Transport element clamp system
Transport element clamp system
- New search for: GILBERTSON MICHAEL LESLIE
- New search for: MICHEL JON P
- New search for: CARPENTER MARK L
- New search for: GILBERTSON MICHAEL LESLIE
- New search for: MICHEL JON P
- New search for: CARPENTER MARK L
TRANSPORTELEMENTCLAMPSYSTEM A transport element clamp system (206) comprising a lower portion (222), an upper portion (224), and a channel system (226). The lower portion (222) has a first number of cutouts (228) and the upper portion (224) has a second number of cutouts (230). The lower portion (222) is configured to bridge a gap (220) between two support structures (202) in an aircraft (201). The upper portion (224) is configured to interlock with the lower portion (222). The channel system (226) is formed by the first number of cutouts (228) and the second number of cutouts (230). The channel system (226) is configured to receive a number of transport elements (208) when the upper portion (224) and the lower portion (222) are coupled to each other. The transport element clamp system (206) electrically isolates the number of transport elements (204) from the two support structures (202). clco v o
Document information
Transport element clamp system
2023-10-19
Patent
Electronic Resource
English
| IPC: | B64C AEROPLANES , Flugzeuge |