or
Bookmark and Share
Belt driven gyroscopic instrument for an aircraft
   
Document Number
US Patent 3911591
Issued Date
October 14, 1975
Link
Inventors
Map
Abstract
An improvement in panel-mounted gyroscopic attitude indicators for aircraft of the type having a generally spherical indicating element on which a horizon line divides the element into upper sky and lower ground portions. The indicating sphere is supported in an instrument housing with full roll freedom by a roll gimbal yoke directly attached to and driven in roll by a forward enlarged trunion of the full closed roll gimbal of a vertical gyroscope. The sphere is driven in pitch by a pulley and belt drive mechanism wherein the vertical gyro inner or pitch gimbal carries the drive pulley and the sphere carries the driven pulley. To provide the conventional "inside out" or reversed pitch sensing, the belt is reeved on the pulleys and in crossed or in "figure eight" fashion with the belt crossing or intersection located within the said enlarged forward trunion of the roll gimbal.
Drawing
Belt driven gyroscopic instrument for an aircraft - US Patent 3911591 Drawing
Drawing from US Patent 3911591
Tags:
Description:
Amusing 0%
Clever 0%
Complex 0%
Efficient 0%
Historic 0%
Important 0%
Innovative 0%
Interesting 0%
Practical 0%
Simple 0%
Number of Claims:
5
Comments:
no comments yet
Owner
Published
October 14, 1975
Application Number
05/238,599
Filed
March 27, 1972
US Classification
33/330  
Int'l Classification
G01C   19/00   (20060101)   G01C   19/44   (20060101)  
Examiner
USPTO Field of Search
33/328   33/329   33/330  
Related Patents
Claims
Description
About| FAQs| Terms & Disclaimer| Link to Us| Contact Us