Invention Application
- Patent Title: EMBEDDED ENGINES IN HYBRID BLENDED WING BODY
- Patent Title (中): 嵌入式混合发动机混合机身
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Application No.: US14203735Application Date: 2014-03-11
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Publication No.: US20160122005A1Publication Date: 2016-05-05
- Inventor: Razvan Virgil Florea , William T. Cousins , Thomas G. Tillman , David J. Arend , John D. Wolter
- Applicant: UNITED TECHNOLOGIES CORPORATION
- Applicant Address: US CT Hartford
- Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Hartford
- Main IPC: B64C21/04
- IPC: B64C21/04 ; B64C1/16 ; B64D29/04 ; B64C39/10
Abstract:
A hybrid wing aircraft has an engine embedded into a body of the hybrid wing aircraft. The embedded engine has a fan that is received within a nacelle. The body of the aircraft provides a boundary layer over a circumferential portion of a fan. A system delivers additional air to correct fan stability issues raised by the boundary layer.
Information query
