Part one points out the adequacy of a consideration of the steady state gyroscopic motion as a basis for the discussion of displacements of the gyroscope mounted on an airplane, and develops a simple theory on this basis. Principal types of gyroscopic inclinometers are described and requirements stated. Part two describes a new type of stabilizing gyro mounted on top of a spindle by means of a universal joint, the spindle being kept in a vertical position by supporting it as a pendulum of which the bob is the driving motor. Methods of tests and the difficulties in designing a satisfactory and reliable compass for aircraft use in considered in part three. Part four contains a brief general treatment of the important features of construction of aircraft compasses and description of the principal types used.
Aeronautic Instruments. Section IV : Direction Instruments
1923-01-01
Miscellaneous
No indication
English
Aeronautic instruments. Section V : power plant instruments
Engineering Index Backfile
|Aeronautic instruments. Section III : aircraft speed instruments
Engineering Index Backfile | 1923
|NTRS | 1924
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