08-11 Ford Aerospace & Communications Corp. Pneumatically actuated ram air steering system for a guided missile
IL167721A (en) 2005-03-29 2008-06-05 Israel Aerospace Ind Ltd Steering system and method for guided flying apparatus
US8076623B2 (en) * 2009-03-17 2011-12-13 Raytheon Company Projectile control device

Also Published As

Publication number Publication date
WO2014178045A1 (en) 2014-11-06

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