Triangular galley on a blended wing body aircraft

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 a leading edge of the BWB aircraft;
• a passenger cabin located within the main body, wherein the passenger cabin comprises one or more structural elements extending vertically and configured to contain a pressure vessel;
• a galley located within the passenger cabin and situated laterally between a first passenger bay and a second passenger bay, wherein the galley comprises a border having a triangular shape, and wherein the border comprises:
• a first side disposed laterally within the BWB aircraft;
• a second side extending from a first end of the first side at a first angle;
• and
• a third side extending from a second end of the first side at a second angle, wherein the second side is arranged to converge with the third side, wherein the second end of the first side is opposite to the first end of the first side;
• and
• wherein the galley comprises an access route extending through located near at least one vertex of one or more vertices of the triangular shape and wherein the access route provides access to an interior of the galley.