NO941502L - Dreibart montert fleksibel båndvinge - Google Patents

Dreibart montert fleksibel båndvinge

Info

Publication number
NO941502L
NO941502L NO941502A NO941502A NO941502L NO 941502 L NO941502 L NO 941502L NO 941502 A NO941502 A NO 941502A NO 941502 A NO941502 A NO 941502A NO 941502 L NO941502 L NO 941502L
Authority
NO
Norway
Prior art keywords
missile
flexible band
band wing
vehicle
center line
Prior art date
Application number
NO941502A
Other languages
English (en)
Other versions
NO941502D0 (no
Inventor
Ralph H Klestadt
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
Publication of NO941502D0 publication Critical patent/NO941502D0/no
Publication of NO941502L publication Critical patent/NO941502L/no

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

En farkost, eksempelvis et missil (20), innbefatter et aerodynamisk tilformet legeme eller en kropp (22) med en langsgående senterlinje, et sett av styreflater (26) på kroppen (22), og fortrinnsvis et fremdriftssystem (28) som kan drive missilet (22) fremover. På missllets kropp (22) er det montert et sylindrisk drelelager (32) hvis sylinderakse går parallelt med missilets lengde- akse (24). Dreielageret (32) bærer en fleksibel bånd- vinge (38). Denne fleksible båndvinge (38) kan dreie seg om missilets (22) senterlinje (24) l samsvar med aerodynamiske krefter som virker på missilets kropp (22) og på den fleksible båndvinge (38), slik at det muliggjøres manøvreringer av farkosten uten at det er nødvendig for farkosten (20) å krenge for derved å rette inn den fleksible båndvinge (38) til samsvar med manøvreringsretningen.
NO941502A 1993-04-27 1994-04-25 Dreibart montert fleksibel båndvinge NO941502L (no)

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 (2)

Publication Number Publication Date
NO941502D0 NO941502D0 (no) 1994-04-25
NO941502L true NO941502L (no) 1994-10-28

Family

ID=21981171

Family Applications (1)

Application Number Title Priority Date Filing Date
NO941502A NO941502L (no) 1993-04-27 1994-04-25 Dreibart montert fleksibel båndvinge

Country Status (8)

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

Families Citing this family (38)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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

Family Cites Families (11)

* 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
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
ES2117210T3 (es) 1998-08-01
EP0622604A2 (en) 1994-11-02
IL109427A (en) 1997-11-20
NO941502D0 (no) 1994-04-25
EP0622604A3 (en) 1995-05-03
DE69411077T2 (de) 1998-10-29
CA2121740A1 (en) 1994-10-28

Similar Documents

Publication Publication Date Title
NO941502L (no) Dreibart montert fleksibel båndvinge
US4434738A (en) Rudder for watercraft
GB1505199A (en) Vessels
GB892246A (en) Improvements relating to rockets
ES8704625A1 (es) Perfeccionamientos en los lanzamisiles destinados a ser montados en una aeronave militar
PT950005E (pt) Dispositivo de governo ou propulsao para uma embarcacao
MY104255A (en) Trimming system for boat propulsion system
DE3877096D1 (de) Querstrahlruder, insbesondere bugstrahlruder, fuer schiffe.
SE8306324D0 (sv) Hydraulsystem for marin framdrivningsanordning med tilt- och trimorgan
EP0372923A3 (en) Spacecraft approach/separation by use of angular measurement
GB1182792A (en) Improvements in or relating to Self-Propelled Diving Vessels.
SE8505667D0 (sv) Styrorgan for en marin framdrivningsanordning
GB1176465A (en) Improvements in or relating to Ships' Steering and Propulsion Equipment
GB1331497A (en) Propulsion systems for ships
GB1419546A (en) Ship having a bow thruster unit
GB1005565A (en) A rudder attachable to or incorporated with an outboard or inboard propulsion unit
SE8701716D0 (sv) Forfarande och anordning vid en isbrytare
WO1990003912A3 (en) Sailing vessel
CA2136762A1 (en) Rudder Device
EP0031224A3 (en) Water weed cutting and/or clearing vessel
FR2414440A1 (fr) Support intermediaire pour un moteur hors-bord
ILIN et al. Space suit used aboard Salyut-6 described
GB2003807A (en) Aircraft
FR2392181A2 (fr) Dispositif et procede de dragage d'un chenal
WALKER Fin design with ACT in the presence of strakes