Turbojet engine mount

Details Turbojet engine mount Turbojet engine mount

B - Operations, Transporting

64

D

B64D 27/00 (2006.01) B64D 27/26 (2006.01)

Patent

CA 2410908

A jet engine suspension comprises a master component (17) for attachment, fixed to an aircraft pylon (29). If it breaks and if the situation arises where the fixing screws are no longer able to transmit force, a peg (26) takes over: the master component (17) collapses until an upper shoulder (35) rests on the pylon (29) and supports this component. The peg (26) is free of dynamic stress in normal service and there is absolutely no risk of it cracking in fatigue.

Une suspension de réacteur comprend une pièce maîtresse (17) d'accrochage fixée à un mât (29) d' aéronef. Si elle se rompt et que des vis de fixation en viennent à ne plus transmettre les efforts, un pion (26) le relaye: la pièce maîtresse (17) s'affaisse jusqu'à ce qu'on épaulement supérieur (35) se pose sur le mât (29) et soutienne celle-là . Le pion (26) est exempt de sollicitations dynamiques en service normal et ne risque point de se fissurer en fatigue.

Affiliated with

Also associated with

Rating

Turbojet engine mount does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1678472