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COMMAND BAR MECHANISM FOR FLIGHT DIRECTOR INDICATOR AIRCRAFT INSTRUMENT
   
Document Number
US Patent 3654597
Issued Date
April 4, 1972
Link
Inventors
Cox; Ronald E. (Cedar Rapids, IA)
Map
Abstract
A compact positioning mechanism for an indicator assembly of the type comprising first and second bar members arranged in a V-like configuration and collectively defining a command plane which is both rotatable about and transversely displaceable with respect to a reference axis. A pair of ring members, each formed with a camming surface, carry the respective bar members on a cam follower pivotably mounted on one ring and in camming engagement with the cam surface on the other. Rotation of the command plane is achieved through like rotation of the two rings while displacement transverse of the reference axis is achieved by relative rotation between the two rings.
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COMMAND BAR MECHANISM FOR FLIGHT DIRECTOR INDICATOR AIRCRAFT INSTRUMENT - US Patent 3654597 Drawing
Drawing from US Patent 3654597
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Number of Claims:
8
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Owner
Collins Radio Company (Cedar Rapids, IA)
Published
April 4, 1972
Application Number
05/061,953
Filed
August 7, 1970
US Classification
340/975   340/979 342/443
Int'l Classification
G01C   23/00   (20060101)   G01C   19/32   (20060101)   G01C   19/00   (20060101)  
Assistant Examiner
USPTO Field of Search
340/27R   340/27AT   340/27NA   343/18R   343/18SM   343/112PT   343/112R   73/178R  
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Claims
Description
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