CN213363560U - Novel fire engine locking force detection device - Google Patents

Novel fire engine locking force detection device Download PDF

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Publication number
CN213363560U
CN213363560U CN202021646157.9U CN202021646157U CN213363560U CN 213363560 U CN213363560 U CN 213363560U CN 202021646157 U CN202021646157 U CN 202021646157U CN 213363560 U CN213363560 U CN 213363560U
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force
locking
unit
force measurement
support body
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CN202021646157.9U
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裴晓龙
刘晓芹
孙放
王宏宇
张君
董泽委
刘秀
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ARMY AVIATION INSTITUTE PLA
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ARMY AVIATION INSTITUTE PLA
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Abstract

The utility model provides a novel fire engine locking force detection device, which comprises a force application unit, a force measurement unit and a recording display unit, wherein the force measurement unit comprises a support body, a transmission rod, a mechanical sensor, a guide rod and a force measurement slider; the force measuring slide block is used for being matched with the conductive locking component in the transmitting tube; the force application unit is connected with the head of the force measurement unit, drives the force measurement unit to move towards the nozzle of the emission tube, and pulls and releases the force measurement unit from the conductive locking component; the recording and displaying unit is used for displaying, recording and storing the locking force data. The utility model discloses the device breaks away from electrically conductive shutting subassembly through simulation rocket projectile transmission, detects the fire ware locking force, has solved the unable realistic problem who detects and adjust of fire ware locking force, has guaranteed shooting security and shooting precision, and detection device uses in a flexible way, efficient.

Description

Novel fire engine locking force detection device
Technical Field
The utility model belongs to the technical field of the mechanical force detects, in particular to novel fire ware locking force detects device.
Background
The launcher is hung on a universal weapon hanger below a helicopter short wing, can safely and reliably carry a plurality of aviation rocket projectiles through the launching tube, realizes the transmission of an ignition signal and an opening time signal according to a fire control system instruction, gives the rocket projectiles initial shooting and muzzle speed, and realizes single-shot and continuous-shot launching at a certain launching interval and a certain launching sequence. After the rocket projectile is ignited in the rocket launcher, only when the gas thrust of the engine reaches a certain value, the rocket projectile can break loose from the locking of the conductive locking component at the tail part of the launching tube of the rocket launcher and fly forwards, and the resistance of the conductive locking component on the rocket projectile from rest to movement is the locking force. The locking force is a value interval and is not a fixed value. Too little latching force may cause "blow out" and too much latching force may cause "finish blasting".
Even when the locking force is within a specified allowable range, the initial disturbance and the flight starting force caused by the inconsistency of the locking forces of the plurality of launch tubes have a large influence on the shooting accuracy. Assuming that the locking force of each launch tube is between a specified maximum and minimum (the range difference is up to several hundred N), the initial force and initial flight conditions achieved by the projectile are not consistent due to the inconsistent locking forces of the plurality of launch tubes, and the projectile may fly out of normal trajectory with greater projectile spread. The reasons are two: one is the increased projectile spread due to initial disturbances caused by uneven latching forces. Factors influencing the shooting accuracy of the rocket projectile are many, such as initial shooting calculated by a fire control system, initial disturbance of the rocket projectile, uneven burning of gunpowder, inconsistent center of mass of the projectile body, high-altitude wind and the like. The initial disturbance refers to random vibration generated by the external influences of gas flow, forward firing on follow-up firing, locking force and the like on the launching tube during launching, and the locking force is a sudden load for the igniter, is a main part of external force for generating random vibration and is also an important factor for causing dispersion. When multiple tubes are fired simultaneously, the reaction force borne by the launching tube with the maximum locking force is the largest, the vibration of the igniter is the largest, and the initial disturbance is the largest; the launch tube with the lowest latching force experiences the least reaction force, the minimum shock to the initiator and the minimum initial disturbance. The effect of the two extreme latching forces necessarily results in a change in the initial launch of the projectile and an increase in the spread of the projectile. Second, projectile dispersion is increased due to inconsistent initial velocity of the projectile caused by the latching force. When the locking force is close to the minimum value, the initial speed of the rocket projectile is reduced, the initial flight angle is reduced due to the influence of gravity at the moment of separating from the launching tube, and a near projectile is generated; the other possibility is that the rocket projectile is ignited and then rapidly discharged after overcoming the smaller locking force due to the small locking force, so that the consumption of gunpowder for overcoming the locking force is less, the subsequent acceleration time is prolonged, and the long projectile is generated; when the locking force is close to the maximum value, the initial speed of the rocket projectile is increased, the initial flight angle is increased, and a long projectile is generated; there is also a possibility that the rocket projectile needs to overcome a larger locking force after ignition to slowly discharge, so that the gunpowder is consumed to overcome the locking force, the subsequent acceleration time is short, and the near projectile is generated. These two extremes necessarily result in a large spread of projectiles.
To minimize the effects of initial disturbances and initial velocity inconsistencies, to maximize the uniformity of latching forces, and to minimize projectile spread, the conductive latch assembly latching force uniformity needs to be detected and adjusted. The existing special device for detecting the locking force of the igniter is lack, the locking force is inconsistent after the igniter is used for many times, the locking force condition of the igniter cannot be flexibly and simply obtained, and the problems of large projectile spreading surface, low shooting precision and the like are often caused.
SUMMERY OF THE UTILITY MODEL
In order to overcome the not enough among the prior art, the inventor has carried out the research of keen interest, provides a novel fire ware locking force detection device, breaks away from electrically conductive shutting subassembly through simulation rocket projectile transmission and detects fire ware locking force, has solved the realistic problem that fire ware locking force can't detect and adjust, has guaranteed shooting security and shooting precision, and detection device uses in a flexible way, and is efficient to accomplish the utility model discloses.
The utility model provides a technical scheme as follows:
a novel fire extinguisher locking force detection device, comprising: the force application unit, the force measurement unit and the recording and displaying unit are arranged, wherein the force measurement unit comprises a support body, a transmission rod, a mechanical sensor, a guide rod and a force measurement sliding block, the support body is of a long columnar structure, the outer diameter of the support body is not larger than the inner diameter of the emission tube, the force measurement sliding block is fixed at the tail of the support body, the mechanical sensor is arranged in the support body, and two ends of the mechanical sensor are respectively connected and fixed to the support body and the force measurement sliding block through the; the force measuring slide block is positioned at the tail end of the force measuring unit, is provided with a ring groove matched with the protruding structure on the conductive locking component and is used for being matched with the conductive locking component in the transmitting tube so as to ensure that the conductive locking component locks and limits the force measuring unit;
the force application unit is connected with the head of the force measurement unit, drives the force measurement unit to move towards the nozzle of the emission tube, and pulls and releases the force measurement unit from the conductive locking component;
the recording and displaying unit comprises a peak value holding instrument which is connected with the mechanical sensor through a lead and used for receiving the signal output by the mechanical sensor and converting the signal into locking force data to be displayed, recorded and stored.
According to the utility model provides a pair of novel fire engine locking force detection device has following beneficial effect:
the utility model discloses well fire engine blocking force detection device, through the structural design of application of force unit, can realize the reliable steady removal of force measuring mechanism in the fire engine, through the structural design of force measuring unit, can realize the detection of blocking force, the device has solved the realistic problem that fire engine blocking force can't detect and adjust, has guaranteed shooting security and shooting precision, and detection device uses in a flexible way, and is efficient, is suitable for using widely.
Drawings
FIG. 1 is a schematic structural diagram of a locking force detection device of a fire engine;
FIG. 2 is a schematic view of a latching force detecting device in a loaded position;
FIG. 3 is a schematic view of a force-measuring slide fully released configuration of the latching force detection device;
description of the reference numerals
11-support body, 12-transmission rod, 13-mechanical sensor, 14-guide rod, 15-force measuring slider, 16-bearing, 21-hand wheel, 22-screw rod, 23-front baffle, 231-guide tube, 31-peak value holding instrument, 32-lead and 41-emission tube.
Detailed Description
The features and advantages of the present invention will become more apparent and appreciated from the following detailed description of the invention.
The utility model provides a novel fire engine locking force detection device, as shown in figure 1, including force application unit, dynamometry unit and record display element, wherein, the dynamometry unit includes supporter 11, transfer line 12, mechanics sensor 13, guide arm 14 and dynamometry slider 15, supporter 11 is long column structure, the external diameter is not more than the internal diameter of launching tube 41, the afterbody of supporter 11 is fixed with dynamometry slider 15, the internally mounted of supporter 11 has mechanics sensor 13, the both ends of mechanics sensor 13 are connected through transfer line 12 and guide arm 14 respectively and are fixed to supporter 11 and dynamometry slider 15; the force measuring slider 15 is positioned at the tail end of the force measuring unit, simulates an annular ignition device at the tail part of a rocket projectile, is provided with an annular groove matched with a protruding structure such as a clamping jaw on the conductive locking component, and is used for being matched with the conductive locking component in the transmitting tube 41 to ensure that the conductive locking component locks and limits the force measuring unit;
the force application unit is connected with the head of the force measurement unit, drives the force measurement unit to move towards the pipe orifice of the launching pipe 41, and pulls and releases the force measurement unit from the conductive locking component;
the recording and displaying unit comprises a peak value holding instrument 31 which is connected with the mechanical sensor 13 through a lead 32, receives the signal output by the mechanical sensor 13 and converts the signal into locking force data for displaying, recording and storing.
In a preferred embodiment of the present invention, the mechanical sensor 13 is a resistance strain gauge sensor.
The utility model relates to an in the preferred embodiment, supporter 11 is inside to have hollow structure, and the hollow structure at the position of mechanics sensor 13 place plays the effect that holds, and the hollow structure at other positions plays the effect that subtracts heavy to improve the convenience in use of device.
The utility model relates to an in the preferred embodiment, the dynamometry unit still includes the bearing 16 of head terminal surface center installation, and force application unit drives the dynamometry unit through cooperating with bearing 16 and breaks away from electrically conductive shutting subassembly.
In a preferred embodiment of the present invention, the force applying unit includes a handwheel 21, a screw 22 and a front baffle 23, a limiting structure is processed on a side plate surface of the front baffle 23, the front baffle 23 is clamped at the pipe orifice of the launching tube 41 through the limiting structure, a guiding tube 231 is processed at the center of the front baffle 23, and an internal thread structure is formed inside the guiding tube 231; one end of the screw 22 is fixed on the hand wheel 21, and the other end of the screw passes through the guide tube 231 and then is fixedly connected with the bearing 16 at the front end of the support body 11, and under the driving of the hand wheel 21, the screw 22 rotates to drive the force measuring unit to axially displace and separate from the conductive locking component.
Furthermore, the limiting structure on the front baffle 23 is an annular boss, and the outer edge of the boss is matched with the inner edge of the nozzle of the launching tube of the igniter, i.e. the structure is the same and the size is equivalent.
Furthermore, the limiting structure on the front baffle 23 is an annular groove matched with the opening of the transmitting tube, and the opening of the transmitting tube enters the annular groove to realize limiting.
In a preferred embodiment of the present invention, the recording and displaying unit middle wire 32 is led out from the end of the force measuring unit and connected to the peak value holding instrument 31.
The utility model discloses in, this locking power detection device is a whole, and by the firing ware front end load target in place (this step is similar with rocket projectile loading method), dynamometry slider is blocked by electrically conductive shutting subassembly, can not remove, sees figure 2.
During force measurement, a hand wheel is rotated, a tension force is formed by the screw and the front baffle, and the force measurement unit is pulled to move forwards integrally. When the force measuring mechanism moves forward for a certain distance, the claws of the conductive locking component completely release the locking of the force measuring slide block, and the hand wheel stops rotating, as shown in figure 3.
And recording and processing the test parameters by a mechanical sensor and a peak value holding instrument so as to obtain the locking force value of the igniter.
The present invention has been described in detail with reference to the specific embodiments and the exemplary embodiments, but the description should not be construed as limiting the present invention. Those skilled in the art will appreciate that various equivalent substitutions, modifications or improvements may be made to the technical solution of the present invention and embodiments thereof without departing from the spirit and scope of the present invention, and all fall within the scope of the present invention. The protection scope of the present invention is subject to the appended claims.
The details of the present invention not described in detail in the specification are well known to those skilled in the art.

Claims (8)

1. The novel fire engine locking force detection device is characterized by comprising a force application unit, a force measurement unit and a recording display unit, wherein the force measurement unit comprises a support body (11), a transmission rod (12), a mechanical sensor (13), a guide rod (14) and a force measurement sliding block (15), the support body (11) is of a long columnar structure, the outer diameter of the support body is not larger than the inner diameter of a transmitting tube (41), the force measurement sliding block (15) is fixed at the tail of the support body (11), the mechanical sensor (13) is installed inside the support body (11), and two ends of the mechanical sensor (13) are respectively connected and fixed to the support body (11) and the force measurement sliding block (15) through the transmission rod (12) and the guide rod (14); the force measuring slide block (15) is positioned at the tail end of the force measuring unit, is provided with a ring groove matched with the protruding structure on the conductive locking component and is used for being matched with the conductive locking component in the transmitting tube (41) to ensure that the conductive locking component locks and limits the force measuring unit;
the force application unit is connected with the head of the force measurement unit, drives the force measurement unit to move towards the pipe orifice of the emission pipe (41), and pulls and releases the force measurement unit from the conductive locking component;
the recording and displaying unit comprises a peak value holding instrument (31) which is connected with the mechanical sensor (13) through a lead (32) and receives the signal output by the mechanical sensor (13) and converts the signal into locking force data for displaying, recording and storing.
2. The fire extinguisher locking force detection device according to claim 1, characterized in that the mechanical sensor (13) is a resistance strain gauge sensor.
3. The fire extinguisher locking force detecting device according to claim 1, characterized in that the inside of the supporting body (11) has a hollow structure.
4. The device for detecting locking force of fire fighting equipment according to claim 1, characterized in that the force-measuring unit further comprises a bearing (16) centrally mounted on the head end face, and the force-applying unit is adapted to move the force-measuring unit away from the conductive locking member by engaging with the bearing (16).
5. The device for detecting the locking force of the fire engine according to claim 4, wherein the force application unit comprises a hand wheel (21), a screw rod (22) and a front baffle plate (23), a limiting structure is processed on one side plate surface of the front baffle plate (23) and used for clamping the front baffle plate (23) at the nozzle of the launching tube (41), a guide tube (231) is processed in the center of the front baffle plate (23), and an internal thread structure is formed inside the guide tube (231); one end of the screw rod (22) is fixed on the hand wheel (21), and the other end of the screw rod passes through the guide pipe (231) and then is fixedly connected with the bearing (16) at the front end of the support body (11).
6. The device for detecting the locking force of the igniter as claimed in claim 5, wherein the limiting structure on the front baffle plate (23) is an annular boss, and the outer edge of the boss is matched with the inner edge of the opening of the firing tube of the igniter.
7. The device for detecting locking force of fire extinguisher according to claim 5, characterized in that the limit structure on the front baffle plate (23) is an annular groove which is matched with the mouth of the firing tube.
8. The device for detecting locking force of fire engine according to claim 1, characterized in that the recording and displaying unit is provided with a lead wire (32) which is led out from the tail of the force measuring unit and is connected with the peak holding instrument (31).
CN202021646157.9U 2020-08-10 2020-08-10 Novel fire engine locking force detection device Active CN213363560U (en)

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Application Number Priority Date Filing Date Title
CN202021646157.9U CN213363560U (en) 2020-08-10 2020-08-10 Novel fire engine locking force detection device

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Application Number Priority Date Filing Date Title
CN202021646157.9U CN213363560U (en) 2020-08-10 2020-08-10 Novel fire engine locking force detection device

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CN213363560U true CN213363560U (en) 2021-06-04

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113739630A (en) * 2021-09-26 2021-12-03 合肥君信电子科技有限公司 Dual-purpose artillery locking body detection device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113739630A (en) * 2021-09-26 2021-12-03 合肥君信电子科技有限公司 Dual-purpose artillery locking body detection device

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