Arrangement and method for installing a component in an...

Details Arrangement and method for installing a component in an... Arrangement and method for installing a component in an...

2011-08-09

2011-08-09

Eldred, J. Woodrow (Department: 3641)

Aeronautics and astronautics

Aircraft structure

Details

C244S00100R, C248S613000, C248S557000, C248S638000

Reexamination Certificate

active

07992821

ABSTRACT:
An arrangement (10) for installing a component (12) in an aircraft comprises a guide device (14) which is connectable to an aircraft structure or is formed integrally with the aircraft structure, as well as an elastically deformable damping element (16; 16a,16b,16c) which is adapted to enable the component (12) to be mounted in the guide device (14) in a self-supporting manner. A locking mechanism (26) is adapted to fasten the component (12) in a desired position in the guide device (14) in a releasable manner.

REFERENCES:
patent: 6260813 (2001-07-01), Whitcomb
patent: 7410127 (2008-08-01), Ahad
patent: 7703291 (2010-04-01), Bushnik et al.
patent: 2003/0209632 (2003-11-01), Hessling
patent: 2006/0086886 (2006-04-01), Humfeldt et al.
patent: 102004042080 (2006-03-01), None

Affiliated with

Also associated with

Rating

Arrangement and method for installing a component in an... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Arrangement and method for installing a component in an..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Arrangement and method for installing a component in an... will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-2630953