Robert Douglass Gates
Engineers at Blackstone Ct, Littleton, CO

License number
Colorado 14088
Issued Date
Jun 15, 1976
Renew Date
Feb 1, 2007
Expiration Date
Jan 31, 2009
Type
Professional Engineer
Address
Address
1531 E Blackstone Ct, Littleton, CO 80126

Professional information

Robert Gates Photo 1

Gas Bearing Reaction Wheel

US Patent:
3936682, Feb 3, 1976
Filed:
Sep 14, 1972
Appl. No.:
5/289028
Inventors:
Robert Lee Gates - Littleton CO
Assignee:
Martin Marietta Corporation - New York NY
International Classification:
H02k 700
US Classification:
310 66
Abstract:
An intermediate rotatable member is driven at relatively high speed about a common axis and is concentrically positioned between first and second relatively rotatable members, one of which is bidirectionally driven with respect to the other. Hydrodynamic fluid bearings are carried by the intermediate member on both surfaces thereof and acting on the first and second members, thus even upon cessation of motion, between said first and second members, there is no loss of the hydrodynamic fluid bearings between the first, second and third members.


Robert Gates Photo 2

Isolation System

US Patent:
4270393, Jun 2, 1981
Filed:
Mar 12, 1979
Appl. No.:
6/019680
Inventors:
Norman A. Osborne - Englewood CO
Robert L. Gates - Littleton CO
Assignee:
Martin Marietta Corporation - Bethesda MD
International Classification:
G01C 1916
US Classification:
74 5F
Abstract:
A vibration-isolating apparatus having orthogonal X, Y, and Z axes is provided for mounting a payload to a base. The payload contains a torque producing device. Torque generated about the X-axis in the payload is communicated to the base through a stiff linkage in the rotational degree of freedom about the X-axis. The apparatus includes first and second support frames, the payload mounted on the first support frame and the second support frame mounted to the base. Gimbal means permit rotation of the payload about the Y and Z axes. Linear dampening means dampen forces between the payload and base communicated linearly along the X, Y and Z axes and rotation dampening means dampen forces between the payload and base communicated rotationally about the Y and Z axes.