Aircraft cabin bin retrofit
Disclosed herein is an asymmetric luggage stowage bin arrangement, with a pair of compartments attached to a single bin housing. The compartments 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 bin divider;
iii. a first bin end-wall on one longitudinal of the bin housing substantially parallel to the bin divider defining a first luggage compartment,
iv. a second end-wall on the longitudinally opposite end of the bin housing from the first bin end-wall substantially parallel to the bin divider defining a second luggage compartment, and
v. 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.
2. The luggage storage system as recited in claim 1 wherein:
a. the longitudinal width of the first luggage compartment is between 35% to 45% of the width of the bin housing; and
b. the longitudinal width of the second luggage compartment 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 compartment is substantially 41% of the width of the bin housing; and
b. the longitudinal width of the second luggage compartment is substantially 69% of the width of the bin housing.
4. The luggage storage system as recited in claim 1 wherein:
a. the first luggage compartment comprises a first luggage compartment 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 compartment comprises a second luggage compartment 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.
5. An aircraft interior retrofit comprising the steps of:
a. removing an 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 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. a bin divider substantially parallel to each end-wall; and
v. 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;
d. defining a first luggage compartment extending from the first bin end-wall to the bin divider;
e. providing a second luggage compartment extending from the second bin end-wall to the bin divider; and
f. installing the retrofit bin housing in place of the existing bin housing.