Patent ID: 11897601
Assignee: JETZERO, INC.
Field: Transport (Mechanical engineering)
Classification: CPC B  Y | IPC B

Claim 0:
1. An aircraft for transonic flight comprising:
a fuselage extending to a back portion lacking a vertical tailfin, wherein the back portion comprises a first main body control surface and a second main body control surface;
a propulsor configured to generate thrust;
a first substantially swept wing having a first winglet disposed beyond the back portion of the fuselage, the first winglet comprising a carbon-fiber composite with carbon fibers between 5-10 micrometers at a distal end of the wing, wherein the first winglet comprises at least a first control surface including a first trailing edge of the first winglet, wherein the fuselage and a leading edge of the first substantially swept wing creates a continuous curvilinear geometry;
a second substantially swept wing having a second winglet disposed beyond the back portion of the fuselage, the second winglet comprising a carbon-fiber composite with carbon fibers between 5-10 micrometers at a distal end of the wing, wherein the second winglet comprises at least a second control surface including a second trailing edge of the second winglet, wherein the fuselage and a leading edge of the second substantially swept wing creates a continuous curvilinear geometry;
wherein the at least a first control surface and the at least a second control surface are independently movable and the at least a first control surface and the at least a second control surface each comprise at least two control surface segments, wherein each of the at least two control surface segments are independently positioned;
a first actuator configured to move the at least first control surface; and
a second actuator configured to move the at least second control surface, wherein an actuator of the first actuator and second actuator comprises a pneumatic actuator.