FIELD: safety devices.
SUBSTANCE: invention relates to safety devices in the detonation circuit and can be used in the design of automation devices. The activation means contains a housing with longitudinal parallel holes, in which a follower mechanism and a safety mechanism with an impact mechanism and an initiating charge are located. The longitudinal parallel holes of the body are separated by a partition with a channel in which a ball locking safety mechanism is installed, and the follower is designed to unlock the safety mechanism and contains a spring-loaded rod protruding with its free end outside the body and equipped with a groove for interaction with the locking ball. The activating device is equipped with a control mechanism and a fixing element. A groove is made on the follower rod, and additional longitudinal parallel and transverse holes are made in the body. An additional longitudinal parallel opening is separated from the housing opening, in which the follower is installed, by a wall with a through channel and communicated with the transverse opening of the housing, in which the locking element is located. The control mechanism is installed in an additional opening of the body and is made in the form of a spring-loaded rod protruding with its free end outside the body, and spring-loaded stoppers located in the through channel of the body wall. On the rod of the control mechanism from the side of the free end, grooves are made for interaction with the fixing element and one of the stoppers, the other of which interacts with the rod of the follower in the region of the groove.
EFFECT: increasing resistance to vibration and ease of use.
1 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
FUSE | 2001 |
|
RU2228514C2 |
BASE FUSE | 2005 |
|
RU2285893C1 |
NOSE FUSE | 2009 |
|
RU2412426C1 |
SAFE-AND-ACTUATE MECHANISM OF MISSILE WARHEAD | 2007 |
|
RU2380653C2 |
SAFETY-TYPE INITIATOR FOR DETONATION SEPARATION SYSTEMS OF SPACE VEHICLES | 2021 |
|
RU2760863C1 |
DETONATION DEVICE FOR CONNECTION AND SUBSEQUENT SEPARATION OF ROCKET AND SPACECRAFT STRUCTURE ELEMENTS | 2019 |
|
RU2729494C1 |
ROTARY IMPACT MECHANISM | 0 |
|
SU969511A1 |
NOSE FUSE | 2009 |
|
RU2422764C1 |
NOSE PERCUSSION FUSE | 2002 |
|
RU2211437C1 |
SAFETY-LAUNCHING DEVICE OF THE ON-BOARD EARTH-BASED AUTOMATION DETONATION CIRCUIT | 2015 |
|
RU2625660C2 |
Authors
Dates
2021-12-28—Published
2021-05-21—Filed