TWO AXIS DRIVE FOR STAGE
Assignee
Hughes Aircraft
Filed as: HUGHES AIRCRAFT COMPANY
Filed
Aug 11, 1982
Granted
Jul 9, 1985
Location
LOS ANGELES CA US
Abstract
Stage 12 is moved into position by traction of capstan 38 on bar 42 which is pivoted under intermediate plate 20, and by traction on bar 66 which is pivoted under stage plate 12. Bar 42 is pressed against motor driven capstan 38 by pressure rollers 44 and 46. The pressure rollers are mounted on a rotatable yoke 50 so that the bar can freely swing and only applies longitudinal forces to the plate. This same structure is provided for drive bar 66.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Dec 30, 1982
Rescinded
Nov 17, 1983
Duration
10 months
Inventor
- 1SIEGFRIED HANSEN
Record Details
- Patent number
- US 4528490
- Application
- 06407024
- Aerospace match
- No
- Dataset source
- 35 USC §181 SO records
Browse by Assignee
Hughes AircraftMore from this assignee
DIGITAL CIRCUIT WITH TRANSISTOR GEOMETRY AND CHANNEL STOPS PROVIDING CAMOUFLAGE AGAINST REVERSE ENGINEERING
Hughes Aircraft
MISSILE FIRE CONTROL SYSTEM
Hughes Aircraft
COORDINATE TRANSFORMATION SYSTEM
Hughes Aircraft
POLYROD ANTENNA WITH FLARED NOTCH FEED
Hughes Aircraft
NEAR-RANGE MICROWAVE DETECTION FOR FREQUENCY-MODULATION CONTINUOUS- WAVE AND STEPPED FREQUENCY RADAR SYSTEMS
Hughes Aircraft
LINEAR ARRAY LATERAL MOTION COMPENSATION METHOD
Hughes Aircraft