公开(公告)号：US20220074369A1

公开(公告)日：2022-03-10

申请号：US17014884

申请日：2020-09-08

申请人： Hypersonix IP Holdings, Inc.

发明人： Michael Kevin Smart

IPC分类号： F02K7/12

摘要： Airframe integrated scramjet engines are disclosed. Scramjet engines within the scope of this disclosure may be configured to integrate smoothly with an airframe of a hypersonic flight aircraft or vehicle. The scramjet engine may include capture shape of an inlet configured to capture airflow, a combustor configured for combustion of fuel and air, and an exit shape of a nozzle configured for expansion of the combusted fuel and air to provide hypersonic thrust. In some embodiments, the scramjet engine has a fixed geometry and a transitioning cross-sectional shape over its full length. The scramjet engine is configured to be a component of launch vehicle system.

公开(公告)号：US11639700B2

公开(公告)日：2023-05-02

申请号：US17014884

申请日：2020-09-08

申请人： Hypersonix IP Holdings, Inc.

发明人： Michael Kevin Smart

IPC分类号： F02K7/10 ,  F02C7/04 ,  F02C7/228 ,  B64D33/02

摘要： Airframe integrated scramjet engines are disclosed. Scramjet engines within the scope of this disclosure may be configured to integrate smoothly with an airframe of a hypersonic flight aircraft or vehicle. The scramjet engine may include capture shape of an inlet configured to capture airflow, a combustor configured for combustion of fuel and air, and an exit shape of a nozzle configured for expansion of the combusted fuel and air to provide hypersonic thrust. In some embodiments, the scramjet engine has a fixed geometry and a transitioning cross-sectional shape over its full length. The scramjet engine is configured to be a component of launch vehicle system.