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Command bar mechanism for flight director indicator
   
Document Number
US Patent 3988927
Issued Date
November 2, 1976
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Inventors
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Abstract
A command driving mechanism for command bars which are rotatable about the longitudinal axis of and transversely displaceable with respect to the horizontal reference line of a flight director indicator includes a command plate, the plane of which is parallel to the front face of the indicator. The perpendicular axis of the command plate is coaxial with the longitudinal axis of the indicator and rotatable thereon in accordance with roll commands. Command bar struts are pivotally supported at diametrically opposed peripheral portions of the command plate and connected through a wire bail which is driven by a helical cam in accordance with pitch commands.
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Command bar mechanism for flight director indicator - US Patent 3988927 Drawing
Drawing from US Patent 3988927
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Number of Claims:
3
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Owner
The Bendix Corporation (Southfield, MI)
Published
November 2, 1976
Application Number
05/609,636
Filed
September 2, 1975
US Classification
73/178R   116/DIG.43
Int'l Classification
G01C   19/00   (20060101)   G01C   19/32   (20060101)  
Examiner
Attorney/Law Firm
USPTO Field of Search
73/178R   73/178T   73/178H   116/DIG.43  
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Claims
Description
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