SUPPORT RACK FOR AT LEAST ONE ITEM OF AIRCRAFT ELECTRONICS, CORRESPONDING SUPPORT DEVICE AND AIRCRAFT
First Claim
1. A support rack for at least one item of aircraft electronics, wherein the support rack comprises:
- a rectangular frame formed by four essentially straight segments and having an essentially planar upper surface; and
four feet each having an essentially planar upper surface which is in the essentially planar upper surface of the rectangular frame, wherein each of said feet are joined to a corner of said frame, and each of said feet extend in a direction forming an angle between 90° and
180°
with a lengthwise direction of each the segments of said frame forming the corner of the frame;
a first set of holes configured to attach at least one item of electronic equipment to the rectangular frame, wherein the first set of holes are in the essentially planar upper surfaces of said rectangular frame or of said feet, andat least one second set of attachment holes configured to anchor the rectangular frame to the structure of the aircraft, wherein the at least one second set of attachment holes are in a surface of the support rack out of the essentially planar upper surface.
2 Assignments
0 Petitions
Accused Products
Abstract
A support rack configured for an aircraft including: a rectangular frame including four substantially straight segments and four feet, wherein upper surfaces of each of the substantially straight segments and the four feet are substantially aligned with a upper plane of the rectangular frame; a first set of attachment holes configured to attach at least one item of aviation electronic equipment, wherein the first set of holes are in the upper surfaces of the straight segments or the, and a second set of attachment holes configured to receive anchoring elements that anchor to a structure of the aircraft, wherein the second set of attachment holes are at a surface of the rack out of the substantially upper planar.
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Citations
15 Claims
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1. A support rack for at least one item of aircraft electronics, wherein the support rack comprises:
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a rectangular frame formed by four essentially straight segments and having an essentially planar upper surface; and
four feet each having an essentially planar upper surface which is in the essentially planar upper surface of the rectangular frame, wherein each of said feet are joined to a corner of said frame, and each of said feet extend in a direction forming an angle between 90° and
180°
with a lengthwise direction of each the segments of said frame forming the corner of the frame;a first set of holes configured to attach at least one item of electronic equipment to the rectangular frame, wherein the first set of holes are in the essentially planar upper surfaces of said rectangular frame or of said feet, and at least one second set of attachment holes configured to anchor the rectangular frame to the structure of the aircraft, wherein the at least one second set of attachment holes are in a surface of the support rack out of the essentially planar upper surface. - View Dependent Claims (2, 3, 4)
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5. A device for supporting at least one item of aircraft electronics comprising:
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a support rack including; a first rectangular frame formed by four essentially straight segments and having an essentially planar upper surface; and
four feet each having an essentially planar upper surface which is in the essentially planar upper surface of the first rectangular frame, wherein each of said feet are joined to a corner of said frame, and each of said feet extend in a direction forming an angle between 90° and
180°
with a lengthwise direction of each the segments of said frame forming the corner of the frame;a first set of holes configured to attach at least one item of electronic equipment to the first rectangular frame, wherein the first set of holes are in the essentially planar upper surfaces of said first rectangular frame or of said feet, and at least one second set of attachment holes configured to anchor the first rectangular frame to the structure of the aircraft, wherein the at least one second set of attachment holes are in a surface of the support rack out of the essentially planar upper surface, and an anchoring element configured to anchor to the structure of the aircraft, wherein said anchoring element is attached to said support rack by attachment devices extending said second set of holes of the first support rack. - View Dependent Claims (6, 7, 8)
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9. A support rack configured for an aircraft, the support rack comprising:
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a rectangular frame including four substantially straight segments and four feet, wherein upper surfaces of each of the substantially straight segments and the four feet are substantially aligned with a upper plane of the rectangular frame, and wherein each of the feet are at a corner of the rectangular frame and the foot at each of the corners extends at a direction forming an angle between ninety and one-hundred eighty degrees with respect to each of the lengthwise directions of the straight segments ending at the corner; a first set of attachment holes configured to attach at least one item of aviation electronic equipment, wherein the first set of holes are in the upper surfaces of the straight segments or the, and a second set of attachment holes configured to receive anchoring elements that anchor to a structure of the aircraft, wherein the second set of attachment holes are at a surface of the rack out of the substantially upper planar. - View Dependent Claims (10, 11)
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12. A electronics equipment support device configured for an aircraft and comprising:
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a support rack including; frames each having upper surfaces in a horizontal plane corresponding to the frame, wherein the upper surfaces are configured to support electronics equipment, and each frame include a first pair of arm segments, a second pair of arm segments orthogonal to the first pair, and four feet each at junction between the first and second pairs of arm segments, a first set of attachment holes configured to attach at least one item of aviation electronic equipment, wherein the first set of holes are in the upper surfaces of each of the frames, and a second set of attachment holes in each of the frames and configured to receive anchoring elements to anchor the frame to a structure of the aircraft, wherein the second set of attachment holes are at a surface of the frame out horizontal plane for the frame; and an anchoring element configured to anchor to the structure of the aircraft, wherein said anchoring element extend through at least one of the second set of holes. - View Dependent Claims (13, 14, 15)
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Specification