RU1821417C - Helicopter system - Google Patents

Helicopter system

Info

Publication number
RU1821417C
RU1821417C SU4896402A RU1821417C RU 1821417 C RU1821417 C RU 1821417C SU 4896402 A SU4896402 A SU 4896402A RU 1821417 C RU1821417 C RU 1821417C
Authority
RU
Russia
Prior art keywords
helicopter
module
cable
control system
earth
Prior art date
Application number
Other languages
Russian (ru)
Inventor
Александр Алексеевич Таранцев
Original Assignee
А.А.Таранцев .
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 А.А.Таранцев . filed Critical А.А.Таранцев .
Priority to SU4896402 priority Critical patent/RU1821417C/en
Application granted granted Critical
Publication of RU1821417C publication Critical patent/RU1821417C/en

Links

Abstract

Изобретение относитс  к области авиации , в частности к вертолетостроению и эксплуатации вертолетных систем. Целью изобретени   вл етс  расширение функциональных возможнбстей таких систем путем применени  автономных пилотируемых на внешней подвеске управл емых грузовых модулей. При этом вертолетна  система включает вертолет 1 и управл емый грузовой модуль 18, соединенные между собой кабель-тросом 10. Грузовой модуль снабжен органами управлени  13,14 и органами перемещени  по земной поверхности, а также кабиной экипажа с системой автономного управлени  модулем и системой дистанционного по кабель-тросу управлени  несущим его вертолётом, а вертолет снабжен системой дистанционного управлени  модулем . Кроме того, грузовой модуль снабжен собственной силовой установкой, обеспечивающей перемещение его по земной поверхности, как транспортное средство и снабжение вертолетной системы энергией в полете в аварийных ситуаци х. 1 з.п.ф-лы, 6 ил.The invention relates to the field of aviation, in particular to helicopter engineering and the operation of helicopter systems. The aim of the invention is to expand the functional capabilities of such systems by using autonomous external-piloted controlled load modules. In this case, the helicopter system includes a helicopter 1 and a controlled cargo module 18, interconnected by a cable-cable 10. The cargo module is equipped with governing bodies 13,14 and moving bodies on the earth's surface, as well as a crew cabin with an autonomous control system for the module and a remote control system a control cable for the helicopter carrying it, and the helicopter is equipped with a module remote control system. In addition, the cargo module is equipped with its own power plant, providing its movement on the earth's surface, like a vehicle and supplying the helicopter system with energy in flight in emergency situations. 1 C.p. f-ls, 6 ill.

Description

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SU4896402 1990-12-27 1990-12-27 Helicopter system RU1821417C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4896402 RU1821417C (en) 1990-12-27 1990-12-27 Helicopter system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4896402 RU1821417C (en) 1990-12-27 1990-12-27 Helicopter system

Publications (1)

Publication Number Publication Date
RU1821417C true RU1821417C (en) 1993-06-15

Family

ID=21552055

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4896402 RU1821417C (en) 1990-12-27 1990-12-27 Helicopter system

Country Status (1)

Country Link
RU (1) RU1821417C (en)

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
Политехнический словарь, Госиздат, М.; с.77. рис.3.1989, Изаксон A.M. Советское вертолетостро- ение, М.:с.243,.1981. Вахитов А. Ф. Вертолет Ка-26, М., Транспорт, с.3-7, 1973. *

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