南方科技大学知识苑(SUSTech KC): 一种基于翼尖涡流增升的飞行器

Title	一种基于翼尖涡流增升的飞行器
Alternative Title	Aircraft based on tip vortex lift -rising
Author	许振宇
First Inventor	许振宇
Original applicant	南方科技大学
First applicant	南方科技大学
Address of First applicant	518055 广东省深圳市南山区西丽学苑大道1088号
Current applicant	南方科技大学
Address of Current applicant	518055 广东省深圳市南山区西丽学苑大道1088号 (广东,深圳,南山区)
First Current Applicant	南方科技大学
Address of First Current Applicant	518055 广东省深圳市南山区西丽学苑大道1088号 (广东,深圳,南山区)
Application Number	CN201820106476.7
Application Date	2018-01-23
Open (Notice) Number	CN207943171U
Date Available	2018-10-09
Publication Years	2018-10-09
Status of Patent	授权 ; 一案双申
Legal Date	2018-10-09
Subtype	实用新型
SUSTech Authorship	First
Abstract	本实用新型涉及飞行器领域，公开了一种基于翼尖涡流增升的飞行器，包括机身和固定在机身上的主机翼，主机翼上安装有主机翼动力组，主机翼动力组包括主机翼电机与主机翼螺旋桨，其特征在于，还包括固定在机身上的鸭翼，以及安装在鸭翼上的鸭翼动力组，鸭翼动力组包括鸭翼电机与鸭翼螺旋桨，其中，鸭翼位于主机翼的上方，鸭翼螺旋桨位于鸭翼的翼尖，且鸭翼螺旋桨的旋向与所在鸭翼的翼尖涡流的旋向一致。本实用新型通过在鸭翼的翼尖设置与翼尖涡旋向相同的鸭翼螺旋桨，增强鸭翼的翼尖涡旋以向主机翼提供涡升力，从而达到增升的效果，提升了飞行器的升阻比，增加了飞行器载重与续航能力。
Other Abstract	The utility model relates to an aircraft field discloses an aircraft based on tip vortex lift -rising, include the fuselage and fix the host computer wing on the fuselage, install host computer wing power package on the host computer wing, host computer wing power package includes host computer wing motor and host computer wing screw, a serial communication port, still including fixing the duck wing on the fuselage, and install the duck wing power package on the duck wing, duck wing power package includes duck wing motor and duck wing screw, wherein, the duck wing is located the top of the host computer wing, duck wing screw is located the wing tip of the duck wing, and the revolving to the unanimity to the tip vortex with the place duck wing soon of duck wing screw. The utility model discloses a wing tip setting of the duck wing and wing tip vortex to the same duck wing screw, the wing tip vortex of the reinforcing duck wing is in order to provide whirlpool lift to the host computer wing to reach the effect of lift -rising, the lift -to -drag who has promoted the aircraft compares, has increased aircraft load and duration.
IPC Classification Number	B64C39/08 ; B64C39/12 ; B64C3/36
INPADOC Legal Status	（+PATENT GRANT）[2018-10-09][CN]
INPADOC Patent Family Count	1
Extended Patent Family Count	2
Priority date	2018-01-23
Patent Agent	谢岳鹏
Agency	广州嘉权专利商标事务所有限公司
URL	[Source Record]
Data Source	PatSnap
Document Type	Patent
Identifier	http://kc.sustech.edu.cn/handle/2SGJ60CL/531555
Department	Department of Mechanics and Aerospace Engineering
Recommended Citation GB/T 7714	许振宇. 一种基于翼尖涡流增升的飞行器[P]. 2018-10-09.

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