RU1828827C - Aircraft cargo suspension and release device - Google Patents

Aircraft cargo suspension and release device

Info

Publication number
RU1828827C
RU1828827C SU904820063A SU4820063A RU1828827C RU 1828827 C RU1828827 C RU 1828827C SU 904820063 A SU904820063 A SU 904820063A SU 4820063 A SU4820063 A SU 4820063A RU 1828827 C RU1828827 C RU 1828827C
Authority
RU
Russia
Prior art keywords
aircraft
load
release device
aircraft cargo
rod
Prior art date
Application number
SU904820063A
Other languages
Russian (ru)
Inventor
Аркадий Дмитриевич Васильев
Сергей Евгеньевич Родных
Сергей Анатольевич Блохин
Александр Александрович Кузьмин
Василий Владиславович Дорохов
Original Assignee
Харьковское Высшее Военное Авиационное Инженерное Краснознаменное Училище
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 Харьковское Высшее Военное Авиационное Инженерное Краснознаменное Училище filed Critical Харьковское Высшее Военное Авиационное Инженерное Краснознаменное Училище
Priority to SU904820063A priority Critical patent/RU1828827C/en
Application granted granted Critical
Publication of RU1828827C publication Critical patent/RU1828827C/en

Links

Landscapes

  • Load-Engaging Elements For Cranes (AREA)

Abstract

Изобретение относитс  к самолетостроению и вертолетостроению, а именно к устройствам , обеспечивающим подвеску, удержание грузов на летательных аппаратах и их сброс. Целью изобретени   вл етс  сокращение времени и средств при снар жении летательного аппарата. Устройство содержит гибкий канат 1, опо сывающий груз 3 и закрепленный одним своим концом в замке 2, а другим св занный со штоком гидроцилиндра 8, Подъем груза 3 до упора в ложемент 5 осуществл ют с помощью штока гидроцилиндра 8, а сброс груза 3 путем открывани  замка 2 при срабатывании элементов управлени  сбросом 5 илThe invention relates to aircraft construction and helicopter engineering, and in particular to devices providing suspension, cargo holding on aircraft and their dumping. The aim of the invention is to reduce the time and cost of equipping an aircraft. The device contains a flexible rope 1, which encloses the load 3 and is fixed at one end to the lock 2 and connected to the rod of the hydraulic cylinder 8 with the other. The load 3 is lifted up to the stop in the lodgement 5 using the rod of the hydraulic cylinder 8, and the load 3 is released by opening lock 2 when triggering the control elements reset 5 silt

Description

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SU904820063A 1990-04-26 1990-04-26 Aircraft cargo suspension and release device RU1828827C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU904820063A RU1828827C (en) 1990-04-26 1990-04-26 Aircraft cargo suspension and release device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU904820063A RU1828827C (en) 1990-04-26 1990-04-26 Aircraft cargo suspension and release device

Publications (1)

Publication Number Publication Date
RU1828827C true RU1828827C (en) 1993-07-23

Family

ID=21511409

Family Applications (1)

Application Number Title Priority Date Filing Date
SU904820063A RU1828827C (en) 1990-04-26 1990-04-26 Aircraft cargo suspension and release device

Country Status (1)

Country Link
RU (1) RU1828827C (en)

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
Авторское свидетельство СССР NT- 284628, кл. В 64 D 1/02, 1969. *

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