ES2117210T3 - Ala de banda flexible montada de forma giratoria. - Google Patents

Ala de banda flexible montada de forma giratoria.

Info

Publication number
ES2117210T3
ES2117210T3 ES94302932T ES94302932T ES2117210T3 ES 2117210 T3 ES2117210 T3 ES 2117210T3 ES 94302932 T ES94302932 T ES 94302932T ES 94302932 T ES94302932 T ES 94302932T ES 2117210 T3 ES2117210 T3 ES 2117210T3
Authority
ES
Spain
Prior art keywords
flexible band
projectile body
projectile
band fin
band wing
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
ES94302932T
Other languages
English (en)
Inventor
Ralph H Klestadt
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 ES2117210T3 publication Critical patent/ES2117210T3/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
    • 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
    • F42B10/02—Stabilising arrangements
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/146—Fabric fins, i.e. fins comprising at least one spar and a fin cover made of flexible sheet material
    • 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
    • F42B15/10—Missiles having a trajectory only in the air
    • F42B15/105—Air torpedoes, e.g. projectiles with or without propulsion, provided with supporting air foil surfaces

Abstract

UN VEHICULO POR EJEMPLO UN PROYECTIL (20) INCLUYE UN CUERPO DE PROYECTIL (22) CONFIGURADO AERODINAMICAMENTE QUE TIENE UNA LINEA CENTRAL LONGITUDINAL, UN CONJUNTO DE SUPERFICIES DE CONTROL (26) UNIDAS AL CUERPO DEL PROYECTIL (22), Y, PREFERIBLEMENTE, UN SISTEMA DE PROPULSION (28) OPERABLE PARA ACCIONAR EL CUERPO DEL PROYECTIL (22) HACIA DELANTE. SE MONTA UN COJINETE ROTACIONAL CILINDRICO (32) SOBRE EL CUERPO DEL PROYECTIL (22) CON SU EJE CILINDRICO PARALELO A LA LINEA CENTRAL LONGITUDINAL (24) DEL CUERPO DEL PROYECTIL. UNA ALETA DE BANDA FLEXIBLE (38) SE SOPORTA DESDE EL COJINETE ROTACIONAL (32). LA ALETA DE BANDA FLEXIBLE (38) PUEDE ROTAR SOBRE LA LINEA CENTRAL (24) DEL CUERPO DEL PROYECTIL (22) SENSIBLE A FUERZAS AERODINAMICAS EJERCIDAS SOBRE EL CUERPO DEL PROYECTIL (22) Y LA ALETA DE LA BANDA FLEXIBLE (38) PARA AYUDAR EN LA PRODUCCION DE MANIOBRAS SIN REQUERIR EL PROYECTIL (20) PARA LADEAR, PARA ALINEAR LA ALETA DE BANDA FLEXIBLE (38) CON LA DIRECCION DE LA MANIOBRA.
ES94302932T 1993-04-27 1994-04-25 Ala de banda flexible montada de forma giratoria. Expired - Lifetime ES2117210T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/052,985 US5417393A (en) 1993-04-27 1993-04-27 Rotationally mounted flexible band wing

Publications (1)

Publication Number Publication Date
ES2117210T3 true ES2117210T3 (es) 1998-08-01

Family

ID=21981171

Family Applications (1)

Application Number Title Priority Date Filing Date
ES94302932T Expired - Lifetime ES2117210T3 (es) 1993-04-27 1994-04-25 Ala de banda flexible montada de forma giratoria.

Country Status (8)

Country Link
US (1) US5417393A (es)
EP (1) EP0622604B1 (es)
JP (1) JP2669783B2 (es)
CA (1) CA2121740A1 (es)
DE (1) DE69411077T2 (es)
ES (1) ES2117210T3 (es)
IL (1) IL109427A (es)
NO (1) NO941502L (es)

Families Citing this family (38)

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US5642867A (en) * 1995-06-06 1997-07-01 Hughes Missile Systems Company Aerodynamic lifting and control surface and control system using same
FR2747464B1 (fr) * 1996-04-16 1999-09-17 Aerospatiale Engin volant a aile deployable
US5816531A (en) * 1997-02-04 1998-10-06 The United States Of America As Represented By The Secretary Of The Army Range correction module for a spin stabilized projectile
FR2769287B1 (fr) 1997-10-08 1999-12-24 Lacroix Soc E Dispositif de freinage de la chute d'une charge
US5927643A (en) * 1997-11-05 1999-07-27 Atlantic Research Corporation Self-deploying airfoil for missile or the like
US6727485B2 (en) * 2001-05-25 2004-04-27 Omnitek Partners Llc Methods and apparatus for increasing aerodynamic performance of projectiles
AUPR583001A0 (en) * 2001-06-20 2001-07-12 Kusic, Tom Aircraft spiralling mechanism
US7637453B2 (en) * 2001-06-22 2009-12-29 Tom Kusic Aircraft spiraling mechanism with jet assistance - A
US7093791B2 (en) * 2001-06-22 2006-08-22 Tom Kusic Aircraft spiralling mechanism—c
US7635104B1 (en) * 2001-06-22 2009-12-22 Tom Kusic Aircraft spiraling mechanism with jet assistance—B
US7165742B2 (en) * 2001-06-22 2007-01-23 Tom Kusic Aircraft spiralling mechanism - B
US6749153B1 (en) * 2002-12-04 2004-06-15 The Boeing Company Survivable and reusable launch vehicle
US6691948B1 (en) 2003-04-10 2004-02-17 The United States Of America As Represented By The Secretary Of The Navy High torque rocket nozzle
US7262394B2 (en) * 2004-03-05 2007-08-28 The Boeing Company Mortar shell ring tail and associated method
DE102006006160B4 (de) * 2006-02-10 2017-05-24 Mbda Deutschland Gmbh Wickelflügel für einen Flugkörper
US7642491B2 (en) 2007-03-19 2010-01-05 Tom Kusic Aircraft spiraling mechanism with jet assistance—D
US9040885B2 (en) * 2008-11-12 2015-05-26 General Dynamics Ordnance And Tactical Systems, Inc. Trajectory modification of a spinning projectile
WO2010064945A1 (ru) * 2008-12-01 2010-06-10 Afanasyev Sergey Nikolaevich Летательный аппарат
AU2010239639B2 (en) 2009-02-02 2015-01-15 Aerovironment Multimode unmanned aerial vehicle
US8878111B2 (en) 2009-02-24 2014-11-04 Blue Origin, Llc Bidirectional control surfaces for use with high speed vehicles, and associated systems and methods
IL198124A0 (en) 2009-04-16 2011-08-01 Raphael E Levy Air vehicle
RU2482021C1 (ru) * 2009-06-01 2013-05-20 Сергей Николаевич Афанасьев Летательный аппарат
EP2475578B1 (en) 2009-09-09 2017-07-19 AeroVironment, Inc. Reinforced UAV launch tube
EP2475575B1 (en) * 2009-09-09 2017-11-01 AeroVironment, Inc. UAV whith deployable wings and method of flight control
US8367993B2 (en) * 2010-07-16 2013-02-05 Raytheon Company Aerodynamic flight termination system and method
US8552349B1 (en) * 2010-12-22 2013-10-08 Interstate Electronics Corporation Projectile guidance kit
SE535991C2 (sv) * 2011-07-07 2013-03-19 Bae Systems Bofors Ab Rotationsstabiliserad styrbar projektil och förfarande därför
US8698059B2 (en) * 2012-05-03 2014-04-15 Raytheon Company Deployable lifting surface for air vehicle
US8899515B2 (en) 2012-05-18 2014-12-02 Textron Systems Corporation Folding configuration for air vehicle
US9193480B2 (en) * 2012-12-07 2015-11-24 Raven Industries, Inc. High altitude balloon system
US9845141B2 (en) 2012-12-07 2017-12-19 Raven Industries, Inc. Atmospheric balloon system
US9487308B2 (en) * 2013-03-15 2016-11-08 Blue Origin, Llc Launch vehicles with ring-shaped external elements, and associated systems and methods
CN104354852B (zh) * 2014-10-20 2017-02-22 中国科学院力学研究所 上置翼调节装置及高速飞行器
US20160221661A1 (en) 2015-02-02 2016-08-04 Derek Lee Bohannon Tendon sleeve for high-altitude balloon and system for making the same
CN104976926B (zh) * 2015-07-15 2017-07-21 江西洪都航空工业集团有限责任公司 一种弹翼单侧翼面折叠机构
FR3041744B1 (fr) * 2015-09-29 2018-08-17 Nexter Munitions Projectile d'artillerie ayant une phase pilotee.
WO2018125942A1 (en) 2016-12-28 2018-07-05 Blue Origin, Llc Vertical landing systems for space vehicles and associated methods
CN110539877A (zh) * 2019-08-21 2019-12-06 成都飞机工业（集团）有限责任公司 一种可旋转伸缩的机翼连接结构

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1448166A (en) * 1918-05-15 1923-03-13 Edw Fay Wilson Projectile
US3135484A (en) * 1959-11-18 1964-06-02 Lockheed Aircraft Corp Control system for annular wing aircraft
US3188957A (en) * 1962-04-03 1965-06-15 Aerojet General Co Ring stabilizer
DE1159314B (de) * 1962-07-11 1963-12-12 Werner Gohlke Dr Ing Elastisches Klappleitwerk, insbesondere fuer Flugkoerper
DE1244586B (de) * 1963-07-05 1967-07-13 Dornier System Gmbh Fluggeraet mit flexiblen Fluegelflaechen
US3374969A (en) * 1966-07-28 1968-03-26 Army Usa Stabilized projectile
US3603533A (en) * 1969-09-29 1971-09-07 Us Army Spin stabilized ring-wing canard controlled missile
US3790103A (en) * 1972-08-21 1974-02-05 Us Navy Rotating fin
GB2244968B (en) * 1982-11-26 1992-05-13 Secr Defence Improvements in missile and other fuselages
DE3516367A1 (de) * 1985-05-07 1986-11-13 Diehl GmbH & Co, 8500 Nürnberg Flugkoerper mit klappfluegel
DE3827590A1 (de) * 1988-08-13 1990-02-22 Messerschmitt Boelkow Blohm Flugkoerper

Also Published As

Publication number Publication date
JPH0769294A (ja) 1995-03-14
NO941502L (no) 1994-10-28
IL109427A0 (en) 1996-12-05
JP2669783B2 (ja) 1997-10-29
EP0622604B1 (en) 1998-06-17
DE69411077D1 (de) 1998-07-23
US5417393A (en) 1995-05-23
EP0622604A2 (en) 1994-11-02
IL109427A (en) 1997-11-20
NO941502D0 (es) 1994-04-25
EP0622604A3 (en) 1995-05-03
DE69411077T2 (de) 1998-10-29
CA2121740A1 (en) 1994-10-28

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