EP2083238A3 - Klappflügel mit Entfaltvorrichtung - Google Patents

Klappflügel mit Entfaltvorrichtung Download PDF

Info

Publication number
EP2083238A3
EP2083238A3 EP09000744.4A EP09000744A EP2083238A3 EP 2083238 A3 EP2083238 A3 EP 2083238A3 EP 09000744 A EP09000744 A EP 09000744A EP 2083238 A3 EP2083238 A3 EP 2083238A3
Authority
EP
European Patent Office
Prior art keywords
wing
unfolding device
folding
folding fin
folding 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.)
Granted
Application number
EP09000744.4A
Other languages
English (en)
French (fr)
Other versions
EP2083238B1 (de
EP2083238A2 (de
Inventor
Klaus Baumgartner
Herbert Gleisinger
Jürgen Rühe
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.)
MBDA Deutschland GmbH
Original Assignee
MBDA Deutschland GmbH
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 MBDA Deutschland GmbH filed Critical MBDA Deutschland GmbH
Publication of EP2083238A2 publication Critical patent/EP2083238A2/de
Publication of EP2083238A3 publication Critical patent/EP2083238A3/de
Application granted granted Critical
Publication of EP2083238B1 publication Critical patent/EP2083238B1/de
Ceased legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F42B10/16—Wrap-around fins
    • 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

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aerials With Secondary Devices (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Storing, Repeated Paying-Out, And Re-Storing Of Elongated Articles (AREA)

Abstract

Ein Klappflügel für einen Flugkörper umfasst eine mechanische Antriebseinrichtung zur Entfaltung des Klappflügels nach dessen Freigabe. Als Antrieb wird eine vorgespannte Spiralfeder (20) verwendet, welche mit einem Zugseil (21) gekoppelt ist, welches über einen doppelten Flaschenzug (2,3) geführt wird.
Der Klappflügel besteht aus einer Flügelwuzzel (13), einer inneren Flügelfläche (12) und einer äußeren Flügelfläche (9).
EP20090000744 2008-01-24 2009-01-21 Klappflügel mit Entfaltvorrichtung Ceased EP2083238B1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE200810005705 DE102008005705A1 (de) 2008-01-24 2008-01-24 Klappflügel mit Entfaltvorrichtung

Publications (3)

Publication Number Publication Date
EP2083238A2 EP2083238A2 (de) 2009-07-29
EP2083238A3 true EP2083238A3 (de) 2013-05-22
EP2083238B1 EP2083238B1 (de) 2014-01-08

Family

ID=40578683

Family Applications (1)

Application Number Title Priority Date Filing Date
EP20090000744 Ceased EP2083238B1 (de) 2008-01-24 2009-01-21 Klappflügel mit Entfaltvorrichtung

Country Status (2)

Country Link
EP (1) EP2083238B1 (de)
DE (2) DE102008005705A1 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104677199B (zh) * 2015-01-21 2016-07-13 浙江理工大学 一种单驱动多折叠舵面同步展开机构
DE102015014367B4 (de) 2015-11-06 2020-07-16 Mbda Deutschland Gmbh Klappflügel für einen Flugkörper und Flugkörper mit mindestens einem daran angeordneten Klappflügel
DE102015014368A1 (de) 2015-11-06 2017-05-11 Mbda Deutschland Gmbh Klappflügel für einen Flugkörper sowie einen Flugkörper mit mindestens einem daran angeordneten Klappflügel
DE102017113058B4 (de) 2017-06-14 2023-04-27 Deutsches Zentrum für Luft- und Raumfahrt e.V. Raumtransport-Fluggerät
CN108688793B (zh) * 2018-07-27 2023-11-24 中国工程物理研究院总体工程研究所 筒式发射无人机机翼折叠展开机构
US11685510B2 (en) 2018-11-01 2023-06-27 Viettel Group Wing deployment mechanism and design method using pneumatic technique
RU2730903C1 (ru) * 2019-09-10 2020-08-26 Акционерное общество "Машиностроительное конструкторское бюро "Факел" имени Академика П.Д. Грушина" Механизм раскрытия и стопорения аэродинамического руля с двумя осями складывания
CN112985190A (zh) * 2021-04-13 2021-06-18 西安航天动力技术研究所 一种涡卷弹簧式折叠弹翼展开机构
RU2770956C1 (ru) * 2021-12-21 2022-04-25 Акционерное общество "Машиностроительное конструкторское бюро "Факел" имени академика П.Д. Грушина Механизм раскрытия и стопорения рулей с двумя складывающимися секциями
CN116499315B (zh) * 2023-04-28 2025-11-21 南京理工大学 一种电磁铁锁定式巡飞弹弹翼折叠展开机构
CN118701278A (zh) * 2024-06-12 2024-09-27 哈尔滨工业大学 一种基于火工作动的绳驱式同步折叠机构

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2045687A1 (de) * 1970-09-16 1972-03-23 Dynamit Nobel Ag Thermische Auslösung von Flugkörperfunktionen
GB2140136A (en) * 1983-05-14 1984-11-21 British Aerospace Folding fin assembly for missiles
DE3838735A1 (de) * 1988-11-15 1990-05-31 Diehl Gmbh & Co Klapp-fluegel, insbesondere fuer ein geschoss
US5762294A (en) * 1997-03-31 1998-06-09 The United States Of America As Represented By The Secretary Of The Army Wing deployment device
GB2369177A (en) * 1989-06-02 2002-05-22 British Aerospace Aerofoil deployment system
US20040159227A1 (en) * 2003-02-18 2004-08-19 Lockheed Martin Corporation Apparatus and method for restraining and releasing a control surface

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2045687A1 (de) * 1970-09-16 1972-03-23 Dynamit Nobel Ag Thermische Auslösung von Flugkörperfunktionen
GB2140136A (en) * 1983-05-14 1984-11-21 British Aerospace Folding fin assembly for missiles
DE3838735A1 (de) * 1988-11-15 1990-05-31 Diehl Gmbh & Co Klapp-fluegel, insbesondere fuer ein geschoss
GB2369177A (en) * 1989-06-02 2002-05-22 British Aerospace Aerofoil deployment system
US5762294A (en) * 1997-03-31 1998-06-09 The United States Of America As Represented By The Secretary Of The Army Wing deployment device
US20040159227A1 (en) * 2003-02-18 2004-08-19 Lockheed Martin Corporation Apparatus and method for restraining and releasing a control surface

Also Published As

Publication number Publication date
DE202008018033U1 (de) 2011-04-14
EP2083238B1 (de) 2014-01-08
DE102008005705A1 (de) 2009-07-30
EP2083238A2 (de) 2009-07-29

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