CN216955124U - Inertia mechanism closed overload test tool - Google Patents

Inertia mechanism closed overload test tool Download PDF

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Publication number
CN216955124U
CN216955124U CN202220653245.4U CN202220653245U CN216955124U CN 216955124 U CN216955124 U CN 216955124U CN 202220653245 U CN202220653245 U CN 202220653245U CN 216955124 U CN216955124 U CN 216955124U
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China
Prior art keywords
connect
inertia mechanism
circuit board
centrifugal seat
overload test
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Active
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CN202220653245.4U
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Chinese (zh)
Inventor
王智焕
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Jiangxi Spark Military Industry Co ltd
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Jiangxi Spark Military Industry Co ltd
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Priority to CN202220653245.4U priority Critical patent/CN216955124U/en
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Abstract

The utility model provides a closed overload test tool for an inertia mechanism. Inertia mechanism closed overload test frock includes centrifugal seat and locates circuit board on the centrifugal seat, the concave at least one mounting groove that is equipped with of lateral part of centrifugal seat, set up the mounting hole that is used for installing inertia mechanism on the cell wall of mounting groove, be equipped with in the mounting groove and connect the electroplax and connect the electric plate, connect the electroplax to insert through the recess of its relative both sides and locate on the centrifugal seat, connect the electric plate one end with connect the electric plate to connect, connect the electric plate the other end with the circuit board is connected, be equipped with switch, signal lamp and portion of holding on the circuit board, the portion of holding has accommodated the plug screw. The inertia mechanism closed overload test tool is simple and reasonable in structure, convenient to operate, high in measurement efficiency, time-saving and labor-saving.

Description

Inertia mechanism closed overload test tool
Technical Field
The utility model relates to the field of military products, in particular to a closed overload test tool for an inertia mechanism.
Background
The inertia mechanism is assembled by an inertia spring, an inertia pin, an electric connecting sleeve and a screw plug, and is a common firing mode of the firearm. During the action of the firearm, under the action of the inertia force, the inertia pin is pressed forward to continuously compress the inertia spring, and when the inertia force is larger than the inertia mechanism and is closed and overloaded, the inertia pin is communicated with the circuit to fire the firearm. In the course of testing the product, it is necessary to ensure that the closing overload of the inertial mechanism is within a certain range, in order to ensure the operational reliability of the firearm. However, when testing the inertia mechanism in the past, most testers hold the load rod with hands to load the inertia mechanism, so that the operation of the testers is inconvenient, the error of the overload value tested by the inertia mechanism is large, and uncertain factors can be brought to subsequent use when the small or fully-sealed inertia mechanism cannot be tested, and the test is inaccurate or cannot be tested.
SUMMERY OF THE UTILITY MODEL
Based on the structure, the utility model provides a reliable and effective inertia mechanism closing overload test tool.
The utility model discloses a closed overload test tool for an inertia mechanism, which comprises a centrifugal seat and a circuit board arranged on the centrifugal seat, wherein at least one mounting groove is concavely arranged on the side part of the centrifugal seat, a mounting hole for mounting the inertia mechanism is formed in the wall of the mounting groove, an electric connection plate and an electric connection piece are arranged in the mounting groove, the electric connection plate is inserted on the centrifugal seat through grooves on two opposite sides of the electric connection plate, one end of the electric connection piece is connected with the electric connection plate, the other end of the electric connection piece is connected with the circuit board, a power switch, a signal lamp and an accommodating part are arranged on the circuit board, and a screw plug is accommodated in the accommodating part.
Furthermore, the number of the installation grooves is 6, and the 6 installation grooves are uniformly formed around the periphery of the centrifugal seat.
Furthermore, the power receiving piece comprises a first bending portion and a second bending portion, the first bending portion is connected with the circuit board, and the second bending portion is connected with the centrifugal seat.
Furthermore, the accommodating part is provided with an accommodating hole for installing the screw plug, and the accommodating hole penetrates through two opposite sides of the accommodating part.
Further, the circuit board is fixedly connected with the centrifugal seat through screws.
Further, the centrifugal seat is fixedly connected with the centrifugal machine through threads.
Further, the power switch and the signal lamp are welded on the circuit board.
The inertia mechanism closed overload testing tool is simple and reasonable in structure, convenient to operate, high in measuring efficiency, time-saving and labor-saving. Both can set up the centrifuge rotational speed according to inertia mechanism's closed overload scope to whether come the rapid judgement product to meet the requirements according to the condition of signal lamp, also can obtain clear inertia mechanism closure overload according to the condition of signal lamp again through adjusting the centrifuge rotational speed simultaneously.
Drawings
FIG. 1 is a schematic perspective view of an inertia mechanism closed overload test fixture according to the present invention;
fig. 2 is a schematic plan view of the inertia mechanism closing overload test fixture shown in fig. 1 from a perspective.
Description of reference numerals:
centrifugal seat 1, connect electric plate 2, connect electric plate 3, circuit board 4, signal lamp 5, plug screw 6, switch 7, mounting hole 11.
Detailed Description
To facilitate an understanding of the utility model, the utility model will now be described more fully with reference to the accompanying drawings. Preferred embodiments of the present invention are shown in the drawings. This invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete.
Referring to fig. 1 and 2, the utility model provides an inertia mechanism closed overload test tool, which includes a centrifugal seat 1 and a circuit board 4 arranged on the centrifugal seat, wherein at least one mounting groove is concavely arranged on a side portion of the centrifugal seat, a mounting hole 11 for mounting an inertia mechanism is formed in a wall of the mounting groove, an electric connection plate 3 and an electric connection piece 2 are arranged in the mounting groove, the electric connection plate is inserted into the centrifugal seat through grooves on two opposite sides of the electric connection plate, one end of the electric connection piece is connected with the electric connection plate, the other end of the electric connection piece is connected with the circuit board, a power switch 7, a signal lamp 5 and an accommodating portion are arranged on the circuit board 4, and a screw plug 6 is accommodated in the accommodating portion.
In one embodiment, the number of the installation grooves is 6, and the 6 installation grooves are uniformly arranged around the periphery of the centrifugal seat.
In one embodiment, the electric connecting piece comprises a first bending part and a second bending part, the first bending part is connected with the circuit board, and the second bending part is connected with the centrifugal seat.
In one embodiment, the accommodating portion has an accommodating hole for mounting the screw plug, and the accommodating hole penetrates through two opposite sides of the accommodating portion.
In one embodiment, the circuit board is fixedly connected with the centrifugal seat through screws.
In one embodiment, the centrifuge holder is fixedly connected to the centrifuge by means of a screw thread.
In one embodiment, the power switch and the signal lamp are soldered to the circuit board.
According to the inertia mechanism closed overload test tool, the position for installing the inertia mechanism is designed on the centrifugal seat, and the 6-shot inertia mechanism can be measured at the same time. When the centrifugal machine is used, the power switch is firstly turned on, then the centrifugal machine is started, the rotating speed is adjusted, and whether the closing overload value of the inertia mechanism meets the requirement or not is judged through the signal lamp. The tool is simple and reasonable in structure, convenient to operate, high in measuring efficiency, time-saving and labor-saving.
The working principle of the inertia mechanism closed overload testing tool is as follows: before working, the tool is directly installed on a centrifuge through threads, then 6 products to be tested are placed in a centrifuge seat at the position shown in figure 1, and then a power connection plate is inserted. At the moment, one level of the inertia mechanism is directly connected with the circuit board through the centrifugal seat, the other level of the inertia mechanism is connected with the power connection plate, and the power connection plate is connected with the circuit board through the power connection piece, so that two poles of the inertia mechanism are connected into the circuit. When the centrifugal machine works, a power switch is turned on firstly, then the centrifugal machine is started, when the preset rotating speed is reached, the inertia mechanism is closed under the action of centrifugal force, and a signal lamp is turned on, so that the product is qualified; if the preset rotating speed is reached, the signal lamp is not lighted, and the inertia mechanism is unqualified. The tool can judge whether the inertia mechanism is qualified or not, and can measure the exact closed overload of the inertia mechanism by adjusting the rotating speed. The device simple structure is reasonable, and the operation is safe convenient, labour saving and time saving, when by a wide margin improved detection efficiency, also improved greatly and detected the accuracy.
The inertia mechanism closed overload testing tool is simple and reasonable in structure, convenient to operate, high in measuring efficiency, time-saving and labor-saving. Both can set up the centrifuge rotational speed according to inertia mechanism's closed overload scope to whether come the rapid judgement product to meet the requirements according to the condition of signal lamp, also can obtain clear inertia mechanism closure overload according to the condition of signal lamp again through adjusting the centrifuge rotational speed simultaneously.
The above examples only express embodiments of the present invention, and the description thereof is more specific and detailed, but not construed as limiting the scope of the present invention. It should be noted that, for a person skilled in the art, several variations and modifications can be made without departing from the inventive concept, which falls within the scope of the present invention. Therefore, the protection scope of the present patent shall be subject to the appended claims.

Claims (7)

1. The utility model provides an inertia mechanism closure overload test frock which characterized in that: including centrifugal seat and locating circuit board on the centrifugal seat, the concave at least one mounting groove that is equipped with of lateral part of centrifugal seat, offer the mounting hole that is used for installing inertial mechanism on the cell wall of mounting groove, be equipped with in the mounting groove and connect the electroplax and connect the electric plate, connect the electroplax to insert through the recess of its relative both sides and locate on the centrifugal seat, connect the electric plate one end with connect the electric plate to connect, connect the electric plate the other end with the circuit board is connected, be equipped with switch, signal lamp and the portion of holding on the circuit board, it has the plug screw to hold in the portion of holding.
2. The inertia mechanism closed overload test tool of claim 1, wherein: the number of the installation grooves is 6, and the 6 installation grooves are uniformly arranged around the periphery of the centrifugal seat.
3. The inertia mechanism closed overload test tool of claim 2, wherein: the power receiving piece comprises a first bending portion and a second bending portion, the first bending portion is connected with the circuit board, and the second bending portion is connected with the centrifugal seat.
4. The inertia mechanism closed overload test tool of claim 3, wherein: the accommodating part is provided with an accommodating hole for installing the screw plug, and the accommodating hole penetrates through two opposite sides of the accommodating part.
5. The inertia mechanism closed overload test tool of claim 4, wherein: the circuit board is fixedly connected with the centrifugal seat through screws.
6. The inertia mechanism closed overload test tool of claim 5, wherein: the centrifugal seat is fixedly connected with the centrifugal machine through threads.
7. The inertia mechanism closed overload test tool of claim 6, wherein: the power switch and the signal lamp are welded on the circuit board.
CN202220653245.4U 2022-03-24 2022-03-24 Inertia mechanism closed overload test tool Active CN216955124U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202220653245.4U CN216955124U (en) 2022-03-24 2022-03-24 Inertia mechanism closed overload test tool

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202220653245.4U CN216955124U (en) 2022-03-24 2022-03-24 Inertia mechanism closed overload test tool

Publications (1)

Publication Number Publication Date
CN216955124U true CN216955124U (en) 2022-07-12

Family

ID=82297478

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202220653245.4U Active CN216955124U (en) 2022-03-24 2022-03-24 Inertia mechanism closed overload test tool

Country Status (1)

Country Link
CN (1) CN216955124U (en)

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