CA1306384C - Mecanisme de deploiement des ailes d'un missile, a ressort de torsion - Google Patents

Mecanisme de deploiement des ailes d'un missile, a ressort de torsion

Info

Publication number
CA1306384C
CA1306384C CA000538281A CA538281A CA1306384C CA 1306384 C CA1306384 C CA 1306384C CA 000538281 A CA000538281 A CA 000538281A CA 538281 A CA538281 A CA 538281A CA 1306384 C CA1306384 C CA 1306384C
Authority
CA
Canada
Prior art keywords
wing
linkage
foldable
fixed
section
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 - Fee Related
Application number
CA000538281A
Other languages
English (en)
Inventor
Arthur M. Frank
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.)
Grumman Corp
Original Assignee
Grumman Aerospace Corp
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 Grumman Aerospace Corp filed Critical Grumman Aerospace Corp
Priority to CA000538281A priority Critical patent/CA1306384C/fr
Application granted granted Critical
Publication of CA1306384C publication Critical patent/CA1306384C/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Landscapes

  • Pivots And Pivotal Connections (AREA)
CA000538281A 1987-05-28 1987-05-28 Mecanisme de deploiement des ailes d'un missile, a ressort de torsion Expired - Fee Related CA1306384C (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA000538281A CA1306384C (fr) 1987-05-28 1987-05-28 Mecanisme de deploiement des ailes d'un missile, a ressort de torsion

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA000538281A CA1306384C (fr) 1987-05-28 1987-05-28 Mecanisme de deploiement des ailes d'un missile, a ressort de torsion

Publications (1)

Publication Number Publication Date
CA1306384C true CA1306384C (fr) 1992-08-18

Family

ID=4135767

Family Applications (1)

Application Number Title Priority Date Filing Date
CA000538281A Expired - Fee Related CA1306384C (fr) 1987-05-28 1987-05-28 Mecanisme de deploiement des ailes d'un missile, a ressort de torsion

Country Status (1)

Country Link
CA (1) CA1306384C (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108548457A (zh) * 2018-03-20 2018-09-18 浙江理工大学 一种导弹用单一动力源同步驱动式二次折叠展开机构
CN115979074A (zh) * 2022-12-21 2023-04-18 彩虹无人机科技有限公司 利用舵机解除折叠锁定的导弹尾翼折叠机构及导弹

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108548457A (zh) * 2018-03-20 2018-09-18 浙江理工大学 一种导弹用单一动力源同步驱动式二次折叠展开机构
CN108548457B (zh) * 2018-03-20 2023-12-05 浙江理工大学 一种导弹用单一动力源同步驱动式二次折叠展开机构
CN115979074A (zh) * 2022-12-21 2023-04-18 彩虹无人机科技有限公司 利用舵机解除折叠锁定的导弹尾翼折叠机构及导弹

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