SU545785A1 - Болт - Google Patents
БолтInfo
- Publication number
- SU545785A1 SU545785A1 SU2131207A SU2131207A SU545785A1 SU 545785 A1 SU545785 A1 SU 545785A1 SU 2131207 A SU2131207 A SU 2131207A SU 2131207 A SU2131207 A SU 2131207A SU 545785 A1 SU545785 A1 SU 545785A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- bolt
- Prior art date
Links
Landscapes
- Control Of Motors That Do Not Use Commutators (AREA)
- Finger-Pressure Massage (AREA)
- Laying Of Electric Cables Or Lines Outside (AREA)
Description
(54) БОЛТ
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU2131207A SU545785A1 (ru) | 1975-05-04 | 1975-05-04 | Болт |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU2131207A SU545785A1 (ru) | 1975-05-04 | 1975-05-04 | Болт |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SU545785A1 true SU545785A1 (ru) | 1977-02-05 |
Family
ID=20618464
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SU2131207A SU545785A1 (ru) | 1975-05-04 | 1975-05-04 | Болт |
Country Status (1)
| Country | Link |
|---|---|
| SU (1) | SU545785A1 (ru) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4718801A (en) * | 1986-07-24 | 1988-01-12 | Microdot Inc. | Composite core fastener |
| US4824314A (en) * | 1985-02-19 | 1989-04-25 | Northrop Corporation | Composite fastener system and manufacturing method thereof |
| WO2014130184A1 (en) * | 2013-02-21 | 2014-08-28 | The Boeing Company | Hybrid fastener and method of making the same |
| US9205579B2 (en) | 2009-11-06 | 2015-12-08 | The Boeing Company | Compression molding method and reinforced thermoplastic parts molded thereby |
| FR3029580A1 (fr) * | 2014-12-09 | 2016-06-10 | Airbus Operations Sas | Vis pour moyen d'assemblage de deux pieces |
| US9623612B2 (en) | 2013-02-21 | 2017-04-18 | The Boeing Company | Method for fabricating composite fasteners |
-
1975
- 1975-05-04 SU SU2131207A patent/SU545785A1/ru active
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4824314A (en) * | 1985-02-19 | 1989-04-25 | Northrop Corporation | Composite fastener system and manufacturing method thereof |
| US4718801A (en) * | 1986-07-24 | 1988-01-12 | Microdot Inc. | Composite core fastener |
| US9205579B2 (en) | 2009-11-06 | 2015-12-08 | The Boeing Company | Compression molding method and reinforced thermoplastic parts molded thereby |
| WO2014130184A1 (en) * | 2013-02-21 | 2014-08-28 | The Boeing Company | Hybrid fastener and method of making the same |
| US9238339B2 (en) | 2013-02-21 | 2016-01-19 | The Boeing Company | Hybrid fastener and method of making the same |
| US9623612B2 (en) | 2013-02-21 | 2017-04-18 | The Boeing Company | Method for fabricating composite fasteners |
| US10328643B2 (en) | 2013-02-21 | 2019-06-25 | The Boeing Company | Apparatus for fabricating composite fasteners |
| US10350718B2 (en) | 2013-02-21 | 2019-07-16 | The Boeing Company | Hybrid fastener and method of making the same |
| FR3029580A1 (fr) * | 2014-12-09 | 2016-06-10 | Airbus Operations Sas | Vis pour moyen d'assemblage de deux pieces |
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