Patent ID: 11878798
Assignee: JETZERO, INC.
Field: Transport (Mechanical engineering)
Classification: CPC B  Y | IPC B

Claim 0:
1. A blended wing body aircraft with a fuel cell, the aircraft comprising:
a blended wing body aircraft;
at least a first fuel store located within a transitional portion of the blended wing body aircraft and configured to store a first fuel, wherein the at least a first fuel store comprises a fuel environment mitigation configured to regulate the temperature and pressure of the first fuel, wherein the fuel environment mitigation comprises an insulation, wherein the insulation comprises a vacuum chamber disposed between an inner wall of the at least a first fuel store and an outer wall of the at least a first fuel store, and a pressure vessel wherein the pressure vessel is further configured to control fuel pressure;
at least a fuel cell configured to combine the first fuel with oxygen to produce electricity;
at least a second fuel store located within the blended wing body aircraft and configured to store a second fuel wherein the at least a second fuel store comprises a second environment mitigation configured to regulate the temperature and pressure of the second fuel, wherein the second fuel environment mitigation comprises a second insulation, wherein the second insulation comprises a second vacuum chamber disposed between an inner wall of the at least a second fuel store and an outer wall of the at least a second fuel store, and a second pressure vessel wherein the second pressure vessel is further configured to control a second fuel pressure;
an auxiliary power system operatively connected with the at least a fuel cell, wherein the at least a fuel cell is configured to power the auxiliary power system, wherein the auxiliary power system is configured to power an anti-ice system and a braking system while in flight;
at least a propulsor mechanically affixed to an upper aft surface of the blended wing body aircraft and configured to propel the blended wing body aircraft; and
at least a nacelle configured to encapsulate the at least a propulsor.