Aircraft cabin bin retrofit
Disclosed herein is an asymmetric luggage stowage bin arrangement, with a pair of buckets attached to a single bin housing. The buckets being unequal in length, to optimize the storage capacity of the bin housing relative to the most common luggage dimensions on the market. In one form, the asymmetric luggage stowage bin arrangement is used as a retrofit to replace shelf-style luggage stowage compartments common to older style aircraft.
1. A luggage storage system for commercial aircraft, the system comprising:
a. a bin housing comprising:
i. an aircraft frame attachment device,
ii. a first bin end-wall on one longitudinal end of the bin housing,
iii. a second end-wall on the longitudinally opposite end of the bin housing from the first bin end-wall,
iv. a end-wall pivot on facing sides of the first and the second end-wall,
v. a bin divider substantially parallel to each end-wall,
vi. wherein the distance between the first bin end-wall and the bin divider is substantially less than the distance between the second bin end-wall and the bin divider,
vii. a divider pivot on both longitudinal sides of the bin divider;
b. a first luggage bucket extending from the first bin end-wall to the bin divider the first luggage bucket attached to corresponding end-wall pivot and corresponding divider pivot; and
c. a second luggage bucket extending from the second bin end-wall to the bin divider, the second luggage bucket attached to corresponding end-wall pivot and corresponding divider pivot.
2. The luggage storage system as recited in claim 1 wherein:
a. the longitudinal width of the first luggage bucket is between 35% to 45% of the width of the bin housing; and
b. the longitudinal width of the second luggage bucket is between 55% to 65% of the width of the bin housing.
3. The luggage storage system as recited in claim 2 wherein:
a. the longitudinal width of the first luggage bucket is substantially 41% of the width of the bin housing; and
b. the longitudinal width of the second luggage bucket is substantially 59% of the width of the bin housing.
4. The luggage storage system as recited in claim 1 wherein:
a. the first luggage bucket comprises a first luggage bucket face which longitudinally overlies the first bin end-wall and a portion of the bin divider less than half the longitudinal thickness of the bin divider; and
b. the second luggage bucket comprises a second luggage bucket face which longitudinally overlies the second bin end-wall and a portion of the bin divider less than half the longitudinal thickness of the bin divider.
5. An aircraft luggage bin retrofit of an existing bin housing produced by the process comprising the steps of:
a. removing the existing bin housing from the aircraft;
b. providing a retrofit bin housing having substantially the same longitudinal dimension as the existing bin housing;
c. the retrofit bin housing comprising:
i. an aircraft frame attachment device,
ii. a first bin end-wall on one longitudinal end of the retrofit bin housing,
iii. a second end-wall on the longitudinally opposite end of the retrofit bin housing from the first bin end-wall,
iv. an end-wall pivot on facing sides of the first and the second end-wall,
v. a bin divider substantially parallel to each end-wall,
vi. wherein the distance between the first bin end-wall and the bin divider is substantially less than the distance between the second bin end-wall and the bin divider,
vii. a divider pivot on both longitudinal sides of the bin divider;
d. providing a first luggage bucket extending from the first bin end-wall to the bin divider the first luggage bucket attached to corresponding end-wall pivot and corresponding divider pivot;
e. providing a second luggage bucket extending from the second bin end-wall to the bin divider, the second luggage bucket attached to corresponding end-wall pivot and corresponding divider pivot; and
f. installing the retrofit bin housing in place of the existing bin housing.