Turbomachine casing comprising an endoscopy port

A turbomachine casing (10) comprising an endoscopy port (12) and a member (14) mounted on and fixed to the casing and comprising a duct (16) that communicates with the port and that comprises an internal thread into which a cap (28) can be screwed, and means (22, 26) for fixing the member to the cas...

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Bibliographische Detailangaben
Hauptverfasser:	Durand, Didier Noel, Jamon, Thibault, Leutard, Florence Irene Noelle
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ENGINE PLANTS IN GENERAL EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PARACHUTES PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A turbomachine casing (10) comprising an endoscopy port (12) and a member (14) mounted on and fixed to the casing and comprising a duct (16) that communicates with the port and that comprises an internal thread into which a cap (28) can be screwed, and means (22, 26) for fixing the member to the casing, characterised in that it further comprises a cover (30) mounted on the member and at least partially covering the fixing means in order to hinder, or indeed prevent, access to same when the cover is mounted on the member, the cover being arranged to allow free access to the duct when the cap is not screwed into the duct.