AIRCRAFT EQUIPMENT SUPPORT

• US 20110133030A1
• Filed: 02/17/2011
• Published: 06/09/2011
• Est. Priority Date: 03/27/2007
• Status: Active Grant

• Current Assignee: AMI Industries, Inc. (Rtx Corporation)
• Original Assignee: AMI Industries, Inc. (Rtx Corporation)
• Inventors: KENNEDY, Othar P., Ferguson, Keith Michael, Porter, Ryan Stuart
• Granted Patent: US 8,292,221 B2
• Time in Patent Office: Days
• US Class Current: 244/118.5
• CPC Class Codes: B64D 11/06 Arrangements of seats, or adaptations or details specially adapted for aircraft seats crew seat constructions for emergency purposes B64D25/04
• CPC Class Codes: B64D 11/0649 Seats characterised by special features for reducing weight
• CPC Class Codes: B64D 11/0696 Means for fastening seats to floors, e.g. to floor rails
• CPC Class Codes: Y02T 50/40 Weight reduction

Abstract

A support for an aircraft seat, table or other piece of equipment has a lower support link that sweeps out a lateral arc. The lower support link cooperates with a conventional linear track to support the piece of equipment. The linear track provides fore/aft movement substantially orthogonal to a line tangent to the center of the lateral arc. A pilot link is operatively attached to the piece of equipment to form a four-bar linkage that maintains the equipment in a predetermined rotational attitude as the lower support link sweeps out its lateral arc.

Claims

1. An equipment support for securing aircraft interior equipment to an airframe comprising:

a base adapted to be attached to the airframe, said base having an upper portion and a lower portion;

a lower support link rotationally attached to the upper portion of said base, said lower support link having a fixed end and a free end, said fixed end of said lower support link comprising a first rotating joint defining a first axis of rotation about said base, said first axis of rotation being oriented substantially vertically relative to said airframe, said free end of said lower link having a second rotating joint thereon defining a second axis of rotation parallel to and offset from said first axis of rotation, said lower support link having a longitudinal axis passing through said first and second axes of rotation;

a pilot link, said pilot link having a fixed end and a free end, said fixed end of said pilot link comprising a third rotating joint defining a third axis of rotation relative to said base, said third axis of rotation being parallel to and offset from said first axis of rotation, said free end of said pilot link having a fourth rotating joint thereon defining a fourth axis of rotation, said pilot link having a second longitudinal axis passing through said third and fourth axes of rotation;

an equipment platform, said equipment platform rotationally attached to said lower support link at said second rotating joint and to said pilot link at said fourth rotating joint to form a four bar linkage for defining a rotational attitude of said equipment platform as said lower support link rotates about said first axis of rotation;

a linear track attached to said equipment platform; and

an aircraft interior equipment member attached to said linear track.

2. The equipment support of claim 1, wherein:

said lower support link and said pilot link cooperate to form a parallelogram linkage, whereby said equipment platform is maintained in a rotationally fixed attitude as said lower support link rotates about said first axis of rotation.

3. An equipment support for securing aircraft interior equipment to an airframe comprising:

a linear track attached to the airframe;

base slidingly engaging said linear track, whereby said base is moveable linearly with respect to said airframe, said base having an upper portion and a lower portion;

a lower support link rotationally attached to the upper portion of said base, said lower support link having a fixed end and a free end, said fixed end of said lower support link comprising a first rotating joint defining a first axis of rotation about said base, said first axis of rotation being oriented substantially vertically relative to said airframe, said free end of said lower link having a second rotating joint thereon defining a second axis of rotation parallel to and offset from said first axis of rotation, said lower support link having a longitudinal axis passing through said first and second axes of rotation;

a pilot link, said pilot link having a fixed end and a free end, said fixed end of said pilot link comprising a third rotating joint defining a third axis of rotation relative to said base, said third axis of rotation being parallel to and offset from said first axis of rotation, said free end of said pilot link having a fourth rotating joint thereon defining a fourth axis of rotation, said pilot link having a second longitudinal axis passing through said third and fourth axes of rotation; and

an equipment platform operatively attached to said lower support link at said second rotating joint and to said pilot link at said fourth rotating joint to form a four bar linkage for defining a rotational attitude of said equipment platform as said lower support link rotates about said first axis of rotation.

4. The equipment support of claim 3, wherein:

said lower support link and said pilot link cooperate to form a parallelogram linkage, whereby said equipment platform is maintained in a rotationally fixed attitude as said lower support link rotates about said first axis of rotation.

5. The equipment support of claim 3, further comprising:

a first rotation lock coupled to said lower support link, said first rotation lock being moveable from a disengaged position to an engaged position for engaging said base to prevent rotation of said lower support link about said base.

6. The equipment support of claim 3, wherein:

said pilot link is of substantially lighter construction than said lower support link.

7. The equipment support of claim 3, further comprising:

a bearing support member operatively disposed between said lower support link and said equipment platform, said bearing support member comprising a thrust bearing for enabling said equipment platform to rotate about a vertical axis independent of said lower support link.