RU2744901C1 - Device for braking an object ejected from a transport container on a rope - Google Patents

Device for braking an object ejected from a transport container on a rope Download PDF

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Publication number
RU2744901C1
RU2744901C1 RU2020123181A RU2020123181A RU2744901C1 RU 2744901 C1 RU2744901 C1 RU 2744901C1 RU 2020123181 A RU2020123181 A RU 2020123181A RU 2020123181 A RU2020123181 A RU 2020123181A RU 2744901 C1 RU2744901 C1 RU 2744901C1
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RU
Russia
Prior art keywords
rope
bushings
bushing
transport
braking
Prior art date
Application number
RU2020123181A
Other languages
Russian (ru)
Inventor
Павел Андреевич Агнистиков
Юрий Николаевич Левченко
Владимир Данилович Матрусов
Елтуган Кимашевич Сыздыков
Валерий Анатольевич Щеглов
Original Assignee
Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка"
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.)
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Publication date
Application filed by Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" filed Critical Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка"
Priority to RU2020123181A priority Critical patent/RU2744901C1/en
Application granted granted Critical
Publication of RU2744901C1 publication Critical patent/RU2744901C1/en

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    • A—HUMAN NECESSITIES
    • A62—LIFE-SAVING; FIRE-FIGHTING
    • A62B—DEVICES, APPARATUS OR METHODS FOR LIFE-SAVING
    • A62B1/00—Devices for lowering persons from buildings or the like
    • A62B1/06—Devices for lowering persons from buildings or the like by making use of rope-lowering devices
    • A62B1/08—Devices for lowering persons from buildings or the like by making use of rope-lowering devices with brake mechanisms for the winches or pulleys
    • A62B1/12—Devices for lowering persons from buildings or the like by making use of rope-lowering devices with brake mechanisms for the winches or pulleys hydraulically operated
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H51/00—Forwarding filamentary material
    • B65H51/02—Rotary devices, e.g. with helical forwarding surfaces
    • B65H51/04—Rollers, pulleys, capstans, or intermeshing rotary elements
    • B65H51/08—Rollers, pulleys, capstans, or intermeshing rotary elements arranged to operate in groups or in co-operation with other elements
    • B65H51/10—Rollers, pulleys, capstans, or intermeshing rotary elements arranged to operate in groups or in co-operation with other elements with opposed coacting surfaces, e.g. providing nips
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H59/00—Adjusting or controlling tension in filamentary material, e.g. for preventing snarling; Applications of tension indicators
    • B65H59/38—Adjusting or controlling tension in filamentary material, e.g. for preventing snarling; Applications of tension indicators by regulating speed of driving mechanism of unwinding, paying-out, forwarding, winding, or depositing devices, e.g. automatically in response to variations in tension
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Remote Sensing (AREA)
  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Load-Engaging Elements For Cranes (AREA)

Abstract

FIELD: aviation and rocket technology.
SUBSTANCE: invention relates in particular to the design of devices for braking objects launched from a transport and launch container, and subsequent towing of an object on a rope to prevent the tow rope from breaking. The invention can also be used in devices for throwing objects tied with a rope, with the subsequent use of the rope, for example, in firefighting or mountaineering gear. The device consists of a bushing with a helical groove and two split bushings. The cut edges of the bushings overlap one another. The bushings are made of thin sheet spring steel and are thin-walled cylinders. One of the bushings fixes the first part of the rope in a bushing with a helical groove. The second bushing fixes the second part of the rope wound on the outer surface of the first bushing. In this case, the inner diameter of the bushings is less than the outer diameter of the rope winding. The rope is connected to the ejected object using a swivel. The protrusions in the transport and launch container have a rounded shape.
EFFECT: programmed braking of objects launched from the transport and launch container to prevent breaking the towing rope.
1 cl, 4 dwg

Description

Изобретение относится к авиационной и ракетной технике, в частности к конструкции устройств для торможения объектов, запускаемых из транспортно-пускового контейнера и последующей буксировки объекта на канате для предотвращения обрыва буксировочного каната. Может также использоваться в устройствах для забрасывания объектов, связанных канатом с последующим использованием каната (например, в снаряжении пожарных, альпинистском снаряжении и др.).The invention relates to aviation and rocket technology, in particular to the design of devices for braking objects launched from a transport and launch container and subsequent towing of an object on a rope to prevent the tow rope from breaking. It can also be used in devices for throwing objects tied with a rope with the subsequent use of the rope (for example, in equipment for firefighters, mountaineering equipment, etc.).

Прототип не найден.No prototype found.

Предлагаемым изобретением решается задача программируемого торможения объектов, запускаемых из транспортно-пускового контейнера для предотвращения обрыва буксировочного каната.The proposed invention solves the problem of programmed braking of objects launched from the transport-launch container to prevent the towing rope from breaking.

Устройство для торможения объекта (далее - устройство), выбрасываемого из транспортно-пускового контейнера (далее - ТПК) на канате представлено на фиг. 1…4.A device for braking an object (hereinafter referred to as a device) ejected from a transport and launch container (hereinafter referred to as a TPK) on a rope is shown in Fig. 1 ... 4.

На фиг. 1 и фиг. 2 представлено устройство в сложенном положении на объекте, размещенном в транспортно-пусковом контейнере.FIG. 1 and FIG. 2 shows the device in a folded position on an object located in a transport and launch container.

На фиг. 3 представлена втулка с винтовой канавкой для размещения каната.FIG. 3 shows a bushing with a helical groove to accommodate a rope.

На фиг. 4 представлена одна из разрезных втулок для закрепления каната.FIG. 4 shows one of the split sleeves for securing the rope.

Представленное на фиг. 1 и фиг. 2 устройство состоит из втулки 1 с винтовой канавкой, закрепленной на ТПК, каната 2 и двух разрезных втулок 3 и 4.As shown in FIG. 1 and FIG. 2, the device consists of a bushing 1 with a helical groove fixed to the TPK, a rope 2 and two split bushings 3 and 4.

Втулка 1 закреплена на ТПК и имеет гнездо, куда ввернут пиропатрон. Первая часть каната 2 уложена в винтовую канавку втулки 1 и удерживается в ней разрезной втулкой 3. Вторая часть каната 2 намотана на наружную Bushing 1 is fixed on the TPK and has a socket where the squib is screwed. The first part of the rope 2 is laid in the helical groove of the sleeve 1 and is held in it by the split sleeve 3. The second part of the rope 2 is wound on the outer

Claims (1)

Устройство для торможения объекта, выбрасываемого из транспортно-пускового контейнера на канате, характеризующееся тем, что состоит из втулки с винтовой канавкой, двух разрезных втулок, грани разреза которых заходят одна на другую, выполненных из тонколистовой пружинной стали, представляющих собой тонкостенные цилиндры, одна из втулок фиксирует первую часть каната во втулке с винтовой канавкой, вторая втулка фиксирует вторую часть каната, намотанную на наружной поверхности первой втулки, при этом внутренний диаметр втулок меньше наружного диаметра намотки каната, который соединен с выбрасываемым объектом с помощью вертлюга, а выступы в транспортно-пусковом контейнере имеют округленную форму. A device for braking an object ejected from a transport and launch container on a rope, characterized by the fact that it consists of a bushing with a helical groove, two split bushings, the cut edges of which overlap one another, made of thin sheet spring steel, which are thin-walled cylinders, one of bushings fixes the first part of the rope in a bushing with a helical groove, the second bushing fixes the second part of the rope wound on the outer surface of the first bushing, while the inner diameter of the bushings is less than the outer diameter of the rope winding, which is connected to the ejected object using a swivel, and the protrusions in the transport the launch container have a rounded shape.
RU2020123181A 2020-07-07 2020-07-07 Device for braking an object ejected from a transport container on a rope RU2744901C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2020123181A RU2744901C1 (en) 2020-07-07 2020-07-07 Device for braking an object ejected from a transport container on a rope

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2020123181A RU2744901C1 (en) 2020-07-07 2020-07-07 Device for braking an object ejected from a transport container on a rope

Publications (1)

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RU2744901C1 true RU2744901C1 (en) 2021-03-17

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Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3268091A (en) * 1961-06-01 1966-08-23 Gen Mills Inc Reaction thrust operated manipulator
RU2088491C1 (en) * 1993-08-31 1997-08-27 Ракетно-космическая корпорация "Энергия" им.С.П.Королева Long-endurance manned orbital cable complex
US7503526B1 (en) * 2005-09-23 2009-03-17 Taylor Thomas C Space transportation node including tether system
RU2430861C1 (en) * 2010-03-04 2011-10-10 Федеральное государственное унитарное предприятие "Центральный научно-исследовательский институт машиностроения" (ФГУП ЦНИИмаш) Method of spaceship docking and device to this end
RU2521082C2 (en) * 2012-08-21 2014-06-27 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Омский государственный технический университет" Method for docking spacecrafts
RU2709070C1 (en) * 2019-03-11 2019-12-13 Федеральное государственное бюджетное образовательное учреждение высшего образования "Петербургский государственный университет путей сообщения Императора Александра I" Deployable orbital system

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3268091A (en) * 1961-06-01 1966-08-23 Gen Mills Inc Reaction thrust operated manipulator
RU2088491C1 (en) * 1993-08-31 1997-08-27 Ракетно-космическая корпорация "Энергия" им.С.П.Королева Long-endurance manned orbital cable complex
US7503526B1 (en) * 2005-09-23 2009-03-17 Taylor Thomas C Space transportation node including tether system
RU2430861C1 (en) * 2010-03-04 2011-10-10 Федеральное государственное унитарное предприятие "Центральный научно-исследовательский институт машиностроения" (ФГУП ЦНИИмаш) Method of spaceship docking and device to this end
RU2521082C2 (en) * 2012-08-21 2014-06-27 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Омский государственный технический университет" Method for docking spacecrafts
RU2709070C1 (en) * 2019-03-11 2019-12-13 Федеральное государственное бюджетное образовательное учреждение высшего образования "Петербургский государственный университет путей сообщения Императора Александра I" Deployable orbital system

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