Measuring and testing – Speed – velocity – or acceleration – Angular rate using gyroscopic or coriolis effect
Patent
1978-04-06
1979-04-17
Gill, James J.
Measuring and testing
Speed, velocity, or acceleration
Angular rate using gyroscopic or coriolis effect
74 51, 74 542, G01P 902, G01C 1930
Patent
active
041494180
ABSTRACT:
A turn rate indicator for an aircraft includes magnetic substance pieces facing each other, one being rotatable integrally with a gimbal and the other being fixed to a body. Because of the attracting force generated between the magnetic substance pieces, a pointer of the indicator returns to its zero point smoothly and certainly.
REFERENCES:
patent: 1713930 (1929-05-01), Sperry
patent: 2924978 (1960-02-01), Barnes
Gill James J.
Tokyo Aircraft Instrument Co. Ltd.
LandOfFree
Turn rate indicator of aircraft with improved zero seeking chara does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Turn rate indicator of aircraft with improved zero seeking chara, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turn rate indicator of aircraft with improved zero seeking chara will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-1256518