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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
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.
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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.
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公开(公告)号：US11878798B2
公开(公告)日：2024-01-23
申请号：US17478724
申请日：2021-09-17
Applicant: JETZERO, INC.
Inventor： Shailesh Atreya , Ronald Tatsuji Kawai
CPC classification number: B64C39/10 , B64D27/24 , B64D37/04 , B64D37/30 , B64C2039/105 , B64D2041/005 , B64D2221/00
Abstract: Certain aspects relate to a blended wing body aircraft with a fuel cell and methods of use. An exemplary aircraft includes a blended wing body, at least a propulsor mechanically affixed to the aircraft and configured to propel the aircraft, at least a first fuel store configured to store a first fuel, and at least a fuel cell configured to combine the first fuel with oxygen to produce electricity.
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公开(公告)号：US11851210B2
公开(公告)日：2023-12-26
申请号：US17731685
申请日：2022-04-28
Applicant: JETZERO, INC.
Inventor： Ronald Tatsuji Kawai , Shailesh Atreya
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.
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Patent Agency Ranking
公开(公告)号：US20240239485A1
公开(公告)日：2024-07-18
申请号：US18538226
申请日：2023-12-13
Applicant: JETZERO, INC.
Inventor： Shailesh Atreya , Ronald Tatsuji Kawai
IPC: B64C39/10 , B64D27/10 , B64D27/33 , B64D27/355 , B64D41/00 , H01M8/04082
CPC classification number: B64C39/10 , B64D27/10 , B64D27/33 , B64D27/355 , B64D41/00 , H01M8/04201 , B64C2039/105 , B64D2041/005 , H01M2250/20
Abstract: Certain aspects relate to a blended wing body aircraft with a fuel cell and methods of use. An exemplary aircraft includes a blended wing body, at least a propulsor mechanically affixed to the aircraft and configured to propel the aircraft, at least a first fuel store configured to store a first fuel, and at least a fuel cell configured to combine the first fuel with oxygen to produce electricity.
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公开(公告)号：US11891178B2
公开(公告)日：2024-02-06
申请号：US17731622
申请日：2022-04-28
Applicant: JETZERO, INC.
Inventor： Ronald Tatsuji Kawai , Shailesh Atreya
CPC classification number: B64C39/10 , B64D15/00 , B64D37/30 , B64C2039/105 , B64D2041/005 , B64D2221/00
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.
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公开(公告)号：US20230348091A1
公开(公告)日：2023-11-02
申请号：US18200668
申请日：2023-05-23
Applicant: JETZERO, INC.
Inventor： Ronald Tatsuji Kawai , Blaine Knight Rawdon
CPC classification number: B64D37/30 , B64C39/10 , B64C2039/105
Abstract: An aircraft with a multi-walled fuel tank and method of manufacturing is presented. The aircraft includes a blended wing body and a fuel tank attached to the blended wing body configured to store liquified gas fuel. The fuel tank includes an inner wall, outer wall, and interstitial volume in between that is filled with insulation. The interstitial volume includes a reflective film layer and a structural insulation layer.
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公开(公告)号：US20250066032A1
公开(公告)日：2025-02-27
申请号：US18941638
申请日：2024-11-08
Applicant: JetZero, Inc.
Inventor： Blaine Knight Rawdon , Ronald Tatsuji Kawai , Thomas James O'Leary , Terrence Kevin O'Leary, JR.
Abstract: A system and method for a blended wing body aircraft with permanent tanks is presented. The aircraft comprises a blended wing body and at least a tank permanently attached the blended wing body. The at least a tank is configured to store liquified gas fuel and further comprises at least a vent configured to vent gaseous fuel from the at least a tank and an insulation to reduce thermal transfer to the liquified gas fuel inside of the at least a tank.
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公开(公告)号：US12168521B2
公开(公告)日：2024-12-17
申请号：US17731655
申请日：2022-04-28
Applicant: JetZero, Inc.
Inventor： Blaine Knight Rawdon , Ronald Tatsuji Kawai , Thomas James O'Leary , Terrence Kevin O'Leary, Jr.
Abstract: A system and method for a blended wing body aircraft with permanent tanks is presented. The aircraft comprises a blended wing body and at least a tank permanently attached the blended wing body. The at least a tank is configured to store liquified gas fuel and further comprises at least a vent configured to vent gaseous fuel from the at least a tank and an insulation to reduce thermal transfer to the liquified gas fuel inside of the at least a tank.
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