GB648675A - Improvements in electrical plug and socket connectors - Google Patents
Improvements in electrical plug and socket connectorsInfo
- Publication number
- GB648675A GB648675A GB706847D GB706847D GB648675A GB 648675 A GB648675 A GB 648675A GB 706847 D GB706847 D GB 706847D GB 706847 D GB706847 D GB 706847D GB 648675 A GB648675 A GB 648675A
- Authority
- GB
- United Kingdom
- Prior art keywords
- block
- shell
- socket
- plug
- key
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
- H01R13/46—Bases; Cases
- H01R13/502—Bases; Cases composed of different pieces
- H01R13/5025—Bases; Cases composed of different pieces one or more pieces being of resilient material
Landscapes
- Details Of Connecting Devices For Male And Female Coupling (AREA)
Abstract
648,675. Two-part couplings. BENDIX AVIATION CORPORATION. March 13, 1947, No. 7067. Addition to 632,501. [A Specification was laid open to inspection under Sect. 91 of the Acts, Aug. 12, 1946.] [Class 38 (i)] In a plug-and-socket connector 5, 6 of the kind described in the parent Specification, and comprising rigid shells 7, 32 and soft resilient contact-carrying blocks 18, 43 each slid axially into its respective shell, and readily removable thereform, the shells have circumferential lands 10, 39 which interengage with grooves 27, 48 in the blocks to locate each block in its correct position. The plug 5 and socket 6 can be fastened together by a screw-ring 17 and the block 18 is located within the shell 7 by the interengagement of its keyway 30 with a shell key 14, a similar engagement 51, 42 being provided for the block 43 and the shell 32. The key-ways 30, 51 are located in diametral alignment with two holes for the pin and socket contacts, 36, 20. The diameters of the lands 10, 39 are greater than those of the adjacent block ends but less than the diameters of the block mid-portions 25, 37, the abutment surfaces 12 and 50 of the lands being bevelled to permit the blocks to be forced into position after being correctly orientated. The other land abutment surfaces 28, 49 are flat. Key 35 and keyway 13 on the shells ensure the proper coupling of the plug and socket.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB706847D GB648675A (en) | 1947-03-13 | 1947-03-13 | Improvements in electrical plug and socket connectors |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB706847D GB648675A (en) | 1947-03-13 | 1947-03-13 | Improvements in electrical plug and socket connectors |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB648675A true GB648675A (en) | 1951-01-10 |
Family
ID=9825999
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB706847D Expired GB648675A (en) | 1947-03-13 | 1947-03-13 | Improvements in electrical plug and socket connectors |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB648675A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1460723A2 (en) * | 2003-03-21 | 2004-09-22 | The Boeing Company | Connector interface pad for structurally integrated wiring |
-
1947
- 1947-03-13 GB GB706847D patent/GB648675A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1460723A2 (en) * | 2003-03-21 | 2004-09-22 | The Boeing Company | Connector interface pad for structurally integrated wiring |
| EP1460723B1 (en) * | 2003-03-21 | 2017-01-25 | The Boeing Company | Connector interface pad for structurally integrated wiring |
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