US4852347A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Advanced composite polar boss
Assignee: United States Department of the Air Force
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Filing: 1987-10-16
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Granted: 1989-08-01
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Expires: 2007-10-16
Abstract
Abstract Composite polar bosses applied in rocket motor cases have very desirable characteristics. The lead time for a boss can be reduced from 6-12 months to 4-6 months. Weight savings for the boss/nozzle assembly are about 20-40 percent. A composite polar boss which attaches nozzle assemblies to solid fueled rocket motor cases is disclosed. This polar boss is a carbonized fabrication which sits within a circumferential indentation within the motor case, and has a threaded inner circumference which permits the nozzle assembly to be attached thereto. The materials of the boss are selected to permit a service temperature of up to 3,200 degrees F.
Inventors
- 👤 Hugh M. Reynolds
- 👤 Curt M. Kawabata
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-24 08:56
CPC Classifications
F; F02; F02K; F02K9/00; F02K9/08; F02K9/32; F02K9/34; C; C04; C04B; C04B35/00; C04B35/71; C04B35/78; C04B35/80; C04B35/83; Y; Y10; Y10S; Y10S60/00; Y10S60/909
Claims Analysis
Total Claims: 2
Claim 1
Independent Claim
179 words
A composite polar boss for attaching a nozzle assembly to a solid fueled rocket motor case, said solid fueled rocket motor case having an exhaust opening which has an indentation which circumscribes its inner circumference, said composite polar boss comprising: an annular billet which forms a ring with an outer circumference which is shaped to fit within the indentation of the solid fueled rocket motor case, said annular billet thereby being fixed to said solid fueled rocket motor case, said annular billet having a threaded inner circumference which screws onto a complementary set of threads on said nozzle assembly to attach it to said fueled rocket motor case, said annular billet being constructed of materials which enable it to withstand service temperatures of up to about 1,200 degrees F., wherein said annular billet is composed of carbon-carbon fabricated material which is machined into said ring with said set of threads machined onto its inner circumference, and wherein said carbon-carbon fabricated material includes 2D and 3D fabrics which have been impregnated with a resin and carbonized into said annular billet.
Claim 2
Dependent Claim
179 words
A composite polar boss for attaching a nozzle assembly to a solid fueled rocket motor case, said solid fueled rocket motor case having an exhaust opening which has an indentation which circumscribes its inner circumference, said composite polar boss comprising: an annular billet which forms a ring with an outer circumference which is shaped to fit within the indentation of the solid fueled rocket motor case, said annular billet thereby being fixed to said solid fueled rocket motor case, said annular billet having a threaded inner circumference which screws onto a complementary set of threads on said nozzle assembly to attach it to said fueled rocket motor case, said annular billet being constructed of materials which enable it to withstand service temperatures of up to about 1,200 degrees F., wherein said annular billet is composed of carbon-carbon fabricated material which is machined into said ring with said set of threads machined onto its inner circumference, and wherein said carbon-carbon fabricated material includes 2D and 3D fabrics which have been impregnated with a resin and carbonized into said annular billet.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1992-07-31 | 1993-01-30 | 1993-08-01 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1996-07-31 | 1997-01-30 | 1997-08-01 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2000-07-31 | 2001-01-30 | 2001-08-01 | $7700.00 | Window Closed / Lapsed |