RU1773804C - Parachute system - Google Patents

Parachute system

Info

Publication number
RU1773804C
RU1773804C SU904791434A SU4791434A RU1773804C RU 1773804 C RU1773804 C RU 1773804C SU 904791434 A SU904791434 A SU 904791434A SU 4791434 A SU4791434 A SU 4791434A RU 1773804 C RU1773804 C RU 1773804C
Authority
RU
Russia
Prior art keywords
control lines
cargo
parachute system
control
silt
Prior art date
Application number
SU904791434A
Other languages
Russian (ru)
Inventor
Валерий Геннадьевич Юрис
Original Assignee
Опытно-конструкторское бюро "Сокол"
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 Опытно-конструкторское бюро "Сокол" filed Critical Опытно-конструкторское бюро "Сокол"
Priority to SU904791434A priority Critical patent/RU1773804C/en
Application granted granted Critical
Publication of RU1773804C publication Critical patent/RU1773804C/en

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  • Emergency Lowering Means (AREA)

Abstract

Изобретение относитс  к авиационной технике и может быть использовано при создании средств десантировани  грузов, обладающих собственным флюгерным, моментом , и спасени  летательных аппаратов в аварийной ситуации. Целью изобретени   вл етс  повышение надежности управлени  куполом за счет исключени  защепле- ни  строп управлени . В управл емом парашютной системе, содержащей купол- крыло 1, подвесную систему 2 груза 3, основные стропы 4 и стропы 5 управлени , введена кинематическа  пара 7 с вращательной степенью свободы и отверстием 8 вдоль оси 9 вращени , через которое проход т стропы 5 управлени . 4 ил,The invention relates to aeronautical engineering and can be used to create means of airborne cargo possessing its own weather vane, moment, and rescue aircraft in an emergency. The aim of the invention is to increase the reliability of control of the dome by eliminating the clogging of the control lines. In a controlled parachute system comprising a canopy 1, a suspension system 2 of cargo 3, main slings 4 and control lines 5, a kinematic pair 7 with a rotational degree of freedom and a hole 8 along the axis of rotation 9 through which control lines 5 pass is introduced. 4 silt

Description

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SU904791434A 1990-02-14 1990-02-14 Parachute system RU1773804C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU904791434A RU1773804C (en) 1990-02-14 1990-02-14 Parachute system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU904791434A RU1773804C (en) 1990-02-14 1990-02-14 Parachute system

Publications (1)

Publication Number Publication Date
RU1773804C true RU1773804C (en) 1992-11-07

Family

ID=21496233

Family Applications (1)

Application Number Title Priority Date Filing Date
SU904791434A RU1773804C (en) 1990-02-14 1990-02-14 Parachute system

Country Status (1)

Country Link
RU (1) RU1773804C (en)

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
1. Крыль родины, № 3, 1989, с.9 2. Рекламный проспект фирмы Пзра- флайт (US) Система Пара-Пойнт - управл ема парашютна система, 1985. *

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