公开(公告)号：USD1042301S1

公开(公告)日：2024-09-17

申请号：US29813763

申请日：2021-11-01

Applicant: JetZero, Inc.

Designer： Mark Allan Page ,  Blaine Knight Rawdon

Abstract: FIG. 1 is a perspective view of an aircraft showing the new design;
FIG. 2 is a front view thereof;
FIG. 3 is a rear view thereof;
FIG. 4 is a side view thereof;
FIG. 5 is a second side view thereof;
FIG. 6 is a top view thereof; and,
FIG. 7 is a bottom view thereof.
The broken lines in the figures show portions of the aircraft that form no part of the claimed design.

公开(公告)号：US20240294271A1

公开(公告)日：2024-09-05

申请号：US18518881

申请日：2023-11-24

Applicant: JETZERO, INC.

Inventor： Ronald Tatsuji Kawai ,  Shailesh Atreya

IPC: B64F1/28 ,  B64C39/10 ,  B64D37/08 ,  B64D37/30

CPC classification number: B64F1/28 ,  B64C39/10 ,  B64D37/08 ,  B64D37/30 ,  B64C2039/105

Abstract: In an aspect, an aircraft fueling apparatus is disclosed. The apparatus includes at least a container comprising a fuel tank configured to store liquified gas fuel. The apparatus may also include a translocation device configured to carry the at least a container. An orientation guidance track may also be included in the apparatus. The orientation guidance track may be configured to direct a movement of the translocation device to a first position.

公开(公告)号：US20240253780A1

公开(公告)日：2024-08-01

申请号：US18102301

申请日：2023-01-27

Applicant: JETZERO, INC.

Inventor： Mark Allan Page ,  John Vassberg

IPC: B64C39/00 ,  B64D9/00

CPC classification number: B64C39/00 ,  B64D9/00 ,  B64C2039/105 ,  B64D27/16

Abstract: an aircraft with high transport efficiency, wherein the aircraft include a blended wing body with a downward depressed upper aft surface, configured to operate at a high cruising level within a high cruise altitude range, wherein the blended wing body include a main body configured to accommodate a payload, and at least a wing, wherein the blended wing body include no striking demarcation between the main body and the at least a wing and at least a propulsor attached to the blended wing body and configured to propel the aircraft.

公开(公告)号：US20240190556A1

公开(公告)日：2024-06-13

申请号：US18407605

申请日：2024-01-09

Applicant: JetZero, Inc.

Inventor： Mark Allan Page ,  Blaine Knight Rawdon

IPC: B64C23/06 ,  B64C9/06 ,  B64C13/24 ,  B64C39/10

CPC classification number: B64C23/076 ,  B64C9/06 ,  B64C39/10 ,  B64C13/24 ,  B64C2039/105

Abstract: Aspects relate to aircraft and methods of use for aerodynamic control with winglet surfaces. In an aspect an exemplary aircraft includes a first wing having a first winglet at a distal end of the wing, wherein the first winglet comprises at least a first control surface at a first trailing edge of the first winglet and a second wing having a second winglet at a distal end of the wing, wherein the second winglet comprises at least a second control surface at a second trailing edge of the second winglet.

公开(公告)号：US20240132220A1

公开(公告)日：2024-04-25

申请号：US18397011

申请日：2023-12-27

Applicant: JetZero, Inc.

Inventor： Ronald Tatsuji Kawai ,  Shailesh Atreya

IPC: B64D27/10 ,  B64C39/10 ,  B64D37/06 ,  B64D41/00 ,  H01M8/04082

CPC classification number: B64D27/10 ,  B64C39/10 ,  B64D37/06 ,  B64D41/00 ,  H01M8/04201 ,  B64C2039/105 ,  B64D2041/005 ,  H01M2250/20

Abstract: A system for a blended wing body aircraft with a combustion engine is illustrated. The aircraft comprises a blended wing body, at least a fuel source located within the blended wing body and configured to store a fuel, wherein the fuel includes liquid hydrogen, and at least a propulsor configured to propel the blended wing body aircraft. The at least a propulsor comprises a combustion engine configured to burn the fuel from the fuel source and produce mechanical work to power the at least a propulsor.

公开(公告)号：US11945574B2

公开(公告)日：2024-04-02

申请号：US17895384

申请日：2022-08-25

Applicant: JETZERO, Inc.

Inventor： Mark A. Page

IPC: B64C25/04 ,  B64C39/10

CPC classification number: B64C25/04 ,  B64C39/10 ,  B64C2039/105

Abstract: Aspects related to aircraft for commercial air travel and methods of manufacture. An aircraft includes a blended wing body, a single deck located within the blended wing body, wherein the single deck additionally includes a passenger compartment located in a lateral middle portion of the blended wing body and at least a cargo store located laterally outside the passenger compartment, and a landing gear, wherein the landing gear includes at least a nose gear located substantially forward of the single deck and at least a main gear located substantially aft of the single deck, wherein one or more of the at least a nose gear and the at least a main gear occupies a gear housing that overlaps with a plane coincident with at least a portion of the single deck.

公开(公告)号：US20240051659A1

公开(公告)日：2024-02-15

申请号：US18373690

申请日：2023-09-27

Applicant: JETZERO, INC.

Inventor： Ewald Schuster ,  Jennifer Whitlock ,  Joshua B. Long ,  Cristina Donastorg ,  Brendan Kennelly ,  Mark A. Page

IPC: B64C25/14 ,  B64C25/22 ,  B64C25/26 ,  B64C25/40

CPC classification number: B64C25/14 ,  B64C25/22 ,  B64C25/26 ,  B64C25/40

Abstract: Systems and methods for mechanically rotating an aircraft about its center-of-gravity (CG) are disclosed. The system can enable the rear, or main, landing gear to squat, while the nose landing gear raises to generate a positive pitch angle for the aircraft for takeoff or landing. The system can also enable the nose gear and main gear to return to a relatively level fuselage attitude for ground operations. The system can include one or more hydraulically linked hydraulic cylinders to control the overall height of the nose gear and the main gear. Because the hydraulic cylinders are linked, a change on the length of the nose cylinder generates a proportional, and opposite, change in the length of the main cylinder, and vice-versa. A method and control system for monitoring and controlling the relative positions of the nose gear and main gear is also disclosed.

公开(公告)号：US20230348036A1

公开(公告)日：2023-11-02

申请号：US18214464

申请日：2023-06-26

Applicant: JETZERO, INC.

Inventor： Mark Allan Page

IPC: B64C1/06 ,  B64C39/10 ,  B64C9/00 ,  B64F5/10 ,  B64C39/00 ,  B64C7/02

CPC classification number: B64C1/069 ,  B64C39/10 ,  B64C9/00 ,  B64F5/10 ,  B64C39/00 ,  B64C7/02 ,  B64C2039/105 ,  B64C2211/00

Abstract: A system for modular aircraft includes at least a common component, wherein the at least a common component includes at least a flight component. The system includes at least a modular component, wherein the at least modular component includes at least a fuselage component and a collar component. The system includes at least an interface component, wherein the at least an interface component is configured to connect the at least a common component at a first end to the at least a modular component at a second end.

公开(公告)号：US12162602B2

公开(公告)日：2024-12-10

申请号：US18090173

申请日：2022-12-28

Applicant: JetZero, Inc.

Inventor： Blaine Knight Rawdon

IPC: B64C3/56 ,  B64C13/40 ,  B64C13/50 ,  B64C39/10

Abstract: Aspects relate to systems and methods for folding wings on an aircraft. An exemplary system includes a blended wing body, where the blended wing body includes a main body and at least a wing, a hinge located on the at least a wing and configured to allow folding of the at least a wing, an actuation system configured to fold the at least a wing, and a controller configured to control the at least an actuation system.

公开(公告)号：US20240391586A1

公开(公告)日：2024-11-28

申请号：US18201923

申请日：2023-05-25

Applicant: JETZERO, INC.

Inventor： John Charles Vassberg ,  Blaine Knight Rawdon

IPC: B64C39/10 ,  B64D27/20 ,  B64D37/04

Abstract: A commercial aircraft for long distance air travel, the commercial aircraft comprising, a blended wing body aircraft having a main body, a transition and wings with no clear demarcation between the wings and the main body along a leading edge of the commercial aircraft, a passenger cabin, the passenger cabin located within the main body and having a single aisle passenger capacity, at least a propulsor, the at least a propulsor attached to a portion of the main body and configured to propel the blended wing body aircraft through air, and a fuel storage having a fuel capacity, the fuel capacity configured for long range flight, wherein the commercial aircraft is configured for long-range flight.