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RU1828444C - Airship - Google Patents

Airship

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Publication number
RU1828444C
RU1828444C SU904866158A SU4866158A RU1828444C RU 1828444 C RU1828444 C RU 1828444C SU 904866158 A SU904866158 A SU 904866158A SU 4866158 A SU4866158 A SU 4866158A RU 1828444 C RU1828444 C RU 1828444C
Authority
RU
Russia
Prior art keywords
tail
rotary wing
airship
rudders
distance
Prior art date
Application number
SU904866158A
Other languages
Russian (ru)
Inventor
Владислав Евгеньевич Кульчицкий
Original Assignee
В.Е Кульчицкий
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 В.Е Кульчицкий filed Critical В.Е Кульчицкий
Priority to SU904866158A priority Critical patent/RU1828444C/en
Application granted granted Critical
Publication of RU1828444C publication Critical patent/RU1828444C/en

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  • Transmission Devices (AREA)

Abstract

Изобретение относитс  к летательным аппаратам, использующим аэростатическую подъемную силу, в частности к дирижабл м . Целью изобретени   вл етс  улучшение летно-технических характеристик путем повышени  маневренности. Дирижабль содержит оболочку 14 обтекаемой формы, гондолу 1, хвостовое оперение с рул ми высоты 11 и направлени  13, поворотное крыло 3 и двигатели с винтами, за- крепленные на поворотном крыле 3. Дирижабль снабжен передним вертикальным оперением с рул ми 7, закрепленными на каждой консоли поворотного крыла 3. Хвостовое вертикальное оперение выполнено разнесенным Рассто ние между кил ми переднего и хвостового 12 вертикальных оперений равно рассто нию между ос ми винтов и составл ет не менее диаметра оболочки , а диапазон углов поворота крыла от горизонтального положени  ±120°. 3 ил.The invention relates to aircraft using aerostatic lift, in particular to airships. The aim of the invention is to improve flight performance by increasing maneuverability. The airship contains a streamlined shell 14, a nacelle 1, tail unit with rudders 11 and direction 13, a rotary wing 3 and engines with screws mounted on a rotary wing 3. The airship is equipped with a front vertical tail unit with rudders 7 attached to each console of the rotary wing 3. Tail vertical tail made spaced The distance between the keels of the front and tail 12 vertical tail is equal to the distance between the axes of the screws and is not less than the diameter of the shell, and the range of angles of rotation to snouts from a horizontal position of ± 120 °. 3 ill.

Description

Фиг 2Fig 2

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ФигЗFigz

SU904866158A 1990-07-04 1990-07-04 Airship RU1828444C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU904866158A RU1828444C (en) 1990-07-04 1990-07-04 Airship

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU904866158A RU1828444C (en) 1990-07-04 1990-07-04 Airship

Publications (1)

Publication Number Publication Date
RU1828444C true RU1828444C (en) 1993-07-15

Family

ID=21536018

Family Applications (1)

Application Number Title Priority Date Filing Date
SU904866158A RU1828444C (en) 1990-07-04 1990-07-04 Airship

Country Status (1)

Country Link
RU (1) RU1828444C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008097136A1 (en) 2007-02-05 2008-08-14 Boris Vasileevich Khakimov Emergency and rescue aircraft

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
Арие М.Я , Пол нкер А.Г. Дирижабль нового поколени Киев; Наукова Думка, 1983, с 149. Арие М.Я., Пол нкер А Г Дирижабль нового поколени . Киев, Наукова Думка, 1983, с.159- 160 Итоги науки и техники, сери Авиаци , том 8, М., ВИНИТИ, 1984, с.49. *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008097136A1 (en) 2007-02-05 2008-08-14 Boris Vasileevich Khakimov Emergency and rescue aircraft

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