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A platform for research: civil engineering, architecture and urbanism
WEAR RESISTANT SLEEVE FOR COMPOSITE CYLINDER
A rod assembly includes a tubular rod body (52) formed from a composite material and a localized sleeve (54) installed to the rod body. The sleeve is secured to the rod body by application of heat to the sleeve material. A bushing (56) is located radially between the rod body and the sleeve. The bushing is configured to absorb thermal energy of the application of heat. A door and hold open rod assembly of an aircraft includes a door, and a hold open rod (22) assembly secured to the door. The hold open rod assembly is configured to support the door in an opened position when the hold open rod is deployed. The hold open rod assembly includes a tubular rod body formed from a composite material, and a localized sleeve installed to the rod body. A bushing is located radially between the rod body and the sleeve.
WEAR RESISTANT SLEEVE FOR COMPOSITE CYLINDER
A rod assembly includes a tubular rod body (52) formed from a composite material and a localized sleeve (54) installed to the rod body. The sleeve is secured to the rod body by application of heat to the sleeve material. A bushing (56) is located radially between the rod body and the sleeve. The bushing is configured to absorb thermal energy of the application of heat. A door and hold open rod assembly of an aircraft includes a door, and a hold open rod (22) assembly secured to the door. The hold open rod assembly is configured to support the door in an opened position when the hold open rod is deployed. The hold open rod assembly includes a tubular rod body formed from a composite material, and a localized sleeve installed to the rod body. A bushing is located radially between the rod body and the sleeve.
WEAR RESISTANT SLEEVE FOR COMPOSITE CYLINDER
VERSCHLEISSFESTE HÜLSE FÜR VERBUNDZYLINDER
MANCHON RÉSISTANT À L'USURE POUR CYLINDRE COMPOSITE
VENUGOPAL SANJAY (author) / TRIPATHI AMIT KUMAR (author) / KRISHNAPPA RAJIV (author)
2024-06-19
Patent
Electronic Resource
English
IPC:
B64D
Ausrüstung für Flugzeuge
,
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
/
B23P
Sonstige Metallbearbeitung
,
OTHER WORKING OF METAL
/
B64C
AEROPLANES
,
Flugzeuge
/
E05C
Riegel oder Feststellvorrichtungen für Flügel, insbesondere für Türen oder Fenster
,
BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS
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