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公开(公告)号:US11668243B2
公开(公告)日:2023-06-06
申请号:US17329501
申请日:2021-05-25
Applicant: Raytheon Technologies Corporation
Inventor: Marc J. Muldoon , Carroll V. Sidwell
IPC: F02C7/224 , F02C3/22 , F02C7/232 , F02C7/26 , F02C9/40 , B64D37/14 , B64D37/30 , F02C7/262 , F02C7/32 , B64D37/04 , B64D37/10 , B64D37/16 , B64D37/34 , B64D37/06 , B64F1/28
CPC classification number: F02C7/224 , F02C3/22 , F02C7/232 , F02C7/26 , F02C7/262 , F02C7/32 , F02C9/40 , B64D37/04 , B64D37/06 , B64D37/10 , B64D37/14 , B64D37/16 , B64D37/30 , B64D37/34 , B64F1/28 , F05D2220/323 , F05D2240/36
Abstract: Aircraft hydrogen fuel systems and methods and systems of starting such systems are described. The aircraft hydrogen fuel systems include a hydrogen burning main engine, a main tank configured to contain liquid hydrogen to be supplied to the main engine during a normal operation, and a starter tank configured to contain gaseous hydrogen to be used during a startup operation of the main engine. Methods and processes for starting and/or restarting such systems are described.
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公开(公告)号:US20220381185A1
公开(公告)日:2022-12-01
申请号:US17329501
申请日:2021-05-25
Applicant: Raytheon Technologies Corporation
Inventor: Marc J. Muldoon , Carroll V. Sidwell
Abstract: Aircraft hydrogen fuel systems and methods and systems of starting such systems are described. The aircraft hydrogen fuel systems include a hydrogen burning main engine, a main tank configured to contain liquid hydrogen to be supplied to the main engine during a normal operation, and a starter tank configured to contain gaseous hydrogen to be used during a startup operation of the main engine. Methods and processes for starting and/or restarting such systems are described.
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公开(公告)号:US20240052782A1
公开(公告)日:2024-02-15
申请号:US18144576
申请日:2023-05-08
Applicant: Raytheon Technologies Corporation
Inventor: Marc J. Muldoon , Carroll V. Sidwell
CPC classification number: F02C7/224 , F02C3/22 , F02C7/232 , F02C7/26 , F02C7/262 , F02C7/32 , F02C9/40 , B64F1/28
Abstract: Aircraft hydrogen fuel systems and methods and systems of starting such systems are described. The aircraft hydrogen fuel systems include a hydrogen burning main engine, a main tank configured to contain liquid hydrogen to be supplied to the main engine during a normal operation, and a starter tank configured to contain gaseous hydrogen to be used during a startup operation of the main engine. Methods and processes for starting and/or restarting such systems are described.
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