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RU1835060C - Impact machine for testing of units - Google Patents

Impact machine for testing of units

Info

Publication number
RU1835060C
RU1835060C SU914935445A SU4935445A RU1835060C RU 1835060 C RU1835060 C RU 1835060C SU 914935445 A SU914935445 A SU 914935445A SU 4935445 A SU4935445 A SU 4935445A RU 1835060 C RU1835060 C RU 1835060C
Authority
RU
Russia
Prior art keywords
piston
striker
levers
barrel
cavity
Prior art date
Application number
SU914935445A
Other languages
Russian (ru)
Inventor
Вадим Дмитриевич Степанов
Original Assignee
Всесоюзный научно-исследовательский институт технической физики
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 Всесоюзный научно-исследовательский институт технической физики filed Critical Всесоюзный научно-исследовательский институт технической физики
Priority to SU914935445A priority Critical patent/RU1835060C/en
Application granted granted Critical
Publication of RU1835060C publication Critical patent/RU1835060C/en

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Landscapes

  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)

Abstract

Сущность: поршень-боек 5, разгон емый в стволе 1 давлением сжатого газа в предпоршневой полости ствола, удерживаетс  в исходном положении пусковым механизмом . Последний включает соединенный с поршнем-бойком центральный шток 11, который размещен в предпоршневой полости и имеет выступ 12 на свободном конце, соединенные с тыльной крышкой 2 ствола рычаги 15с ответными выступами-захватами 16 и охватывающий рычаги кольцеобразный поршень 17, при воздействии которого на рычаги выступы-захваты сцепл ютс - расцепл ютс  с выступом штока. Привод перемещени  поршн  17 может быть выполнен в виде двухполостного пневмоцилиндра 18, установленного на внешней стороне тыльной крышки. Разогнанный поршень-боек сообщает импульс поршню 3 с испытуемым изделием 4 через воздушный упругий элемент. 1 з.п, ф-лы, 1 ил.SUBSTANCE: piston-striker 5, accelerated in the barrel 1 by the pressure of compressed gas in the pre-piston cavity of the barrel, is held in its initial position by the trigger mechanism. The latter includes a central rod 11 connected to the piston-striker, which is located in the pre-piston cavity and has a protrusion 12 at its free end, levers 15 with mating arms 16 connected to the rear cover 2 of the barrel, and an annular piston 17 surrounding the levers, when exposed to the levers the grips engage — disengage from the stem protrusion. The actuator for moving the piston 17 may be in the form of a two-cavity pneumatic cylinder 18 mounted on the outside of the back cover. The overclocked piston-striker sends an impulse to the piston 3 with the test product 4 through an air elastic element. 1 s.p., f-ly, 1 ill.

SU914935445A 1991-05-12 1991-05-12 Impact machine for testing of units RU1835060C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU914935445A RU1835060C (en) 1991-05-12 1991-05-12 Impact machine for testing of units

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU914935445A RU1835060C (en) 1991-05-12 1991-05-12 Impact machine for testing of units

Publications (1)

Publication Number Publication Date
RU1835060C true RU1835060C (en) 1993-08-15

Family

ID=21574094

Family Applications (1)

Application Number Title Priority Date Filing Date
SU914935445A RU1835060C (en) 1991-05-12 1991-05-12 Impact machine for testing of units

Country Status (1)

Country Link
RU (1) RU1835060C (en)

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
Авторское свидетельство СССР № 1208488, кл. G 01 М 7/08, 1983. Авторское свидетельство СССР № 1295252, кл. G 01 М 7/08, 1985. *

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