Machine element or mechanism – Gyroscopes – With caging or parking means
Patent
1991-10-28
1995-02-21
Brown, David
Machine element or mechanism
Gyroscopes
With caging or parking means
310 90, G01C 1976, F16C 3900
Patent
active
053905547
ABSTRACT:
A spacecraft component bearing unit for resisting axial lead due to launch vibration. This component includes a stator having drive coils, an inertia wheel having a ring magnet, a shaft having a fixed upper bearing cartridge and a floating lower bearing cartridge mounted on the stator and supporting the inertia wheel, three snubber units spaced peripherally at equal angles around an axis of the shaft, and each snubber unit having a piston with a face engaging the shaft and having a bellows connected to the piston for withdrawing the piston from contact with the shaft upon exposure to vacuum pressure at launch completion.
REFERENCES:
patent: 2959695 (1960-11-01), Huff
patent: 4182967 (1980-01-01), Jordan
patent: 4211452 (1980-07-01), Poubeau
patent: 4566740 (1986-01-01), Beau et al.
patent: 4872357 (1989-10-01), Vaillant De Guelis et al.
patent: 5027926 (1991-07-01), Cox
Brown David
Honeywell Inc.
Rendos Thomas A.
LandOfFree
Spacecraft component bearing does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Spacecraft component bearing, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Spacecraft component bearing will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-1923029