US5395074A — Retrofit bezel assembly

Claim 1

Independent Claim 116 words

An apparatus to replace at least a portion of an interior bezel assembly of an aircraft having stowage bins with shelves, comprising: (a) a first support member for attachment to a bin shelf; (b) a first bin shelf extension attached to the first support member, the first support member extending upwardly from the first bin shelf extension, the first bin shelf extension having a top surface oriented generally horizontally and adapted to abut and extend inwardly front the end of the existing bin shelf; and (c) attachment means for securing the first bin shelf extension to the inward end of the existing bin shelf such that the first bin shelf extension extends the usable shelf width.

Claim 2

Independent Claim 116 words

An apparatus to replace at least a portion of an interior bezel assembly of an aircraft having stowage bins with shelves, comprising: (a) a first support member for attachment to a bin shelf; (b) a first bin shelf extension attached to the first support member, the first support member extending upwardly from the first bin shelf extension, the first bin shelf extension having a top surface oriented generally horizontally and adapted to abut and extend inwardly front the end of the existing bin shelf; and (c) attachment means for securing the first bin shelf extension to the inward end of the existing bin shelf such that the first bin shelf extension extends the usable shelf width.

Claim 3

Dependent Claim 71 words

The apparatus of claim 1, wherein the aircraft has right-side stowage bins and left-side stowage bins, the apparatus further comprising a second support member for attachment to a bin shelf and a ceiling panel attached to an upper end of the first support member and an upper end of the second support member, said ceiling panel adapted for spanning the area between a right-side stowage bin and a left-side stowage bin.

Claim 4

Dependent Claim 92 words

The apparatus of claim 2, further comprising a second bin shelf extension and wherein the first and second support members comprise first and second bulkhead extensions, the first bulkhead extension being attached to the first bin shelf extension and the second bulkhead extension being attached to the second bin shelf extension, the bulkhead extensions having upper ends attached to the ceiling panel, and wherein the attachment means includes means for securing the first bin shelf extension to the right-side bin shelf and the second bin shelf extension to the left-side bin shelf.

Claim 5

Dependent Claim 84 words

The apparatus of claim 3, wherein the stowage bins include side walls, the apparatus further comprising a plurality of bin doors, each door being attached to at least one of said bulkhead extensions, wherein at least one of said bulkhead extensions is coupled to a bin shelf adjacent to one of the side walls of the stowage bins, said at least one bulkhead extension having a shape substantially matching the shape of the space between the stowage bin side wall and the bin door.

Claim 6

Dependent Claim 37 words

The apparatus of claim 1, further comprising a bin door attached to the first support member, said door constructed and arranged to close with its bottom end disposed near an inner edge of the bin shelf extension.

Claim 7

Dependent Claim 15 words

The apparatus of claim 1, further comprising a handrail attached to the bin shelf extension.

Claim 8

Dependent Claim 66 words

The apparatus of claim 1, wherein the stowage bin shelves include bullnose holes, wherein the attachment means include attachment holes in the first support member and first bin shelf extension that are adapted to match the preexisting bullnose holes in the bin shelves, such that the entire bezel assembly can be secured in place by fastening the assembly to the aircraft at the preexisting bullnose holes.

Claim 9

Independent Claim 134 words

A method of updating an aircraft interior with interior replacement bezel assembly units, the aircraft interior including bins and bin shelves and an old bezel assembly having an old ceiling panel, an old bullnose assembly, and an old door, each replacement unit including a ceiling panel, bulkhead extensions, bin doors, and shelf extensions, comprising the steps of: (a) removing the old bezel assembly including the old ceiling panel, the old stowage bin doors, and the old bullnose assembly, leaving old bins and bin shelves in place; (b) positioning an entire replacement bezel assembly unit in place within the aircraft in place of the old bezel assembly; (c) fastening the unit in place; and (d) attaching said shelf extension to the inside end of the bin shelves to extend the width of the bin shelves.

Claim 10

Independent Claim 134 words

A method of updating an aircraft interior with interior replacement bezel assembly units, the aircraft interior including bins and bin shelves and an old bezel assembly having an old ceiling panel, an old bullnose assembly, and an old door, each replacement unit including a ceiling panel, bulkhead extensions, bin doors, and shelf extensions, comprising the steps of: (a) removing the old bezel assembly including the old ceiling panel, the old stowage bin doors, and the old bullnose assembly, leaving old bins and bin shelves in place; (b) positioning an entire replacement bezel assembly unit in place within the aircraft in place of the old bezel assembly; (c) fastening the unit in place; and (d) attaching said shelf extension to the inside end of the bin shelves to extend the width of the bin shelves.

Claim 11

Dependent Claim 31 words

The method of claim 8, wherein the step of positioning is carried out such that pre-existing bullnose holes in the bin shelves are aligned with attachment locations on the replacement unit.

Claim 12

Dependent Claim 19 words

The method of claim 8, wherein the unit is completely pre-assembled before positioning and fastening it within the aircraft.

Claim 13

Dependent Claim 138 words

A preassembled retrofit bezel assembly to be installed within an interior of an aircraft having stowage bins with shelves, the assembly comprising: (a) a ceiling panel to substantially span and cover the upper surface of the interior of the airplane from a right-side stowage bin to a left-side stowage bin; (b) a plurality of bulkhead extensions attached to the sides of the ceiling panel to extend downwardly along portions of the front of the stowage bins and to be attached to inside ends of the bin shelves; and (c) a plurality of shelf extensions each attached to at least one bulkhead extension, the shelf extensions including means for attachment to the inside ends of the bin shelves to extend the width of the bin shelves, the shelf extensions having upper surfaces oriented generally transverse to the bulkhead extensions.

Claim 14

Dependent Claim 138 words

A preassembled retrofit bezel assembly to be installed within an interior of an aircraft having stowage bins with shelves, the assembly comprising: (a) a ceiling panel to substantially span and cover the upper surface of the interior of the airplane from a right-side stowage bin to a left-side stowage bin; (b) a plurality of bulkhead extensions attached to the sides of the ceiling panel to extend downwardly along portions of the front of the stowage bins and to be attached to inside ends of the bin shelves; and (c) a plurality of shelf extensions each attached to at least one bulkhead extension, the shelf extensions including means for attachment to the inside ends of the bin shelves to extend the width of the bin shelves, the shelf extensions having upper surfaces oriented generally transverse to the bulkhead extensions.

Annuity Stage	Window Opens	Payment Deadline	Surcharge Period Until	Estimated Fee	Status
3.5 Years (Year 4)	1998-03-06	1998-09-05	1999-03-07	$2000.00	Window Closed / Lapsed
7.5 Years (Year 8)	2002-03-06	2002-09-05	2003-03-07	$3760.00	Window Closed / Lapsed
11.5 Years (Year 12)	2006-03-06	2006-09-05	2007-03-07	$7700.00	Window Closed / Lapsed

Retrofit bezel assembly

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