US2007075183A1PendingUtilityA1

Wing arrangement as well as a missile

Assignee: DIEHL BGT DEFENCE GMBH & CO KGPriority: Jun 7, 2005Filed: May 16, 2006Published: Apr 5, 2007
Est. expiryJun 7, 2025(expired)· nominal 20-yr term from priority
F42B 10/06
32
PatentIndex Score
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Cited by
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References
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Claims

Abstract

A wing arrangement ( 10 ), which can be pushed onto a structure, such as a missile, and which includes a number of tubular segments ( 14 ) and a number of wings ( 16 ) which are arranged on the tubular segments ( 14 ). In order to allow the wing arrangement ( 10 ) to be pushed on over a missile, it includes structure for expandable connection of the tubular segments ( 14 ). Also provided is a missile having a wing arrangement ( 10 ) of that kind.

Claims

exact text as granted — not AI-modified
1 . A wing arrangement ( 10 ), which is pushable onto a structure, such as a missile, wherein said wing arrangement has a number of tubular segments ( 14 ) and a number of wings ( 16 ) which are arranged on the tubular segments ( 14 ), and includes means for expandable connection of the tubular segments ( 14 ).  
   
   
       2 . A wing arrangement ( 10 ) according to  claim 1 , wherein the means for expandable connection is formed by wing parts.  
   
   
       3 . A wing arrangement ( 10 ) according to  claim 2 , wherein the tubular segments ( 14 ) are each connected via two wing faces ( 18 ,  20 ) which form the wing ( 16 ), said wing faces point outwardly and meet one another at an angle.  
   
   
       4 . A wing arrangement ( 10 ) according to  claim 3 , wherein reinforcing means are provided between the wing faces ( 18 ,  20 ).  
   
   
       5 . A wing arrangement ( 10 ) according to  claim 3  wherein apertures ( 24 ) for attachment of the wing arrangement to a missile are provided in the wing faces ( 18 ,  20 ), in the area of a root ( 22 ) of a wing ( 16 ).  
   
   
       6 . A wing arrangement ( 10 ) according to  claim 3 , wherein the wing arrangement ( 10 ) is manufactured from sheet steel.  
   
   
       7 . A wing arrangement ( 10 ) according to  claim 1 , wherein the wing arrangement ( 10 ) has a wall thickness which is less than 0.7 mm.  
   
   
       8 . A missile incorporating a wing arrangement ( 10 ) according to  claim 1 .  
   
   
       9 . A missile according to  claim 8 , wherein the wing arrangement ( 10 ) is adhesively bonded to said missile.  
   
   
       10 . A missile according to  claim 8 , wherein said missile has a plurality of webs ( 26 ) fitted thereon, said wing arrangement ( 10 ) being attached to said webs.

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