Link component for aircraft engine mounting systems

Details Link component for aircraft engine mounting systems Link component for aircraft engine mounting systems

B - Operations, Transporting

64

D

B64D 27/26 (2006.01) B64D 27/18 (2006.01)

Patent

CA 2351281

A link (24) for use in an aircraft engine mounting system includes a span section (38) having a first connector (40) formed at one end thereof and a second connector (40) formed at another end thereof. A lumped mass (46,146) is disposed on the span section (38) for placing the resonant frequency of the link (24) away from engine excitation frequencies.

Affiliated with

Also associated with

Rating

Link component for aircraft engine mounting systems does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1702917