TEMPERATURE NORMALIZED STRUCTURE
Assignee
ROCKWELL INTERNATIONAL CORP.
Filed
Dec 7, 1989
Granted
Apr 26, 1994
Location
El Segundo CA (Aerospace Corp/TRW)
Abstract
Circulation of temperature controlled fluid through cavities in structure stiffening members of hypersonic aerospace vehicles precludes destructive temperature gradients in such members and preserves stress residuals for functional requirements.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Mar 30, 1990
Rescinded
Aug 18, 1993
Duration
3 years, 4 months
Inventor
- 1HARRY SHORTLAND
Sensitive facility: El Segundo CA (Aerospace Corp/TRW)
Record Details
- Patent number
- US 5305973
- Application
- 07447347
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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