CN100513256C - 一种增加升力和失速迎角的篷翼 - Google Patents

一种增加升力和失速迎角的篷翼 Download PDF

Info

Publication number
CN100513256C
CN100513256C CNB021338620A CN02133862A CN100513256C CN 100513256 C CN100513256 C CN 100513256C CN B021338620 A CNB021338620 A CN B021338620A CN 02133862 A CN02133862 A CN 02133862A CN 100513256 C CN100513256 C CN 100513256C
Authority
CN
China
Prior art keywords
wing
paulin
airfoil
lift
stalling
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CNB021338620A
Other languages
English (en)
Chinese (zh)
Other versions
CN1517269A (zh
Inventor
朱上翔
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CNB021338620A priority Critical patent/CN100513256C/zh
Priority to AU2003289606A priority patent/AU2003289606A1/en
Priority to PCT/CN2003/001035 priority patent/WO2004092009A1/fr
Publication of CN1517269A publication Critical patent/CN1517269A/zh
Application granted granted Critical
Publication of CN100513256C publication Critical patent/CN100513256C/zh
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/54Varying in area

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CNB021338620A 2003-01-17 2003-01-17 一种增加升力和失速迎角的篷翼 Expired - Fee Related CN100513256C (zh)

Priority Applications (3)

Application Number Priority Date Filing Date Title
CNB021338620A CN100513256C (zh) 2003-01-17 2003-01-17 一种增加升力和失速迎角的篷翼
AU2003289606A AU2003289606A1 (en) 2003-01-17 2003-12-04 A Wing ASSEMBLY CAPABLE OF INCREASIGN THE LIFT AND THE ANGLE OF STALL
PCT/CN2003/001035 WO2004092009A1 (fr) 2003-01-17 2003-12-04 Ensemble aile capable d'augmenter la portance et l'angle de decrochage

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNB021338620A CN100513256C (zh) 2003-01-17 2003-01-17 一种增加升力和失速迎角的篷翼

Publications (2)

Publication Number Publication Date
CN1517269A CN1517269A (zh) 2004-08-04
CN100513256C true CN100513256C (zh) 2009-07-15

Family

ID=34231318

Family Applications (1)

Application Number Title Priority Date Filing Date
CNB021338620A Expired - Fee Related CN100513256C (zh) 2003-01-17 2003-01-17 一种增加升力和失速迎角的篷翼

Country Status (3)

Country Link
CN (1) CN100513256C (fr)
AU (1) AU2003289606A1 (fr)
WO (1) WO2004092009A1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009006212A1 (de) * 2009-01-27 2010-09-23 Fritz Unger Verfahren zur Steigerung des Auftriebs von Tragflügeln
US8882470B2 (en) 2011-01-07 2014-11-11 Fritz Unger Rotor for a wind power generator
US9016637B2 (en) * 2012-02-10 2015-04-28 The Boeing Company High-positioned 3-position variable camber krueger
CN113968341B (zh) * 2021-12-08 2024-01-26 北京航空航天大学 一种使用仿生小翼的微型无人机
CN114506442B (zh) * 2022-01-28 2024-07-05 中国商用飞机有限责任公司 带有扰流辅助装置的机翼及包括其的飞行装置

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2237254A (en) * 1989-10-25 1991-05-01 Richard Harry Barnard Secondary lifting surfaces using separated flow
CN2095830U (zh) * 1991-04-22 1992-02-12 林永克 空气螺旋桨
DE4140139A1 (de) * 1991-12-05 1993-06-09 Klaus Dipl.-Werkmeister 6600 Saarbruecken De Lellig Umsteuerbares flugzeug vom ein- zum doppeldecker
CN2186706Y (zh) * 1994-01-24 1995-01-04 南京理工大学 一种高升力捕涡机翼
US5772155A (en) * 1996-06-01 1998-06-30 Nowak; Dieter K. Aircraft wing flaps

Also Published As

Publication number Publication date
WO2004092009A1 (fr) 2004-10-28
AU2003289606A1 (en) 2004-11-04
CN1517269A (zh) 2004-08-04

Similar Documents

Publication Publication Date Title
CN108995803B (zh) 一种超声速客机的可折叠式乘波体气动布局结构及方法
US9555895B2 (en) Motor pylons for a kite and airborne power generation system using same
US5681014A (en) Torsional twist airfoil control means
US5842666A (en) Laminar supersonic transport aircraft
US10377471B2 (en) Apparatus, system and method for drag reduction
US7475848B2 (en) Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance
US5772155A (en) Aircraft wing flaps
US4460138A (en) Flexible flap for an airfoil
CN108639339B (zh) 一种无人机气动布局
CN110667822B (zh) 一种可变面积可转动的仿生翼梢小翼
US20070262205A1 (en) Retractable multiple winglet
CN113291459B (zh) 一种分布式涵道风扇高升力***及其使用方法
CN111017194B (zh) 一种动力增升机翼
CN210235305U (zh) 一种可变机翼外翼后掠角和可倾斜小翼的飞翼式飞机
US20050116116A1 (en) Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance
US6935592B2 (en) Aircraft lift device for low sonic boom
Boermans Research on sailplane aerodynamics at Delft University of Technology
US4093156A (en) Supersonic transport
CN110550216A (zh) 一种动力提升地效飞行器
CN100513256C (zh) 一种增加升力和失速迎角的篷翼
CN112173065A (zh) 一种应用于倾转机翼飞机的机翼
CN210822780U (zh) 一种动力提升地效飞行器
US20070290098A1 (en) Airfoil having a movable control surface
CN219192541U (zh) 一种仿生鹰翼翼梢小翼气动结构
WO2013104007A1 (fr) Pylônes à moteur pour un cerf-volant et système de génération d'énergie aéroporté les utilisant

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C57 Notification of unclear or unknown address
DD01 Delivery of document by public notice

Addressee: Guo Xiaodong

Document name: Deemed as a notice of withdrawal

C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
C56 Change in the name or address of the patentee
CP02 Change in the address of a patent holder

Address after: 214177, Zhu Shangxiang, two, building C20, 18 Xin Yan Dong Road, Huishan District, Jiangsu, Wuxi

Patentee after: Zhu Shangxiang

Address before: 100093, Zhu Hongzhuan, Zhu Shangxiang, 2811, Xiangshan art villa No. 88, Xiangshan South Road, Beijing, Haidian District

Patentee before: Zhu Shangxiang

CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20090715

Termination date: 20160117

EXPY Termination of patent right or utility model