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SU1762488A1 - Adaptive wing - Google Patents

Adaptive wing

Info

Publication number
SU1762488A1
SU1762488A1 SU4786820/23A SU4786820A SU1762488A1 SU 1762488 A1 SU1762488 A1 SU 1762488A1 SU 4786820/23 A SU4786820/23 A SU 4786820/23A SU 4786820 A SU4786820 A SU 4786820A SU 1762488 A1 SU1762488 A1 SU 1762488A1
Authority
SU
USSR - Soviet Union
Prior art keywords
panels
wing
caisson
flexible skin
places
Prior art date
Application number
SU4786820/23A
Other languages
Russian (ru)
Inventor
Г.А. Амирьянц
Original Assignee
Центральный аэрогидродинамический институт им.проф.Н.Е.Жуковского
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 Центральный аэрогидродинамический институт им.проф.Н.Е.Жуковского filed Critical Центральный аэрогидродинамический институт им.проф.Н.Е.Жуковского
Priority to SU4786820/23A priority Critical patent/SU1762488A1/en
Application granted granted Critical
Publication of SU1762488A1 publication Critical patent/SU1762488A1/en

Links

Landscapes

  • Laminated Bodies (AREA)

Abstract

FIELD: aeronautics. SUBSTANCE: wing is provided by reinforced elastomeric panels 15, rigidly connected with a framework, flexible skin and caisson. The panels are arranged on places of butt joining of sections 8, 9, 10 and of nose and tail wing part sections and also on places of the flexible skin and the caisson butt joining. The panels, the flexible skin and surface of the caisson are covered by elastic film; reinforcing walls of the panels 15 are arranged along normal line relative to the wing profile contour. Flexible ramrods are passed through the panels 15; the film may have riblets. There are isolated spaces 24. EFFECT: enhanced aerodynamic properties of wing and increased damping degree of deformable parts of wing. 4 cl, 8 dwg
SU4786820/23A 1990-01-30 1990-01-30 Adaptive wing SU1762488A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4786820/23A SU1762488A1 (en) 1990-01-30 1990-01-30 Adaptive wing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4786820/23A SU1762488A1 (en) 1990-01-30 1990-01-30 Adaptive wing

Publications (1)

Publication Number Publication Date
SU1762488A1 true SU1762488A1 (en) 1994-04-30

Family

ID=60532866

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4786820/23A SU1762488A1 (en) 1990-01-30 1990-01-30 Adaptive wing

Country Status (1)

Country Link
SU (1) SU1762488A1 (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2130858C1 (en) * 1997-10-22 1999-05-27 Акционерное общество открытого типа "ОКБ Сухого" Flying vehicle variable-camber wing
RU2337430C2 (en) * 2005-11-22 2008-10-27 Онэра (Оффис Насьональ Д`Этюд Э Де Решерш Аэроспасьяль) Flat drive with foliated structure, flat drive device and lifting plane of aircraft
RU2414386C2 (en) * 2005-06-16 2011-03-20 Эйрбас Дойчланд Гмбх Rotary element to increase lift, particularly, deflecting wing tip with high aerodynamic characteristic
RU2557581C1 (en) * 2013-12-30 2015-07-27 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Новосибирский государственный технический университет" Adaptive wing
RU2625478C2 (en) * 2012-04-19 2017-07-14 Зе Боинг Компани Elastomer control surface based on continuous bypassing processing technology
RU2652536C1 (en) * 2017-01-24 2018-04-26 федеральное государственное бюджетное образовательное учреждение высшего образования "Уфимский государственный авиационный технический университет" Adaptive wing
RU2698600C1 (en) * 2016-04-29 2019-08-28 Фасс Аг Aircraft with a winglet or a plane control element
US11174002B2 (en) 2016-02-29 2021-11-16 Flexsys, Inc. Edge morphing arrangement for an airfoil
RU2787983C1 (en) * 2022-08-19 2023-01-16 Федеральное автономное учреждение "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФАУ "ЦАГИ") Active wing tip

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2130858C1 (en) * 1997-10-22 1999-05-27 Акционерное общество открытого типа "ОКБ Сухого" Flying vehicle variable-camber wing
RU2414386C2 (en) * 2005-06-16 2011-03-20 Эйрбас Дойчланд Гмбх Rotary element to increase lift, particularly, deflecting wing tip with high aerodynamic characteristic
US7963484B2 (en) 2005-06-16 2011-06-21 Airbus Deutschland Gmbh Lift-augmenting flap, in particular for a leading edge flap, for an aerodynamically effective wing
RU2337430C2 (en) * 2005-11-22 2008-10-27 Онэра (Оффис Насьональ Д`Этюд Э Де Решерш Аэроспасьяль) Flat drive with foliated structure, flat drive device and lifting plane of aircraft
RU2625478C2 (en) * 2012-04-19 2017-07-14 Зе Боинг Компани Elastomer control surface based on continuous bypassing processing technology
RU2557581C1 (en) * 2013-12-30 2015-07-27 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Новосибирский государственный технический университет" Adaptive wing
US11174002B2 (en) 2016-02-29 2021-11-16 Flexsys, Inc. Edge morphing arrangement for an airfoil
RU2698600C1 (en) * 2016-04-29 2019-08-28 Фасс Аг Aircraft with a winglet or a plane control element
RU2652536C1 (en) * 2017-01-24 2018-04-26 федеральное государственное бюджетное образовательное учреждение высшего образования "Уфимский государственный авиационный технический университет" Adaptive wing
RU2787983C1 (en) * 2022-08-19 2023-01-16 Федеральное автономное учреждение "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФАУ "ЦАГИ") Active wing tip
RU2837710C1 (en) * 2023-11-02 2025-04-03 Алексей Владимирович Потудинский Flexible wing with variable bend

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