KR20170049883A - In-situ Performance Test Equipment for Pyrotechnic Mechanical Device under High Gas Pressure and Operation Method thereof - Google Patents

Abstract

The pneumatic device 100 of the present invention is capable of in-situ measurement of the operating performance of the activated type pyro apparatus 4, in which the gunpowder is aerated under a high pressure (~ 4,000 psig) The operation performance of the deactivation type pyro apparatus 4 in which the pyrolysis of the gunpowder is not performed by using the pyro valve 3 that transfers the air pressure of the pyrolysis apparatus 4 to the pyro apparatus 4, Can be measured in place. Therefore, the pneumatic device 100 is characterized in that the pneumatic performance test of various piro devices can be performed in-situ efficiently while the leakage pressure per second is precisely measured through the stabilization of the measurement system.

Description

Technical Field [0001] The present invention relates to a pneumatic device and a test method for testing the performance of a pyro apparatus in place,

The present invention relates to a pneumatic device for performance testing of a pyro apparatus, and more particularly to a pneumatic apparatus and a test method for testing the performance of a pyro apparatus in situ.

In general, a pyro-device is a device that converts the gas pressure released by a gunpowder within a pressure cartridge into a kinetic kinetic energy such as a piston motion.

Unlike electric devices, it has a simple structure, small size and light weight, and is widely used for guided weapons and aerospace.

Therefore, the pyro apparatus must have a very high operating reliability and, due to the nature of the application system, it must be kept airtight before and after operation even in adverse conditions such as high pressure air pressure.

Because of this, pyrolytic apparatus should perform pneumatic performance test. Especially, pneumatic performance test of single-use pyrolytic apparatus is very important.

Equipment for pneumatic performance testing of pyro-devices is pneumatic and air-tightness inspection equipment. The pneumatic device is capable of verifying the mechanical motion performance of the pyro apparatus by precisely applying pressure by rupturing the rupture disk with the pneumatic pressure taking into account the release gas pressure of the pressure cartridge having an error of +/- 15% do. The airtightness checking device measures the airtightness performance by separating the pneumatic device from the pneumatic device operated by the pneumatic device and then reconnecting to the fitting portion of the airtight portion of the pneumatic device.

Korean Patent Publication No. 10-2010-0000774 (Jan. 06, 2010)

However, since the equipment for pneumatic performance test of the pyro apparatus is divided into the pneumatic apparatus and the hermetic check apparatus, the time required for connection and separation of the pneumatic apparatus and the hermetic check apparatus is inevitably large.

In particular, the rupture disk has the drawback that it is difficult for the tester to rupture at the correct pressure value and point of view desired. In addition, by reconnecting the air-tightness inspection device after the air-pressure device is disconnected, there is a high risk that the fitting portion of the air-tight portion of the pyro-device will be damaged, and if the fitting is damaged, the retest must be performed with another pyrode device, resulting in waste of time and cost none.

Thus, conventional pneumatic devices do not have a quantitative airtightness measuring device for pyrogenic devices, and in particular, there is no specialized pneumatic device capable of performing pneumatic testing of a pyrogenic device in situ.

In view of the above, the present invention can precisely measure the leakage pressure per second through the stabilization of the measuring system while the pneumatic performance test of various piro devices can be efficiently performed in-situ, It is an object of the present invention to provide a pneumatic device and a test method for performing a performance test of a pyro apparatus in place in which a high pressure air pressure can be applied to the pyro apparatus within 0.5 ms instead of the pressure cartridge of the apparatus.

To achieve these and other advantages and in accordance with the purpose of the present invention, as embodied and broadly described herein, there is provided a pneumatic device comprising: a compressor for generating a high pressure gas and storing the compressed gas in a compressed gas tank; A pyro apparatus connected to the compressed gas tank and connected between a main supply line through which the high pressure gas stored in the compressed gas tank flows and a main discharge line through which the high pressure gas is discharged to the atmosphere and in which the pneumatic pressure of the high pressure gas directly acts; A pyro valve connected between a sub supply line branching from the main supply line and a sub connection line connected to the pyro apparatus, the pneumatic valve directly acting on the pneumatic pressure of the high pressure gas; An airtight container provided between the auxiliary return line branched from the sub connection line and the auxiliary supply line leading to the main supply line to provide a volume increasing space; A sensor unit measuring the pressure of the high-pressure gas flowing through the main supply line, the main discharge line and the sub-supply line, and measuring a pressure of the high-pressure gas caught in the sealed vessel; A valve unit for opening / closing a flow path of the charging line, the main supply line, the main discharge line, the sub supply line, and the sub connection line; A regulator unit for regulating a pneumatic pressure of the main supply line and the sub supply line; .

In a preferred embodiment, the pyrovalve includes a pressure cartridge which is burned when ignited and releases a gas pressure, a piston which moves by the gas pressure, and a flow pipe which opens the flow passage through which the high pressure gas passes. The pyro apparatus includes an axial flow pipe to which the main supply line is connected, and a circumferential flow pipe to which the main discharge line is connected.

In a preferred embodiment, the sensor unit comprises an axial pressure measuring sensor for measuring a pneumatic pressure applied to the main supply line, a circumferential pressure measuring sensor for measuring a pneumatic pressure applied to the main discharge line, A closed vessel pressure measuring sensor, and a valve pressure measuring sensor for measuring the air pressure applied to the sub supply line.

In a preferred embodiment, the valve unit comprises a compressor valve for opening and closing the flow passage of the filling line, a regulation valve for regulating the pneumatic pressure of the main supply line, a pair of first and second A main supply line main valve, a sub supply line main valve for opening and closing the flow passage of the sub supply line, an auxiliary supply line valve for opening and closing the flow passage of the auxiliary supply line, an auxiliary return line for opening / closing the flow passage of the auxiliary return line, A main discharge line valve for opening and closing the flow passage of the main discharge line, a first and a second vent valves for opening and closing the main discharge line in communication with the atmosphere, a third vent valve for opening and closing the sub- And a fourth vent valve that opens and closes the sub connection line to communicate with the atmosphere.

In a preferred embodiment, the regulator unit comprises a sub-regulator for regulating the pneumatic pressure of the sub-supply line, and a main regulator for regulating the pneumatic pressure of the main supply line.

As a preferred embodiment, software for testing the operating performance of the pyro apparatus and the airtightness before and after the operation of the compressor, the use of the detection value of the sensor unit, and the operation control of the valve unit and the regulator unit are carried out under high pressure Lt; / RTI >computer; The pyrolysis of the pyrolytic valve and the pyrolytic device is performed with a pyroarrator.

In order to accomplish the above object, there is provided a pyro apparatus performance testing method of the present invention, comprising: (A) when a high pressure gas generated by a compressor is stored in a compressed gas tank, a pyro apparatus pneumatic circuit A pneumatic device setting step in which atmospheric pressure formation of a pyro valve pneumatic circuit in which a valve is installed, and a reset of the pyro apparatus pneumatic circuit and the pneumatic pressure detection value of the pyro valve pneumatic circuit to 0 (zero) are performed by a computer; (B) an active type pyro apparatus in which the pyro apparatus is sputtered or an inert type pyro apparatus in which no sprocket is made, and in the case of the active type pyro apparatus, the pyro valve pneumatic circuit Performing a pressure performance test in which pressure is measured by applying a high pressure to the pyro apparatus without being closed in the case of the inactive type pyro apparatus; (C) after the pressure performance measurement has ended with a pressure performance measurement time elapse, the computer is closed with the pressure of the pyro apparatus pneumatic circuit and the pyro valve pneumatic circuit with reset to 0 psig, To perform the airtightness performance test by observing the pressure measurement and the pressure change during the measurement of the airtightness performance; (D) a closed container provided in the pyro apparatus pneumatic circuit for increasing the measurement volume of the pyro apparatus pneumatic circuit when the leakage amount of the pyro apparatus is increased during the measurement of the airtightness performance, step; As shown in FIG.

In a preferred embodiment, the high pressure is below 4,000 psig and the computer measures the pneumatic detection value in psig.

As a preferred embodiment, the active pyro apparatus test is performed by measuring the axial and circumferential pressures of the pyro apparatus after the pyro apparatus is aerated, and the active pyro apparatus test is performed After pyrolyzing the pyro valve, the axial pressure and circumferential pressure of the pyro apparatus are measured to measure the pressure performance.

In a preferred embodiment, the pressure performance measurement time lapse is one minute, and the airtight performance measurement time is several minutes.

In a preferred embodiment, the measurement volume increase is 40 cc.

The present invention can perform quantitative performance and leak testing related to pneumatic pressure of a pyro apparatus applied to an inorganic system without substantial time and expense in place.

In addition, the present invention has the effect of performing a quantitative performance and leakage test related to pneumatic pressure in place, without requiring a large time and cost, as well as a pyro apparatus which has been applied to existing weapon systems.

FIG. 1 is a configuration diagram of a pneumatic apparatus for performing a performance test of a pyro apparatus in place according to the present invention, FIG. 2 is a configuration diagram of a pyro valve for a performance test of an inactive pyro apparatus according to the present invention, Fig. 4 is a flow chart of a method for testing the performance of a pyro apparatus in situ according to the present invention, and Fig. 5 is a flowchart illustrating a method of testing the performance of a pyro apparatus by a pneumatic apparatus according to the present invention FIG. 6 is a state of operation of the pyro apparatus in the pneumatic apparatus according to the present invention, FIG. 7 is a state of testing the performance of the inert pyro apparatus by the pneumatic apparatus according to the present invention, and FIG. Fig. 9 is an example of airtightness test data before and after the operation of the pyro apparatus which has been tested with the pneumatic apparatus according to the present invention, and Fig. 10 shows an example of the air- This is an example of the airtightness test data after the operation of the pyroelectric device tested.

Hereinafter, exemplary embodiments of the present invention will be described in detail with reference to the accompanying drawings, which illustrate exemplary embodiments of the present invention. The present invention is not limited to these embodiments.

1 shows a pneumatic device configuration for a pyrotechnic device performance test in situ according to the present embodiment.

As shown, the pneumatic device 100 includes a compressor 1, a compressed gas tank 2, a pyrovalve 3, a pyrodevice 4, a hermetically sealed container 5, sensor units 6, 9, the valve units 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, the regulator units 22, 23, the pneumatic circuits 100-1, And the pneumatic performance test of the pyro apparatus 4 is carried out in conjunction with the computer 200 and the pyrolysis apparatus 300 is connected to the pyro valve 3 and the pyro apparatus 4, .

Specifically, the compressor (1) is associated with a compressed gas tank (2) which generates a high pressure gas and stores the generated high pressure gas. The compressed gas tank (2) stores the high-pressure gas generated in the compressor (1). The closed vessel 5 can attenuate noise that can be put on the pressure signal by external vibration or the like by enlarging the measurement volume (for example, 40 cc), and the leak time per hour can be more accurately measured by increasing the measurement time. The pilot valve 3 is used for pneumatic control when testing the piston operating performance of the inactive pyrolyzer (in the disengaged state) using pneumatic instead of pressure cartridge. The pyro apparatus 4 is a measurement object for measuring the operating performance and the airtightness before and after the operation under the high pressure air pressure in place.

Specifically, the sensor unit 6, 7, 8, 9 measures the pressure value inside the pneumatic circuit in psig, and the measured pressure value is transmitted to the measurement software. The measurement software can be installed in the computer 200 have. For example, the sensor units 6, 7, 8, and 9 may include an axial pressure measuring sensor 6 for measuring a high pressure (~ 4,000 psig) caught by a flow pipe in the piston direction of the pyro apparatus 4, A circumferential pressure measurement sensor 7 for measuring a high pressure (~ 4,000 psig) caught by the flow pipe on the side of the device 4, a closed container pressure measurement sensor 8 for measuring the internal pressure of the closed container 5, And a pirovalve pressure measurement sensor 9 for measuring the pressure applied to the valve 3 by the pressure sensor.

Specifically, the valve units 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21 are designed so that the pyro apparatus 4 is operable under high pressure, The pneumatic circuit is formed at atmospheric pressure and high pressure so that it can be measured in place.

For example, the valve units 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20 and 21 are connected to the high- (4,000 psig) applied to the flow pipe in the direction of the piston of the pyro apparatus (4) is controlled by the compressor valve (10) for opening and closing the pressure vessel, the regulation valve (11) A main supply line main valve 12 and a main supply line main valve 13 for controlling a pneumatic pressure to enter the pyro valve 3, 4 and an auxiliary supply line valve 15 for connecting the flow pipe in the piston direction of the pyrolysis apparatus 4 to the closed vessel 5 and the pyro apparatus (not shown) so as to further increase the measurement volume by 40 cc when the pressure leakage amount of the pyro apparatus 4 becomes large. An auxiliary return line valve 16 for connecting the flow pipe on the side of the pyro apparatus 4, a main discharge line valve 16 for discharging pneumatic pressure from the flow pipe on the side of the pyro apparatus 4 to the atmosphere, First and second vent valves 18 and 19 for discharging pneumatic pressure from a flow path pipe on the side of the pyro apparatus 4 to the atmosphere and pneumatic pressures entering the pyro valve 3 to the atmosphere A third vent valve 20 and a fourth vent valve 21 for discharging the air pressure entering the pyro apparatus 4 from the pyro valve 3 to the atmosphere.

Specifically, the regulator units 22 and 23 include a sub-regulator 22 for regulating the pneumatic pressure to enter the pilot valve 3, a main regulator 22 for regulating the pneumatic pressure entering the flow pipe in the piston direction of the pyro apparatus 4, (23).

Specifically, the pneumatic circuits 100-1 and 100-2 include a pyrolytic pneumatic circuit 100-1 for connecting the compressed gas tank 2 with the pyroelectric device 4 and the hermetically sealed container 5, And a pilot valve pneumatic circuit 100-2 for connecting the pilot valve 2 and the pilot valve 3 to each other.

For example, the pyro apparatus pneumatic circuit 100-1 includes a charging line a, a main supply line b, a main discharge line c, an auxiliary supply line d-1, an auxiliary return line d- 2). The charging line (a) connects the compressor (1) and the compressed gas tank (2), and the flow passage is opened and closed by the compressor valve (10). The main supply line b connects the compressed gas tank 2 and the flow path pipe in the piston direction of the pyro apparatus 4 and the pressure is regulated by the regulation valve 11 and the main regulator 23, , The flow passage is opened and closed by the two main supply line main valves (12, 14), and the air pressure is detected by the axial pressure measurement sensor (6). The main discharge line c is connected to the main supply line b from the flow pipe on the side of the pyro apparatus 4 and the flow passage is opened and closed by the main discharge line valve 17, (18, 19), and the pneumatic pressure is detected by the circumferential pressure measuring sensor (7). The auxiliary supply line d-1 is connected to the closed vessel 5 in which the internal pressure is measured by the main supply line b and the closed vessel pressure measurement sensor 8, Respectively. The auxiliary return line (d-2) connects the main discharge line (c) to the closed vessel (5), and the flow passage is opened and closed by the auxiliary return line valve (16).

The pyroelectric valve pneumatic circuit 100-2 is composed of a sub supply line f and a sub connection line g. The sub supply line f branches off from the charging line a and connects the compressed gas tank 2 and the pyro valve 3. The pneumatic pressure is detected by the pirovalve pressure measurement sensor 9, And the flow path is opened and closed to the sub supply line main valve 13, and the air pressure is discharged to the atmosphere through the third vent valve 20. The sub connection line g connects the pyro valve 3 and the pyro apparatus 4 and pneumatic pressure is discharged to the atmosphere through the fourth vent valve 21.

Specifically, the computer 200 controls the operation of the compressor 1, the use of the detection values of the sensor units 6, 7, 8, 9, the valve units 10, 11, 12, 13, 14, 15, , 18, 19, 20, 21) and the regulator units 22, 23 are controlled in accordance with the in-situ pyrolyzer performance test method. As a result, the pneumatic circuits 100-1, Thereby creating a condition in which the pyro apparatus 4 can measure the operating performance under high pressure and the gas-tightness before and after operation in situ. To this end, the computer 200 is equipped with a program for controlling the respective components of the pneumatic device 100 and a pneumatic performance test of the pyro apparatus 4, and can be applied to a notebook computer.

Specifically, the pyrozer 300 performs ignition by igniting the pyrolysis valve 3 or pyrolyzer 4 gunpowder.

On the other hand, Fig. 2 shows the configuration of the pilot valve 3. Fig. As shown, the pyro valve 3 includes a pressure cartridge 24 in which a small amount of explosive gas is burned to release gas pressure, a piston 25 which moves to the gas pressure of the pressure cartridge 24, And a flow pipe 26 for opening the flow path when the piston 25 moves. Particularly, considering that the maximum pressure reaching time is about 0.5 ms when the moving distance of the piston 25 required for completely opening the channel is 10 mm, the moving speed of the piston of the general piro device is averaged It is similar to the maximum pressure reach time inside a pyro apparatus using a pressure cartridge considering that it is more than 20 m / s.

3 shows the configuration of the pyro apparatus 4 in which the operating performance under high pressure and the airtightness before and after the operation are examined. As shown, the pyro apparatus 4 includes a pressure cartridge body 27, a pressure cartridge gun powder 28, a piston 29, a pyrolytic device body 30, an axial flow pipe 31, And a flow pipe (32). The pressure cartridge body 27 is located at one end of the pyro apparatus body 30 with a pressure cartridge gun powder 28. The piston 29 is located in the axial flow pipe 31 formed in the axial direction and is connected to the axial flow pipe 31 by the gas pressure generated in the explosion of the pressure cartridge powder 28, Thereby closing the circumferential flow pipe 32 communicated with the axial flow pipe 31. [0064]

Meanwhile, FIG. 4 shows a flow chart of a method for testing the performance of the pyro apparatus in place according to the present embodiment. Hereinafter, the in-situ pyrode performance test method performed by the computer 200 equipped with the logic of the test method will be described in detail with reference to FIGS. 5 to 8. FIG.

S10 to S30 are pneumatic device setting steps, which are divided into high pressure gas filling (~ 4,000 psig) of S10 and test pressure adjustment, pneumatic circuit setting (atmospheric pressure) of S20, and measurement equipment setting for pneumatic performance test of S30.

The pneumatic device setting step is controlled by the computer 200. Referring to FIG. 5, the high-pressure gas generated by driving the compressor 1 is stored in the compressed gas tank 2. At this time, the computer 200 closes the regulation valve 11 while opening the compressor valve 10. Therefore, only the filling line (a) among the pyro apparatus pneumatic circuit 100-1 and the pyroelectric valve pneumatic circuit 100-2 is opened. Next, when the filling of the compressed gas tank 2 is completed, the computer 200 opens the regulation valve 11 and regulates the desired pressure with the main regulator 23. [ At this time, the computer 200 closes the first main supply line main valve 12 and the sub supply line main valve 13, while opening all the other valves, so that the pyro apparatus pneumatic circuit 100-1 and the piro valve The pneumatic circuit 100-2 is formed in an atmospheric pressure state. Thereafter, the computer 200 measures the pressure value detected by the axial pressure measurement sensor 6, the circumferential pressure measurement sensor 7, the closed vessel pressure measurement sensor 8, and the pyro valve pressure measurement sensor 9 Reset to 0 (zero) on software (logic or program) to prepare the pneumatic pressure to be measured in psig. In addition, the pyroarchet apparatus 300 is connected to the pyro valve 3 or the pyro apparatus 4.

On the other hand, S40 to S80 are the steps in which the pressure performance test of the pyro apparatus 4 is performed.

Step S40 is a stage in which the type of the pyro apparatus 4 is selected, which is divided into application of the active pyro apparatus in which the gunpowder is detonated and application of the inert pyro apparatus in the state in which the gunpowder is removed.

The above-mentioned active pyro apparatus test is carried out by the pyro apparatus installation of S50-1, the preparation preparation of the pyrolysis, the closing of the pneumatic circuit of the pyro valve, the formation of the pyro apparatus pneumatic pressure of S60-1, the pyro apparatus width and pressure measurement of S70-1 do.

The active pyro apparatus test is controlled by the computer 200. Referring to Figs. 5 and 6, the pyro apparatus 4 is installed between the main supply line b and the main discharge line c. In this case, the axial flow pipe 31 in the direction of the piston 29 is connected to the main supply line b in the direction of the axial pressure measurement sensor 6, and the circumferential flow pipe 32 on the side face is connected to the circumferential pressure Is connected to the main discharge line (c) in the direction of the measuring sensor (7). On the other hand, the operation of the sub-supply line main valve 13, the third and fourth vent valves 20, 21 and the sub-regulator 22 is not performed because the pyro-valve 3, The valve pneumatic circuit 100-2 is closed. The computer 200 then closes all the valves 10, 11, 12, 14, 15, 16, 17, 18, 19, 21 of the pyro apparatus pneumatic circuit 100-1, , 7, 8).

Then, the pressure cartridge detonation preparation of the pyro apparatus 4 is completed.

The computer 200 then opens the second main supply line main valve 14 to apply a high pressure gas (~ 4,000 psig) to the axial flow path tube 31 of the pyro apparatus 4. At this time, the axial pressure measurement sensor 6 and the circumferential pressure measurement sensor 7 display a high pressure (~ 4,000 psig). Thereafter, the pyrolyzer 300 is actuated by the computer 200 or by itself, thereby expelling the pressure cartridge gunpowder 28. 6, the piston 29 is moved by the gas pressure of the pressure cartridge gun 28 to move the axial flow passage pipe 31 to close the circumferential flow passage pipe 32. In this state, the computer 200 The operating performance of the pyro apparatus 4 is measured under high pressure by reading the detected values of the axial pressure measurement sensor 6 and the circumferential pressure measurement sensor 7. [

On the other hand, the inactive pyro apparatus test is performed by setting the inactive pyro apparatus installation and pyro valve establishment preparation in S50-2, forming the pneumatic pressure in the inactive pyro apparatus and pyro valve in S60-2, And pressure measurements.

The inactive pyro apparatus test is controlled by the computer 200. Referring to Fig. 7, the pyro valve 3 is set between the sub supply line f and the sub connection line g, whereby the pyro valve pneumatic circuit 100-2 is set. At this time, the pyro apparatus pneumatic circuit 100-1 has the pyro apparatus 4 as shown in Fig. 5, but the pyro apparatus 4 has the pressure cartridge gun powder 28 removed. Therefore, the high-pressure gas outlet of the pilot valve 3 can be connected to the axial flow pipe 31 of the pyro apparatus 4. [ The computer 200 then opens the sub supply line main valve 13 to apply a high pressure gas (~ 4,000 psi) to the pyro valve 3 and the pirovalve pressure measurement sensor 9 displays the desired pressure Check until you do.

 The computer 200 then opens the fourth vent valve 21 when the desired pressure is reached and the pyroarmor 300 disengages the pressure cartridge 24 by the computer 200 or by its own operation. 8, since the pilot valve 3 is also a kind of pyro apparatus, the piston 25 is moved by the gas pressure released by burning a small amount of the gun powder in the pressure cartridge 24, The flow pipe 26 of the pilot valve 3 is opened. That is, when the piston 25 is operated, the hole of the piston 25 coincides with the flow pipe 26, and the flow path is opened. Particularly, since the moving speed of the piston of a general pyrolyzer is more than 20 m / s on an average, the maximum pressure reaching time is about 0.5 ms when the piston travel distance required for opening the complete channel is 10 mm. Therefore, it is similar to the maximum pressure reaching time inside a pyro apparatus using a general pressure cartridge.

Subsequently, by operating the high pressure pyro apparatus 4 through the pyro valve 3, the pyro apparatus 4 measures its operating performance under high pressure as described with reference to FIG. Therefore, the hermetic performance test for the subsequent pyro apparatus 4 can also be carried out in the same manner as the operational performance test.

Meanwhile, S80 is a step for determining whether to stop the active pyro apparatus test or the inactive pyro apparatus test, and for this, whether the pressure measurement time elapses during operation is applied. For example, the pressure measurement time elapses after one minute of operation by applying 1 minute, and then the pressure measurement is stopped.

On the other hand, S90 to S140 are steps in which the airtightness performance test of the pyro apparatus 4 is performed. In particular, the airtightness performance test may change the leakage measurement direction by monitoring the axial pressure measurement sensor 6 while pressing the circumferential flow pipe 32 of the pyro apparatus 4.

S90 is the stage where the pressure measurement is interrupted and the pneumatic circuit is reset, which closes all the valves back to the computer 200 and then opens and closes the valves 18 and 19 to 0 psig. S100, which initiates pressure measurement to the computer 200 and opens the valve 14 to apply a high pressure gas (" 4,000 psig). Measure the pressure for a few minutes and observe especially the pressure change of the pressure sensor (7). S110 is a step of determining whether the pressure leakage amount is increased. If the pressure leakage amount is increased at this step, the measurement volume is increased as in S120. In order to increase the measurement volume, the computer 200 opens the auxiliary return line valve 16 to further increase the measurement volume by 40 cc in the closed container 5, thereby increasing the external vibration of the piping line of the pyro apparatus pneumatic circuit 100-1 It is possible to attenuate the noise that can be carried by the pressure signal and to measure the leakage amount per hour more precisely by increasing the measuring time.

Step S130 is a step of determining the elapsed time of the pressure measuring time after the operation. For example, the pressure measurement time elapsed after 1 minute of operation, and after one minute, the pressure measurement was stopped and the airtightness performance test was stopped.

S140 is a step of determining whether or not the airtightness performance test is to be switched so that the pressure and airtightness performance of another pyrogenic device can be successively tested after the pressure and airtightness of the active pyroitic device or the inert pyrolytic device is completed it means. Therefore, if pressure and airtightness performance are required for other pyrogen devices, such as S150, it is possible to provide the convenience of entering directly into S40 without reworking the pneumatic device setting steps S10 through S30. Therefore, S140 and S150 are omitted in the absence of pressure and airtightness performance tests on other pyrogenic devices.

FIG. 9 is an example of airtightness test data before and after the operation of the pyroelectric device tested by the air pressure device according to the experimental example, FIG. 10 is an example of airtightness test data after the pyroelectric device operation test performed by the air pressure device according to the experimental example to be.

Referring to FIG. 9, a pressure signal before and after the ignition of the pressure cartridge gun 28 in the state where the 4,000 psi air pressure is applied to the pyro apparatus 4 can be known. In this case, the pressure signals and the aerial signal measurements are made at the same time, so the times coincide. 9) shows that 4,000 psig was applied in about 30 seconds as a pressure signal, and FIG. 9, 2) shows that the ignition signal was ignited at about 43 seconds.

Referring to FIG. 10, after the ignition is completed, 4,000 psig is again applied to the pyro apparatus 4, which is the airtightness test data obtained by measuring the leakage amount. In this case, it was pressurized from the axial pressure measurement sensor 6 side, and the circumferential pressure measurement sensor 7 measured the leakage amount through the pyrolysis device 4 at 0 psig. Here, P1 is the directional pressure measurement sensor 6, P2 is the circumferential pressure measurement sensor 7, and P3 is the pressure sensor 8. 10 shows all the measured values of the pressure sensors P1, P2, and P3, and each of 2), 3) and 4) of FIG. 10 is an enlarged view of each measured value, 10, No. 3) shows a result of measuring the leakage amount through P2 to about 0.015 psig / sec.

As described above, the pneumatic device 100 according to the present embodiment is capable of operating performance of the activated type pyro apparatus 4 in which the gunpowder is ignited under a high pressure (~ 4,000 psig) Type pyro apparatus 4 which can be measured and which does not evade the gunpowder by using the pyro valve 3 which transfers a high pressure (~ 4,000 psig) of pneumatic pressure to the pyro apparatus 4 Performance and pre-and-post confidentiality can be measured in place. Therefore, the pneumatic device 100 can precisely measure the leakage pressure per second through the stabilization of the measurement system while the pneumatic performance test of various piro devices can be performed in-situ efficiently.

1: Compressor 2: Compressed gas tank
3: Pyro valve 4: Pyro apparatus
5: Closed container 6: Axial pressure measurement sensor
7: Circumferential pressure measuring sensor 8: Closed container pressure measuring sensor
9: Pyro-valve pressure measuring sensor
10: Compressor valve 11: Regulation valve
12, 14: First and second main supply line main valves
13: Sub supply line main valve
15: Secondary supply line valve
16: auxiliary return line valve 17: main discharge line valve
18,19,20,21: 1st, 2nd, 3rd and 4th vent valves
22: Sub-regulator 23: Main regulator
24: pressure cartridge 25: piston
26: Flow pipe 27: Pressure cartridge body
28: Pressure cartridge gunpowder 29: Piston
30: Pyrode body 31: Axial flow pipe
32: circumferential flow pipe
100: Pneumatic device 100-1: Piro device Pneumatic circuit
100-2: Pyro-valve pneumatic circuit
200: computer 300: pyro-explosive device
a: charge line b: main supply line
c: Main discharge line d-1: Secondary supply line
d-2: auxiliary return line
f: sub-supply line g: sub-connection line

Claims (13)

A compressor for generating a high pressure gas and storing it in a compressed gas tank as a charge line;
A pyro apparatus connected to the compressed gas tank and connected between a main supply line through which the high pressure gas stored in the compressed gas tank flows and a main discharge line through which the high pressure gas is discharged to the atmosphere and in which the pneumatic pressure of the high pressure gas directly acts;
A pyro valve connected between a sub supply line branching from the main supply line and a sub connection line connected to the pyro apparatus, the pneumatic valve directly acting on the pneumatic pressure of the high pressure gas;
An airtight container provided between the auxiliary return line branched from the sub connection line and the auxiliary supply line leading to the main supply line to provide a volume increasing space;
A sensor unit measuring the pressure of the high-pressure gas flowing through the main supply line, the main discharge line, and the sub-supply line, and measuring the pressure of the high-pressure gas caught in the sealed vessel;
A valve unit for opening / closing a flow path of the charging line, the main supply line, the main discharge line, the sub supply line, and the sub connection line;
A regulator unit for regulating a pneumatic pressure of the main supply line and the sub supply line;
Characterized in that the pneumatic device is a pneumatic device. [2] The pyrolytic valve according to claim 1, wherein the pyrovalve includes a pressure cartridge which is burned when ignited and releases a gas pressure, a piston which moves by the gas pressure, and a flow pipe which opens the passage through which the high- Pneumatic device for in - situ pyro - device performance test.
The apparatus of claim 1, wherein the pyro apparatus comprises an axial flow pipe to which the main supply line is connected, and a circumferential flow pipe to which the main discharge line is connected. Pneumatic devices.
The apparatus of claim 1, wherein the sensor unit comprises: an axial pressure measurement sensor for measuring a pneumatic pressure applied to the main supply line; a circumferential pressure measurement sensor for measuring pneumatic pressure applied to the main discharge line; An airtight container pressure measuring sensor, and a valve pressure measuring sensor for measuring the air pressure applied to the sub supply line.
The valve unit according to claim 1, wherein the valve unit comprises: a compressor valve for opening / closing a flow path of the charging line; a regulation valve for regulating a pneumatic pressure of the main supply line; A main supply line main valve, a sub supply line main valve for opening and closing the flow passage of the sub supply line, an auxiliary supply line valve for opening and closing the flow passage of the auxiliary supply line, an auxiliary return line for opening / closing the flow passage of the auxiliary return line, A main discharge line valve for opening and closing the flow passage of the main discharge line, a first and a second vent valves for opening and closing the main discharge line in communication with the atmosphere, a third vent valve for opening and closing the sub- And a fourth vent valve for opening and closing the sub connection line to communicate with the atmosphere. Pneumatic devices for testing.
2. The pneumatic device according to claim 1, wherein the regulator unit comprises a sub-regulator for regulating the pneumatic pressure of the sub-supply line, and a main regulator for regulating the pneumatic pressure of the main supply line. .
2. The control apparatus according to claim 1, wherein software for testing the operating performance of the pyro apparatus and the airtightness before and after the operation of the compressor, the detection value of the sensor unit, and the operation control of the valve unit and the regulator unit under high pressure Lt; / RTI >computer;
Characterized in that the pyrovalves and the pyrodes of the pyro apparatus are carried out with pyro-aerodynamic apparatus.
(A) atmospheric pressure formation of a pyrolytic pneumatic circuit provided with a pyrolytic pneumatic circuit and a pyrolytic valve in which a pyrogenic device is installed when a high-pressure gas generated by the compressor is stored in a compressed gas tank, A pneumatic device setting step of resetting the pneumatic pressure detection value of the pyro valve pneumatic circuit to 0 (zero) by the computer;
(B) an active type pyro apparatus in which the pyro apparatus is sputtered or an inert type pyro apparatus in which no sprocket is made, and in the case of the active type pyro apparatus, the pyro valve pneumatic circuit Wherein the high pressure is applied to the pyro apparatus pneumatic circuit in a closed state to measure pressure performance of the pyro apparatus, and in the case of the inactive type pyro apparatus, the pyro apparatus pneumatic circuit and the pyro valve Performing a pressure performance test in which the pressure performance of the pyro apparatus is measured by applying a high pressure to the pneumatic circuit;
(C) after the pressure performance measurement has ended with a pressure performance measurement time elapse, the computer is closed with the pressure of the pyro apparatus pneumatic circuit and the pyro valve pneumatic circuit with reset to 0 psig, To perform the airtightness performance test by observing the pressure measurement and the pressure change during the measurement of the airtightness performance;
(D) a closed container provided in the pyro apparatus pneumatic circuit for increasing the measurement volume of the pyro apparatus pneumatic circuit when the leakage amount of the pyro apparatus is increased during the measurement of the airtightness performance, step;
Wherein the test is performed on the basis of the test results.
The method according to claim 8, wherein the high pressure is 4,000 psig or less.
10. The method of claim 8, wherein in the pneumatic device setting step, the computer measures the pneumatic detection value in psig.
10. The method of claim 8, wherein in performing the pressure performance test, the active pyro apparatus test is performed by measuring the axial and circumferential pressures of the pyro apparatus after the pyro apparatus is exploded, , And the active pyro apparatus test is performed by measuring the axial pressure and the circumferential pressure of the pyro apparatus after the pyro valve is worn, and the pressure performance measurement is performed.
The pyrolysis apparatus performance test method according to claim 8, wherein the pressure performance measurement time is one minute, and the airtight performance measurement time is several minutes.
10. The method of claim 8, wherein the measured volume increase is 40 cc.

Images