RU99120934A - DEVICE FOR MOVING IN THE AIR ENVIRONMENT SV Budanov - Google Patents

DEVICE FOR MOVING IN THE AIR ENVIRONMENT SV Budanov

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Publication number
RU99120934A
RU99120934A RU99120934/28A RU99120934A RU99120934A RU 99120934 A RU99120934 A RU 99120934A RU 99120934/28 A RU99120934/28 A RU 99120934/28A RU 99120934 A RU99120934 A RU 99120934A RU 99120934 A RU99120934 A RU 99120934A
Authority
RU
Russia
Prior art keywords
wing
fuselage
moving
additional
budanov
Prior art date
Application number
RU99120934/28A
Other languages
Russian (ru)
Other versions
RU2172701C2 (en
Inventor
Станислав Васильевич Буданов
Original Assignee
Станислав Васильевич Буданов
Filing date
Publication date
Application filed by Станислав Васильевич Буданов filed Critical Станислав Васильевич Буданов
Priority to RU99120934/28A priority Critical patent/RU2172701C2/en
Priority claimed from RU99120934/28A external-priority patent/RU2172701C2/en
Publication of RU99120934A publication Critical patent/RU99120934A/en
Application granted granted Critical
Publication of RU2172701C2 publication Critical patent/RU2172701C2/en

Links

Claims (1)

Устройство для перемещения в воздушной среде, включающее фюзеляж с хвостовым оперением в виде киля с рулем поворота и стабилизатора, нижнее крыло, верхнее крыло, руль высоты, отличающееся тем, что оно снабжено опорной площадкой, механизмом передвижения верхнего крыла и дополнительным крылом, при этом опорная площадка выполнена на верхней поверхности фюзеляжа, механизм передвижения верхнего крыла состоит из двух направляющих со стойками на концах, четырех ползунов и привода в виде двух силовых цилиндров, а плоскости дополнительного крыла закреплены по бокам хвостовой части фюзеляжа, причем верхнее крыло связано с ползунами и штоком силовых цилиндров, направляющие расположены друг против друга и симметрично относительно продольной оси фюзеляжа, руль высоты смонтирован на плоскостях дополнительного крыла, размер поперечного сечения фюзеляжа одинаковый на всей длине салона, а размах крыльев определен соотношением:
Л1 = Д + 2 • Б;
Figure 00000001

Figure 00000002

где Л1, Л2, Л3 - соответственно размах нижнего, верхнего и дополнительного крыла;
Д - ширина фюзеляжа;
Б - длина плоскости нижнего крыла.A device for moving in the air, including a fuselage with a tail in the form of a keel with a rudder and stabilizer, lower wing, upper wing, elevator, characterized in that it is equipped with a support platform, a mechanism for moving the upper wing and an additional wing, while supporting the platform is made on the upper surface of the fuselage, the mechanism of movement of the upper wing consists of two guides with struts at the ends, four sliders and a drive in the form of two power cylinders, and the plane of the additional wing fixed on the sides of the rear part of the fuselage, with the upper wing connected to the sliders and the rod of the power cylinders, the guides are located opposite each other and symmetrically relative to the longitudinal axis of the fuselage, the elevator is mounted on the planes of the additional wing, the cross-sectional size of the fuselage is the same along the entire length of the cabin, and the span wings defined by the ratio:
L 1 = D + 2 • B;
Figure 00000001

Figure 00000002

where L 1 , L 2 , L 3 - respectively, the scope of the lower, upper and additional wings;
D is the width of the fuselage;
B - the length of the plane of the lower wing.
RU99120934/28A 1999-10-04 1999-10-04 Device for motion in air medium RU2172701C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU99120934/28A RU2172701C2 (en) 1999-10-04 1999-10-04 Device for motion in air medium

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU99120934/28A RU2172701C2 (en) 1999-10-04 1999-10-04 Device for motion in air medium

Publications (2)

Publication Number Publication Date
RU99120934A true RU99120934A (en) 2001-08-10
RU2172701C2 RU2172701C2 (en) 2001-08-27

Family

ID=35873557

Family Applications (1)

Application Number Title Priority Date Filing Date
RU99120934/28A RU2172701C2 (en) 1999-10-04 1999-10-04 Device for motion in air medium

Country Status (1)

Country Link
RU (1) RU2172701C2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10850828B2 (en) * 2017-03-30 2020-12-01 The Boeing Company Movable wing for weight and balance management
CN108263596A (en) * 2018-03-07 2018-07-10 陕西金色科技有限公司 A kind of Quick-disassembling mechanism and its method of adjustment of adjust automatically wing position
CN108688793B (en) * 2018-07-27 2023-11-24 中国工程物理研究院总体工程研究所 Folding and unfolding mechanism for wings of barrel-type launching unmanned aerial vehicle

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