RU1818272C - Aircraft - Google Patents

Aircraft

Info

Publication number
RU1818272C
RU1818272C SU4862693A RU1818272C RU 1818272 C RU1818272 C RU 1818272C SU 4862693 A SU4862693 A SU 4862693A RU 1818272 C RU1818272 C RU 1818272C
Authority
RU
Russia
Prior art keywords
aircraft
wings
angle
fezul
gliders
Prior art date
Application number
Other languages
Russian (ru)
Inventor
Сергей Николаевич Селиванов
Original Assignee
Selivanov Sergej N
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 Selivanov Sergej N filed Critical Selivanov Sergej N
Priority to SU4862693 priority Critical patent/RU1818272C/en
Application granted granted Critical
Publication of RU1818272C publication Critical patent/RU1818272C/en

Links

Landscapes

  • Buildings Adapted To Withstand Abnormal External Influences (AREA)

Abstract

Изобретение относитс  к самолетостроению , а именно к конструкци м планеров и самолетов. Целью изобретени   вл етс  снижение веса летательного аппарата и улучшение аэродинамических характеристик . Летательный аппарат содержит фезю- л ж 1 и крыль  2 и 3, установленные по схеме тандем. Крыль  2 и 3 выполнены одинакового размаха и снабжены установленными на их торцах законцовками 5 конической формы с углом стреловидности 60-62° и отклоненными вниз на угол 12-16°. Переднее крыло 2 установлено выше заднего крыла 3. Крыль  2 и 3 имеют органы управлени  4.3 ил.FIELD OF THE INVENTION The invention relates to aircraft construction, and in particular to structures of gliders and aircraft. The aim of the invention is to reduce aircraft weight and improve aerodynamic performance. The aircraft contains a fezul g 1 and wings 2 and 3 mounted in tandem. Wings 2 and 3 are made of the same size and provided with conical ends 5 mounted on their ends with a sweep angle of 60-62 ° and deflected downward at an angle of 12-16 °. The front wing 2 is mounted above the rear wing 3. The wings 2 and 3 have controls 4.3 ill.

SU4862693 1990-07-09 1990-07-09 Aircraft RU1818272C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4862693 RU1818272C (en) 1990-07-09 1990-07-09 Aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4862693 RU1818272C (en) 1990-07-09 1990-07-09 Aircraft

Publications (1)

Publication Number Publication Date
RU1818272C true RU1818272C (en) 1993-05-30

Family

ID=21534071

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4862693 RU1818272C (en) 1990-07-09 1990-07-09 Aircraft

Country Status (1)

Country Link
RU (1) RU1818272C (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7841559B1 (en) 2006-02-16 2010-11-30 Mbda Incorporated Aerial vehicle with variable aspect ratio deployable wings
RU2597742C1 (en) * 2015-07-20 2016-09-20 Юлия Алексеевна Щепочкина Aircraft

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7841559B1 (en) 2006-02-16 2010-11-30 Mbda Incorporated Aerial vehicle with variable aspect ratio deployable wings
RU2597742C1 (en) * 2015-07-20 2016-09-20 Юлия Алексеевна Щепочкина Aircraft

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