DE69411077D1 - Drehbar angeordneter und mittels eines flexiblen Bandes hergestellter Tragflügel - Google Patents

Drehbar angeordneter und mittels eines flexiblen Bandes hergestellter Tragflügel

Info

Publication number
DE69411077D1
DE69411077D1 DE69411077T DE69411077T DE69411077D1 DE 69411077 D1 DE69411077 D1 DE 69411077D1 DE 69411077 T DE69411077 T DE 69411077T DE 69411077 T DE69411077 T DE 69411077T DE 69411077 D1 DE69411077 D1 DE 69411077D1
Authority
DE
Germany
Prior art keywords
wing
manufactured
rotatably arranged
flexible band
band
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
DE69411077T
Other languages
English (en)
Other versions
DE69411077T2 (de
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
Publication of DE69411077D1 publication Critical patent/DE69411077D1/de
Application granted granted Critical
Publication of DE69411077T2 publication Critical patent/DE69411077T2/de
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
DE69411077T 1993-04-27 1994-04-25 Drehbar angeordneter und mittels eines flexiblen Bandes hergestellter Tragflügel Expired - Lifetime DE69411077T2 (de)

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
DE69411077D1 true DE69411077D1 (de) 1998-07-23
DE69411077T2 DE69411077T2 (de) 1998-10-29

Family

ID=21981171

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69411077T Expired - Lifetime DE69411077T2 (de) 1993-04-27 1994-04-25 Drehbar angeordneter und mittels eines flexiblen Bandes hergestellter Tragflügel

Country Status (8)

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

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 (de) 2009-09-09 2017-07-19 AeroVironment, Inc. Verstärktes Rohr zum katapultieren von Drohnen
EP2475575B1 (de) * 2009-09-09 2017-11-01 AeroVironment, Inc. UAV mit ausfahrbaren Flügeln und Flugsteuerungsverfahren
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
NO941502L (no) 1994-10-28
IL109427A0 (en) 1996-12-05
JP2669783B2 (ja) 1997-10-29
EP0622604B1 (de) 1998-06-17
US5417393A (en) 1995-05-23
ES2117210T3 (es) 1998-08-01
EP0622604A2 (de) 1994-11-02
IL109427A (en) 1997-11-20
NO941502D0 (de) 1994-04-25
EP0622604A3 (de) 1995-05-03
DE69411077T2 (de) 1998-10-29
CA2121740A1 (en) 1994-10-28

Similar Documents

Publication Publication Date Title
DE69411077D1 (de) Drehbar angeordneter und mittels eines flexiblen Bandes hergestellter Tragflügel
DE69504915D1 (de) Lärmverminderungvorrichtung eines Drehflügelflugzeuges
DE3689308D1 (de) AUSBILDUNG DES MUNDSTÜCKS EINES MIT ULTRASCHALL ARBEITENDEN ABSAUG-ENDOSKOPS UND DAZUGEHöRIGER VIBRATOR.
NZ230084A (en) Glove: elongate band of adhesive around cuff
DE69316993T2 (de) Untersuchung eines körpers
DE69218580T2 (de) Steuervorrichtung eines Stromrichters
DE69228819T2 (de) Konfigurations- und Betriebsverfahren eines Telekommunikationsgeräts
DE69432671D1 (de) Flüssigkeitsgekühlte und perfundierte spitze eines katheters
DE69125148D1 (de) Ellbogenstütze zum vermindern der wirkung eines tennisellbogens
DE68927014D1 (de) Assoziatives Musterkonversionssystem und Anpassungsverfahren dafür
DE69807569T2 (de) Verbindungsvorrichtung zwischen dem flexiblen Schirm eines Hubtores und seinen Gurtbändern
IT1132111B (it) Dispositivo di chiusura e montaggio della testa di una bambola o pupazzo flessibile
FR2637196B1 (fr) Perfectionnements aux poupees a corps souple
DE59504416D1 (de) Flexible Verkleidung eines Übergangs
DE69434567D1 (de) Signalübertragungseinrichtung unter Verwendung eines festen und eines drehbaren Körpers
DE69116650T2 (de) Polyimidharz und dessen Zubereitung
DK75092A (da) Fleksibelt ringbind
DE59603298D1 (de) Fungizide mischungen eines oximethercarbonsäureamids mit einem dithiocarbamat
FR2566111B1 (fr) Dispositif de freinage aerodynamique du mouvement de rotation d'un corps
FR2617554B1 (fr) Perfectionnements aux dispositifs d'anti-retour angulaire associes aux tourniquets
DE69116789T2 (de) Anordnung zum Erzeugen einer Dreh- und Linearbewegung eines Körpers
DE69317751D1 (de) Struktur eines statischen Frequenzumwandlers
DE69411055T2 (de) Rotorkopf eines Drehflügelflugzeuges
DE8610769U1 (de) Körperpackung, vorzugsweise Gesichtsmaske für kosmetische und/oder therapeutische Zwecke
ATA24588A (de) Abgasfuehrung eines brennerbeheizten geraetes

Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: RAYTHEON CO. (N.D.GES.D. STAATES DELAWARE), LEXING