ES2092052T3 - Sistema accionador de aleta de control de misil. - Google Patents

Sistema accionador de aleta de control de misil.

Info

Publication number
ES2092052T3
ES2092052T3 ES92306661T ES92306661T ES2092052T3 ES 2092052 T3 ES2092052 T3 ES 2092052T3 ES 92306661 T ES92306661 T ES 92306661T ES 92306661 T ES92306661 T ES 92306661T ES 2092052 T3 ES2092052 T3 ES 2092052T3
Authority
ES
Spain
Prior art keywords
piston
accommodation
housing
missile
pressure
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
Application number
ES92306661T
Other languages
English (en)
Inventor
Charles M Delair
Russell B Cline
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.)
Raytheon Co
Original Assignee
Hughes Aircraft Co
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 Hughes Aircraft Co filed Critical Hughes Aircraft Co
Application granted granted Critical
Publication of ES2092052T3 publication Critical patent/ES2092052T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • 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
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Actuator (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

UN ACTIVADOR DE LA ALETA DE CONTROL (28) PARA UN MISIL DIRIGIDO (20) INCLUYE UN ACTIVADOR DE PRESION (40) QUE TIENE UN PISTON DESLIZABLE (44) DENTRO DE UN ALOJAMIENTO (42). LOS CIERRES DE DIAFRAGMA GIRATORIOS (50,56) DE LA CARA DEL PISTON SUPERIOR (46) Y DE LA CARA DEL PISTON INFERIOR (48) EN LA PARED INTERIOR DEL ALOJAMIENTO (42) DIVIDEN EL INTERIOR DEL ALOJAMIENTO (42) EN AL MENOS DOS CAMARAS (54, 58). LOS CIERRES DE DIAFRAGMA GIRATORIOS (50, 56) ELIMINAN LA FRICCION DE DESLIZAMIENTO MIENTRAS EL PISTON (44) SE MUEVE DENTRO DEL ALOJAMIENTO. LAS DOS CAMARAS (54, 58) ESTAN PRESURIZADAS CONTROLABLEMENTE PARA DESLIZAR EL PISTON (44) DENTRO DEL ALOJAMIENTO (42), MOVIENDO ASI UNA VARILLA DE EMPUJE (78) UNIDA AL PISTON (44) Y EXTENDIENDOSE FUERA DEL ALOJAMIENTO (42). LA VARILLA DE EMPUJE (78) ESTA CONECTADA A UN EJE DE SALIDA DE LA ALETA DE CONTROL DEL MISIL (24) POR UN CONECTOR DE BANDA TENSO (80) QUE IMPIDE UN CONTRAGOLPE. UN IMAN (86) PUEDE ESTAR SITUADO JUNTO A LA VARILLA DE EMPUJE (78) PARAPRODUCIR CORRIENTES DE TORBELLINO EN LA VARILLA DE EMPUJE (78), PROPORCIONANDO ASI UNA FUERZA DE AMORTIGUAMIENTO QUE AUMENTA CON EL COEFICIENTE DE INCREMENTO DE MOVIMIENTO. LA PRESION EN LA CAMARA DE CONTROL (54) ES REALIZADA POR EL ACCIONAMIENTO DE LA VALVULA DE ENTRADA (70) Y LA VALVULA DE ESCAPE (72) EN RESPUESTA A LA INFORMACION DE RETROALIMENTACION DESDE UN SENSOR DE POSICION GIRATORIA (29), UN SENSOR DE POSICION LONGITUDINAL (88) Y/O SENSORES DE PRESION (90, 92).
ES92306661T 1991-08-02 1992-07-21 Sistema accionador de aleta de control de misil. Expired - Lifetime ES2092052T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/739,570 US5293811A (en) 1991-08-02 1991-08-02 Missile control fin actuator system

Publications (1)

Publication Number Publication Date
ES2092052T3 true ES2092052T3 (es) 1996-11-16

Family

ID=24972905

Family Applications (1)

Application Number Title Priority Date Filing Date
ES92306661T Expired - Lifetime ES2092052T3 (es) 1991-08-02 1992-07-21 Sistema accionador de aleta de control de misil.

Country Status (11)

Country Link
US (1) US5293811A (es)
EP (1) EP0529796B1 (es)
JP (1) JP2633144B2 (es)
KR (1) KR970001772B1 (es)
AU (1) AU636081B2 (es)
CA (1) CA2068962C (es)
DE (1) DE69214068T2 (es)
ES (1) ES2092052T3 (es)
NO (1) NO303089B1 (es)
TR (1) TR26552A (es)
TW (1) TW244377B (es)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100512751B1 (ko) * 2003-04-03 2005-09-05 유근형 액츄에이터
US20090108066A1 (en) * 2006-06-14 2009-04-30 Riotec Co., Ltd. Optical system for barcode scanner
DE112008003309T5 (de) * 2007-12-03 2010-10-07 Cts Corp., Elkhart Linearer Positionssensor
CN202101680U (zh) 2008-11-26 2012-01-04 Cts公司 带有抗转器的线性位置传感器
US8664947B2 (en) * 2008-12-02 2014-03-04 Cts Corporation Actuator and sensor assembly
US8408082B2 (en) * 2009-11-18 2013-04-02 General Electric Company Apparatus to measure fluids in a conduit
US9435630B2 (en) 2010-12-08 2016-09-06 Cts Corporation Actuator and linear position sensor assembly
US9618305B2 (en) * 2012-04-24 2017-04-11 Omnitek Partners Llc Very low power actuation devices
DE102015005135A1 (de) 2015-04-22 2016-10-27 Diehl Bgt Defence Gmbh & Co. Kg Flugkörperrudersystem
JP6989321B2 (ja) * 2017-08-29 2022-01-05 三菱重工業株式会社 飛翔体
US11326628B2 (en) * 2019-12-09 2022-05-10 The Boeing Company Hydraulic actuation system for imparting rotation

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3125000A (en) * 1964-03-17 Airfoil controlling actuator
US3020008A (en) * 1957-10-01 1962-02-06 Houdaille Industries Inc Control surface actuator damper hinge
US2997988A (en) * 1959-08-03 1961-08-29 Young Spring & Wire Corp Fluid motor mechanism
US3100399A (en) * 1961-07-21 1963-08-13 Worthington Corp Pneumatic servo-positioner unit
US3063423A (en) * 1961-08-17 1962-11-13 Gen Precision Inc Seal means for hydraulic actuator
US3301141A (en) * 1964-10-20 1967-01-31 Fairchild Hiller Corp Magnetically damped pneumatic control devices
US3673861A (en) * 1969-06-27 1972-07-04 Univ Iowa State Res Found Inc Method and apparatus for in situ measurement of soil creep strength
US3767160A (en) * 1971-01-20 1973-10-23 Collum R Mc Null-balance regulator valve
FR2259245B1 (es) * 1974-01-30 1979-04-13 Aquitaine Petrole
DE2435354C3 (de) * 1974-07-23 1980-03-06 Eckardt Ag, 7000 Stuttgart Doppeltwirkender pneumatischer Stellantrieb
JPS5225600U (es) * 1975-08-09 1977-02-23
US4366722A (en) * 1980-06-26 1983-01-04 International Memories, Incorporated Drive connection between linear actuator and rotatable drive shaft of reversible motor
US4655420A (en) * 1983-06-09 1987-04-07 The United States Of America As Represented By The Secretary Of The Air Force Low height fin control actuator
US4754776A (en) * 1984-01-24 1988-07-05 Mckee James E Pneumatic control valves with diaphragm actuators and modular body structure
DE3410666C2 (de) * 1984-03-23 1986-03-06 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Stellantrieb
US4763560A (en) * 1984-05-25 1988-08-16 Tokyo Precision Instruments Co., Ltd. Method and apparatus of controlling and positioning fluid actuator
US4800798A (en) * 1984-12-11 1989-01-31 The United States Of America As Represented By The Secretary Of The Air Force Control surface dual redundant servomechanism
US4759262A (en) * 1987-05-11 1988-07-26 The Dow Chemical Company Apparatus for restraining rotary motion of a motor component

Also Published As

Publication number Publication date
KR930004741A (ko) 1993-03-23
DE69214068D1 (de) 1996-10-31
NO303089B1 (no) 1998-05-25
AU636081B2 (en) 1993-04-08
JP2633144B2 (ja) 1997-07-23
NO922977L (no) 1993-02-03
DE69214068T2 (de) 1997-02-06
AU2062392A (en) 1993-02-25
EP0529796B1 (en) 1996-09-25
EP0529796A1 (en) 1993-03-03
JPH05196396A (ja) 1993-08-06
TW244377B (es) 1995-04-01
NO922977D0 (no) 1992-07-28
US5293811A (en) 1994-03-15
KR970001772B1 (ko) 1997-02-15
TR26552A (tr) 1995-03-15
CA2068962A1 (en) 1993-02-03
CA2068962C (en) 1996-11-05

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