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

Claim 9:
10. A method of use of a blended wing body aircraft with a fuel cell, the method comprising:
storing a first fuel, using at least a first fuel store located within a transitional portion of a blended wing body of the blended wing body aircraft, 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;
combining the first fuel with oxygen to produce electricity, using at least a fuel cell;
storing a second fuel, using at least a second fuel store located within the blended wing body, wherein the at least a second fuel store comprises a second environment mitigation configured to regulate the temperature 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;
powering, using the at least a fuel cell, an auxiliary power system operatively connected with the at least a fuel cell, wherein the auxiliary power system is configured to power an anti-ice system and a braking system while in flight; and
propelling the blended wing body aircraft, using at least a propulsor mechanically affixed to an upper aft surface the blended wing body aircraft, wherein the at least a propulsor is encapsulated by at least a nacelle.