GB548904A - Improvements in or relating to the installation of electrical instruments on aircraft - Google Patents
Improvements in or relating to the installation of electrical instruments on aircraftInfo
- Publication number
- GB548904A GB548904A GB131641A GB131641A GB548904A GB 548904 A GB548904 A GB 548904A GB 131641 A GB131641 A GB 131641A GB 131641 A GB131641 A GB 131641A GB 548904 A GB548904 A GB 548904A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- nut
- installation
- attached
- relating
- 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
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
- H02G3/00—Installations of electric cables or lines or protective tubing therefor in or on buildings, equivalent structures or vehicles
- H02G3/02—Details
- H02G3/08—Distribution boxes; Connection or junction boxes
- H02G3/12—Distribution boxes; Connection or junction boxes for flush mounting
- H02G3/123—Distribution boxes; Connection or junction boxes for flush mounting in thin walls
Landscapes
- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Connector Housings Or Holding Contact Members (AREA)
Abstract
548,904. Two-part couplings ; plug boards. TRIGGS, W. W. (Lapco Soc. Anon.). Jan. 31, 1941, No. 3616. [Class 38 (i)] Interconnection of the wiring installation of an aircraft is effected by a junction box 1, the internal connections of which are brought out to multiple socket fittings to receive multiple plugs 2 attached to cables 3 leading to a source of current 4 and the various instruments 5, 6, 7. The box is built up of readily separable parts, a base 10 attached to a support, a polygonal wall 11 carrying the socket fittings, and a cover 12, all secured together by a stud 16 and nut 18. When the nut is removed the internal connections are accessible from both sides of the part 11.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB131641A GB548904A (en) | 1941-01-31 | 1941-01-31 | Improvements in or relating to the installation of electrical instruments on aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB131641A GB548904A (en) | 1941-01-31 | 1941-01-31 | Improvements in or relating to the installation of electrical instruments on aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB548904A true GB548904A (en) | 1942-10-29 |
Family
ID=9719870
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB131641A Expired GB548904A (en) | 1941-01-31 | 1941-01-31 | Improvements in or relating to the installation of electrical instruments on aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB548904A (en) |
-
1941
- 1941-01-31 GB GB131641A patent/GB548904A/en not_active Expired
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