METHOD OF CONSTRUCTING A MOMENT INSENSITIVE PATHLENGTH CONTROL MIRROR ASSEMBLY FOR A RING LASER GYROSCOPE
Assignee
SINGER COMPANY, THE, EIGHT STAMFORD FORUM, STANFORD, CONN 06904 A CORP. OF NJ
Filed
Mar 18, 1988
Granted
Aug 29, 1989
Location
WAYNE NJ US
Abstract
In a precision ring laser gyroscope, to eliminate the effect of an unwanted and unintentional moment generated as a result of a force being applied onto a pathlength controller, a pathlength control assembly is constructed to have optimal hub and diaphragm portions such that the mirror element mounted thereto does not tilt in response to the unintentional moment.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Jan 18, 1989
Rescinded
Mar 10, 1989
Duration
1 month
Inventor
- 1BO H. G. LJUNG
Technology Domains
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Record Details
- Patent number
- US 4861161
- Application
- 07169668
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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