Bellows with rotational joints

Details Bellows with rotational joints Bellows with rotational joints

F - Mech Eng,Light,Heat,Weapons

16

L

285/27

F16L 21/00 (2006.01) F16L 27/111 (2006.01)

Patent

CA 1075280

BELLOWS WITH ROTATIONAL JOINTS Abstract of Disclosure A heat suppressor for a gas turbine engine is mounted on an aircraft by means separate from the engine mounts. A sleeve apparatus is needed to connect the exhaust duct of the engine to the suppressor duct for continuous flow of turbine gases. The sleeve apparatus is in the form of a bellows to absorb bending forces created by flexing of the air frame. This in- vention provides a unique connecting assembly to connect the bellows to the engine. The assembly consists of an annular socket fixed to the bellows and constructed to receive a radially extending flange on a connecting shroud fixed to the engine. The flange and socket are slidably engaged to allow twisting movement between the bellows and the engine, while the bellows allows relative displacement of the axes of the connecting passages.

302650

Affiliated with

Also associated with

Rating

Bellows with rotational joints does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Bellows with rotational joints, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Bellows with rotational joints will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-498732