Suspension assembly for an aircraft turbojet engine

Details Suspension assembly for an aircraft turbojet engine Suspension assembly for an aircraft turbojet engine

B - Operations, Transporting

64

D

B64D 27/26 (2006.01)

Patent

CA 2751112

The invention relates to a suspension assembly for an aircraft turbojet engine (3), including a pylon (1) and connecting rods (13a, 13b) for taking up the thrust of the turbojet engine (3) and connected to the pylon (1), remarkable in that the assembly includes means (19a, 19b; 25) separate from said pylon for thermally insulating the connecting rods (13a, 13b) from the turbojet engine (3).

Cet ensemble de suspension pour turboréacteur (3) d'aéronef, comprenant un mât (1) et des bielles (13a, 13b) de reprise de la poussée dudit turboréacteur (3) reliées audit mât (1), est remarquable en ce qu'il comprend des moyens (19a, 19b; 25), distincts dudit mât (1), pour isoler thermiquement lesdites bielles (13a, 13b) par rapport audit turboréacteur (3).

Affiliated with

Also associated with

Rating

Suspension assembly for an aircraft turbojet engine does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Suspension assembly for an aircraft turbojet engine, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Suspension assembly for an aircraft turbojet engine will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1513583