FR2637064A1 - Engin volant avec bague de rotor a gouverne orientable - Google Patents

Engin volant avec bague de rotor a gouverne orientable

Info

Publication number
FR2637064A1
FR2637064A1 FR8909837A FR8909837A FR2637064A1 FR 2637064 A1 FR2637064 A1 FR 2637064A1 FR 8909837 A FR8909837 A FR 8909837A FR 8909837 A FR8909837 A FR 8909837A FR 2637064 A1 FR2637064 A1 FR 2637064A1
Authority
FR
France
Prior art keywords
flying machine
orientable
rotor
ring
rotor ring
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.)
Granted
Application number
FR8909837A
Other languages
English (en)
Other versions
FR2637064B1 (fr
Inventor
Walter Kranz
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2637064A1 publication Critical patent/FR2637064A1/fr
Application granted granted Critical
Publication of FR2637064B1 publication Critical patent/FR2637064B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F42B10/60—Steering arrangements
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Multiple Motors (AREA)
  • Superconductive Dynamoelectric Machines (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)

Abstract

L'engin volant comprend une bague de rotor 3 qui présente au moins une gouverne 4, 5 orientable pouvant être actionnée par la rotation relative entre la bague de rotor 3 et l'engin volant 1, 2. Au moins un moteur est disposé entre la bague de rotor 3 et l'engin volant 1, 2, et il est prévu un dispositif de commande qui fait fonctionner le moteur comme générateur et commande l'orientation de la gouverne 4, 5.
FR8909837A 1988-08-13 1989-07-21 Engin volant avec bague de rotor a gouverne orientable Expired - Fee Related FR2637064B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3827590A DE3827590A1 (de) 1988-08-13 1988-08-13 Flugkoerper

Publications (2)

Publication Number Publication Date
FR2637064A1 true FR2637064A1 (fr) 1990-03-30
FR2637064B1 FR2637064B1 (fr) 1994-05-13

Family

ID=6360838

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8909837A Expired - Fee Related FR2637064B1 (fr) 1988-08-13 1989-07-21 Engin volant avec bague de rotor a gouverne orientable

Country Status (3)

Country Link
US (1) US4964593A (fr)
DE (1) DE3827590A1 (fr)
FR (1) FR2637064B1 (fr)

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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
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ES2398968T3 (es) * 2005-09-09 2013-03-22 General Dynamics Ordnance And Tactical Systems Sistema de control de la trayectoria de un proyectil
US10408587B1 (en) * 2006-04-20 2019-09-10 United States Of America As Represented By The Secretary Of The Army On-board power generation for rolling motor missiles
US7431237B1 (en) * 2006-08-10 2008-10-07 Hr Textron, Inc. Guided projectile with power and control mechanism
US7800032B1 (en) * 2006-11-30 2010-09-21 Raytheon Company Detachable aerodynamic missile stabilizing system
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US7963442B2 (en) * 2006-12-14 2011-06-21 Simmonds Precision Products, Inc. Spin stabilized projectile trajectory control
US7755012B2 (en) * 2007-01-10 2010-07-13 Hr Textron, Inc. Eccentric drive control actuation system
US7642491B2 (en) 2007-03-19 2010-01-05 Tom Kusic Aircraft spiraling mechanism with jet assistance—D
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US7791007B2 (en) * 2007-06-21 2010-09-07 Woodward Hrt, Inc. Techniques for providing surface control to a guidable projectile
US9040885B2 (en) * 2008-11-12 2015-05-26 General Dynamics Ordnance And Tactical Systems, Inc. Trajectory modification of a spinning projectile
US9127908B2 (en) 2009-02-02 2015-09-08 Aero Vironment, Inc. Multimode unmanned aerial vehicle
US8552351B2 (en) * 2009-05-12 2013-10-08 Raytheon Company Projectile with deployable control surfaces
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KR20120113210A (ko) 2009-09-09 2012-10-12 에어로바이론먼트, 인크. 휴대용 ｒｆ 투명 발사관을 구비한 원격 조종 무인 항공기 포성 억제 발사장치를 위한 시스템 및 장치
US8443726B2 (en) * 2010-02-10 2013-05-21 Omnitek Partners, Llc Miniature safe and arm (S and A) mechanisms for fuzing of gravity dropped small weapons
US8552349B1 (en) * 2010-12-22 2013-10-08 Interstate Electronics Corporation Projectile guidance kit
US8426788B2 (en) * 2011-01-12 2013-04-23 Raytheon Company Guidance control for spinning or rolling projectile
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US8698059B2 (en) 2012-05-03 2014-04-15 Raytheon Company Deployable lifting surface for air vehicle
IL224075A (en) * 2012-12-31 2017-11-30 Bae Systems Rokar Int Ltd Cheap shell kit and method of use
US20160238358A1 (en) * 2014-03-04 2016-08-18 Andrey SOROKIN Ammunition with electromotor
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FR3041744B1 (fr) * 2015-09-29 2018-08-17 Nexter Munitions Projectile d'artillerie ayant une phase pilotee.
DE102015013913A1 (de) * 2015-10-27 2017-04-27 Deutsch Französisches Forschungsinstitut Saint Louis Vollkalibriges, drallstabilisiertes Lenkgeschoss mit einer hohen Reichweite
FR3054030B1 (fr) * 2016-07-18 2018-08-24 Nexter Munitions Projectile comprenant un dispositif de deploiement d'une voilure ou ailette
US10618668B2 (en) * 2016-09-06 2020-04-14 Analytical Mechanics Associates, Inc. Systems and apparatus for controlling movement of objects through a fluid
US11555679B1 (en) 2017-07-07 2023-01-17 Northrop Grumman Systems Corporation Active spin control
US12031802B2 (en) * 2017-07-26 2024-07-09 Northrop Grumman Systems Corporation Despun wing control system for guided projectile maneuvers
US10996031B1 (en) * 2017-07-26 2021-05-04 U.S. Government As Represented By The Secretary Of The Army Free spinning hub for mortar projectiles
US10718294B1 (en) 2017-10-27 2020-07-21 United Launch Alliance, L.L.C. Integrated vehicle fluids
US11578956B1 (en) 2017-11-01 2023-02-14 Northrop Grumman Systems Corporation Detecting body spin on a projectile
CN108801242B (zh) * 2018-04-28 2021-06-29 沈阳理工大学 一种高动态环境下的组合式姿态测量方法
IL263880B (en) * 2018-12-20 2022-02-01 Elbit Systems Rokar Ltd A thundering assembly of a shell guidance kit and methods for its installation and use
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Publication number Priority date Publication date Assignee Title
US4438893A (en) * 1973-08-10 1984-03-27 Sanders Associates, Inc. Prime power source and control for a guided projectile

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FR2321723A1 (fr) * 1975-07-29 1977-03-18 Thomson Brandt Systeme de controle d'attitude et engin equipe d'un tel systeme
AU546338B2 (en) * 1980-09-22 1985-08-29 Commonwealth Of Australia, The Stabilising rotating body
US4565340A (en) * 1984-08-15 1986-01-21 Ford Aerospace & Communications Corporation Guided projectile flight control fin system
DE3645077C2 (de) * 1986-02-27 1996-06-27 Daimler Benz Aerospace Ag Vorrichtung zum Steuern von Flugkörpern

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4438893A (en) * 1973-08-10 1984-03-27 Sanders Associates, Inc. Prime power source and control for a guided projectile

Also Published As

Publication number Publication date
US4964593A (en) 1990-10-23
DE3827590A1 (de) 1990-02-22
DE3827590C2 (fr) 1992-01-23
FR2637064B1 (fr) 1994-05-13

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