RU2012129485A - FLEXIBLE WING RESISTANT TO ADJACTION - Google Patents

FLEXIBLE WING RESISTANT TO ADJACTION Download PDF

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Publication number
RU2012129485A
RU2012129485A RU2012129485/11A RU2012129485A RU2012129485A RU 2012129485 A RU2012129485 A RU 2012129485A RU 2012129485/11 A RU2012129485/11 A RU 2012129485/11A RU 2012129485 A RU2012129485 A RU 2012129485A RU 2012129485 A RU2012129485 A RU 2012129485A
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RU
Russia
Prior art keywords
air
shell
pressure zone
adjaction
resistant
Prior art date
Application number
RU2012129485/11A
Other languages
Russian (ru)
Other versions
RU2527407C2 (en
Inventor
Виктор Иванович Шулига
Original Assignee
Виктор Иванович Шулига
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Application filed by Виктор Иванович Шулига filed Critical Виктор Иванович Шулига
Priority to RU2012129485/11A priority Critical patent/RU2527407C2/en
Publication of RU2012129485A publication Critical patent/RU2012129485A/en
Application granted granted Critical
Publication of RU2527407C2 publication Critical patent/RU2527407C2/en

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  • Tents Or Canopies (AREA)

Abstract

Крыло из гибкого материала, содержащее оболочку с аэродинамическим профилем поддерживаемом нервюрами, надуваемую встречным потоком воздуха через воздухозаборники с клапанами, и стропы, отличающееся тем, что воздухозаборники имеют как минимум две кромки, каждая их которых создает местную зону повышенного давления для местного потока обтекания своего направления и оснащена клапаном в зоне повышенного давления, пропускающим воздух внутрь оболочки.A wing made of flexible material containing a shell with an aerodynamic profile supported by ribs, inflated by a counter flow of air through the air intakes with valves, and slings, characterized in that the air intakes have at least two edges, each of which creates a local pressure zone for the local flow around its direction and is equipped with a valve in the high-pressure zone, passing air into the shell.

Claims (1)

Крыло из гибкого материала, содержащее оболочку с аэродинамическим профилем поддерживаемом нервюрами, надуваемую встречным потоком воздуха через воздухозаборники с клапанами, и стропы, отличающееся тем, что воздухозаборники имеют как минимум две кромки, каждая их которых создает местную зону повышенного давления для местного потока обтекания своего направления и оснащена клапаном в зоне повышенного давления, пропускающим воздух внутрь оболочки. A wing made of flexible material containing a shell with an aerodynamic profile supported by ribs, inflated by a counter flow of air through the air intakes with valves, and slings, characterized in that the air intakes have at least two edges, each of which creates a local pressure zone for the local flow around its direction and is equipped with a valve in the high-pressure zone, passing air into the shell.
RU2012129485/11A 2012-07-09 2012-07-09 Fold-resistant wing made of flexible material RU2527407C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2012129485/11A RU2527407C2 (en) 2012-07-09 2012-07-09 Fold-resistant wing made of flexible material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2012129485/11A RU2527407C2 (en) 2012-07-09 2012-07-09 Fold-resistant wing made of flexible material

Publications (2)

Publication Number Publication Date
RU2012129485A true RU2012129485A (en) 2014-01-20
RU2527407C2 RU2527407C2 (en) 2014-08-27

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ID=49944935

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2012129485/11A RU2527407C2 (en) 2012-07-09 2012-07-09 Fold-resistant wing made of flexible material

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RU (1) RU2527407C2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2584353C1 (en) * 2015-02-16 2016-05-20 Юрий Витальевич Швед Structural elements to increase safety of aircraft with soft wing
RU2708999C1 (en) * 2019-03-25 2019-12-12 Максим Скорик Flexible air-impermeable wing

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH676452A5 (en) * 1988-04-08 1991-01-31 Konrad Schafroth
CH700671A2 (en) * 2009-03-26 2010-09-30 Advance Thun Ag Paraglider canopy, has stagnation chamber divided by separating walls with respect to another stagnation chamber, and air inlet opening arranged above another air inlet opening in region of stagnation point of wing profile

Also Published As

Publication number Publication date
RU2527407C2 (en) 2014-08-27

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MM4A The patent is invalid due to non-payment of fees

Effective date: 20150710