|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-021/06 B64C-003/20 B64F-005/00 F15D-001/00|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 27|
Systems and methods for secondary suctioning for an aerodynamic body are presented. A primary surface is configured along a leading edge of an aerodynamic body, and at least one secondary suction device comprising an elongated shape is configured at least a first distance from the primary surface. A non-suction surface is configured between the primary surface and the at least one secondary suction device.
1. An apparatus for extending laminar flow over an aerodynamic surface having a primary laminar flow region, comprising: a surface skin facesheet comprising a perforated region, the perforated region comprising a plurality of perforations configured to allow a flow of a fluid through the surface skin facesheet;a structural core layer coupled to and configured to structurally support a portion of the surface skin facesheet, wherein a portion of the structural core layer comprise flow channels spanning a thickness of the structural core layer;a channeled s...