Passenger bays on a blended wing body aircraft

Inventors: Scott Savian (Los Angeles, CA); Ian Geoffrey Scoley (Huntington Beach, CA)

Assignee: JetZero, Inc.

B64D11/0606 B64D11/04 B64D11/0601

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Quick Facts

Patent No.: US 12698083
App. No.: 19/285,268
Granted: Aug 4, 2026
Kind: B2

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Abstract

A blended wing body (BWB) aircraft including a blended wing body having a main body and wings with no clear demarcation between the wings and the main body along leading edges of the BWB aircraft, a passenger cabin located within the main body and more than one passenger bays located within the passenger cabin, wherein a perimeter of at least one passenger bay is demarcated by at least a divider and wherein the at least one passenger bay is substantially parallel to at least one leading edge of the BWB aircraft.

Claims (31)

1 . A blended wing body (BWB) aircraft comprising:

a blended wing body having a main body and wings with no clear demarcation between the wings and the main body along leading edges of the BWB aircraft;

a passenger cabin located within the main body; and

a plurality of passenger bays located within the passenger cabin, wherein:

a first portion of the plurality of passenger bays is substantially parallel to a longitudinal axis of the BWB aircraft;

a second portion of the plurality of passenger bays is substantially parallel to at least a portion of the leading edges of the BWB aircraft, wherein the at least a portion of the leading edges is non-parallel to the longitudinal axis;

each passenger bay comprises a plurality of passenger seats; and

wherein the second portion of the plurality of passenger bays comprises a bay aisle that is non-orthogonal to the cross aisle, wherein the plurality of passenger seats of the second portion of the plurality of passenger bays are disposed along the bay aisle.

2 . The BWB aircraft of claim 1 , wherein the second portion of the plurality of passenger bays comprises one or more passenger columns disposed parallel to the at least a portion of the leading edges.

3 . The BWB aircraft of claim 1 , wherein a seat pitch of the plurality of passenger seats of the first portion of the plurality of passenger bays is different than a seat pitch of the plurality of passenger seats of the second portion.

4 . The BWB aircraft of claim 1 , wherein a row size of the plurality of passenger seats of the second portion of the plurality of passenger bays is different than a row size of the plurality of passenger seats of the second portion.

5 . The BWB aircraft of claim 1 , wherein at least a portion of the passenger cabin comprises an ascending seat layout, wherein a rear portion of the at least a portion of the passenger cabin is wider than a front portion of the at least a portion of the passenger cabin.

6 . The BWB aircraft of claim 1 , wherein the passenger cabin comprises at least one passenger row comprising more than 8 of the plurality of passenger seats.

7 . The BWB aircraft of claim 1 , wherein the second portion of the plurality of passenger bays is separated from the first portion of the plurality of passenger bays by a cross aisle.

8 . The BWB aircraft of claim 7 , wherein the cross aisle extends along a lateral axis of the BWB aircraft.

9 . The BWB aircraft of claim 7 , wherein the plurality of passenger bays comprise an access route connecting the plurality of passenger bays to the cross aisle.

10 . The BWB aircraft of claim 1 , wherein the second portion of the plurality of passenger bays comprises a divider that is non-parallel to a divider of the first portion of the plurality of passenger bays.

11 . The BWB aircraft of claim 10 , wherein the divider of the first portion of the plurality of passenger bays comprises a structural element, wherein the structural element is configured to contain a pressure vessel of the BWB aircraft, wherein the pressure vessel comprises at least a portion of the passenger cabin.

12 . The BWB aircraft of claim 10 , wherein the divider of the first portion of the plurality of passenger bays comprises a structural element extending from a floor surface of the passenger cabin toward a roof surface of the passenger cabin.

13 . A blended wing body (BWB) aircraft comprising:

a blended wing body having a main body and wings with no clear demarcation between the wings and the main body along leading edges of the BWB aircraft;

a passenger cabin located within the main body; and

a plurality of passenger bays located within the passenger cabin, wherein:

a first portion of the plurality of passenger bays is situated along a longitudinal axis of the BWB aircraft;

a second portion of the plurality of passenger bays is situated along at least a portion of the leading edges of the BWB aircraft, wherein the at least a portion of the leading edges is non-parallel to the longitudinal axis;

each passenger bay comprises a plurality of passenger seats; and

14 . The BWB aircraft of claim 13 , wherein the second portion of the plurality of passenger bays comprises one or more passenger columns disposed parallel to the at least a portion of the leading edges.

15 . The BWB aircraft of claim 13 , wherein at least a portion of the passenger cabin comprises an ascending seat layout, wherein a rear portion of the at least a portion of the passenger cabin is wider than a front portion of the at least a portion of the passenger cabin.

16 . The BWB aircraft of claim 13 , wherein the second portion of the plurality of passenger bays is separated from the first portion of the plurality of passenger bays by a cross aisle.

17 . The BWB aircraft of claim 16 , wherein the cross aisle extends along a lateral axis of the BWB aircraft.