A spherical gas bearing for airborne applicationA spherical gas bearing is analyzed and tested for an airborne application. The externally pressurized bearing supports an inertially stabilized 36-in aperture, infrared telescope. The bearing provides the isolation of rotary motion from the aircraft and also serves as a seal between the aircraft cabin and cavity condition at 50,000 ft altitude. The accompanying temperature gradient of 135 F across the 16-in.-diam bearing created special design and manufacturing considerations. Test data on the static load under temperature and vacuum environment are presented in support of the analysis.
Document ID
19740045939
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bouvier, A.
Schmertz, J. C. (Owens-Illinois, Inc. Pittsburgh, Pa., United States)