Inertial sensor support structure for accelerometers and gyros

- Honeywell Inc.
Description

FIG. 1 is a perspective view of the inertial sensor support showing mounting surfaces for gyros;

FIG. 2 is a left side perspective of FIG. 1;

FIG. 3 is a rear view of the perspective of FIG. 1;

FIG. 4 is a bottom view of the perspective of FIG. 1 rotated 180.degree. showing mounting surfaces for accelerometers; and,

FIG. 5 is a bottom view of FIG. 1 rotated 90.degree..

Referenced Cited
U.S. Patent Documents
D317132 May 28, 1991 Knipfer et al.
3269179 August 1966 Anderson
3489004 January 1970 Barnhill et al.
Other references
  • Honeywell Air Transport Sys. Div.-Charles R. McClary, Position, Location, Navigation Symposium 1992. ADIRS; Fault-Tolerant; no date provided.
Patent History
Patent number: D352299
Type: Grant
Filed: Mar 19, 1993
Date of Patent: Nov 8, 1994
Assignee: Honeywell Inc. (Minneapolis, MN)
Inventors: Lucien E. Joly (Cook, MN), Michael A. Knipfer (Maple Grove, MN), Michelle J. Miller (Minneapolis, MN), George O. Mitzschke (St. Petersburg, FL), Mark T. Weinberger (Mounds View, MN)
Primary Examiner: Nelson C. Holtje
Assistant Examiner: Antoine D. Davis
Attorney: Robert A. Pajak
Application Number: 0/5,969
Classifications
Current U.S. Class: Miscellaneous (D15/199)