STRUT ASSEMBLY AND METHOD OF FORMING

A strut assembly 20, 120 for an aircraft 10 can include a hollow rod 21, 121 having a body 22, 122 with distal ends 24, 26, 124, 126 spaced apart by a length 28 of the body 22, 122. A wire rope 30, 130 can be operably coupled to the hollow rod 21, 121, where ends 31, 32, 131, 132 of the rope 30, 130...

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Bibliographische Detailangaben
Hauptverfasser:	SONI, Navin, TAMARTHI, David Raju, SM, Khaja Mohiddin, THAKARE, Dhiraj, KUMAR, Sandeep, NAYAK, Subrata
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BEARINGS BLASTING COSMONAUTICS ELEMENTS OR CRANKSHAFT MECHANISMS ENGINEERING ELEMENTS AND UNITS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLEXIBLE SHAFTS FLYING SUITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS ROTARY BODIES OTHER THAN GEARING ELEMENTS SHAFTS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A strut assembly 20, 120 for an aircraft 10 can include a hollow rod 21, 121 having a body 22, 122 with distal ends 24, 26, 124, 126 spaced apart by a length 28 of the body 22, 122. A wire rope 30, 130 can be operably coupled to the hollow rod 21, 121, where ends 31, 32, 131, 132 of the rope 30, 130 can be coupled to the distal ends 24, 26, 124, 126 of the hollow rod 21, 121.