USH206H - Dynamic pressure calibrator - Google Patents

Dynamic pressure calibrator Download PDF

Info

Publication number
USH206H
USH206H US06/835,857 US83585786A USH206H US H206 H USH206 H US H206H US 83585786 A US83585786 A US 83585786A US H206 H USH206 H US H206H
Authority
US
United States
Prior art keywords
pressure chamber
pressure
small
small pressure
channel
Prior art date
Legal status (The legal status 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 status listed.)
Abandoned
Application number
US06/835,857
Inventor
Donald H. Newhall
Arpad A. Juhasz
Charles D. Bullock
II James O. Pilcher
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
US Department of Army
US Department of Navy
Original Assignee
US Department of Army
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 US Department of Army filed Critical US Department of Army
Priority to US06/835,857 priority Critical patent/USH206H/en
Assigned to UNITED STATES OF AMERICA THE, AS REPRESENTED BY THE SECRETARY OF THE NAVY reassignment UNITED STATES OF AMERICA THE, AS REPRESENTED BY THE SECRETARY OF THE NAVY ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: PILCHER, JAMES O. II, BULLOCK, CHARLES D., JUHASZ, ARPAD A.
Assigned to HARWOOD ENGINEERING CO., reassignment HARWOOD ENGINEERING CO., ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: NEWHALL, DONALD H.
Assigned to UNITED STATES OF AMERICA THE, AS REPRESENTED BY THE SECRETARY OF THE ARMY, reassignment UNITED STATES OF AMERICA THE, AS REPRESENTED BY THE SECRETARY OF THE ARMY, ASSIGNMENT OF ASSIGNORS INTEREST. SUBJECT TO LICENSE RECITED Assignors: HARWOOD ENGINEERING CO.
Application granted granted Critical
Publication of USH206H publication Critical patent/USH206H/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L27/00Testing or calibrating of apparatus for measuring fluid pressure
    • G01L27/002Calibrating, i.e. establishing true relation between transducer output value and value to be measured, zeroing, linearising or span error determination
    • G01L27/005Apparatus for calibrating pressure sensors

Definitions

  • the present invention relates in general to ballistic pressure transducers or gauges, and in particular to a new and useful method and apparatus for the dynamic calibration of ballistic pressure transducers.
  • large positive pressure pulses are generated which have very short rise times and which can be utilized for the dynamic calibration of ballistic pressure transducers or gauges.
  • Pressure pulses are generated which are up to 150,000 lbs. per square inch with rise times of less than 600 microseconds.
  • Ballistic pressure gauges are routinely calibrated statically against deadweight pressure standards to obtain pressure vs. static response characteristics.
  • the strength of this calibration technique is its traceability to primary pressure standards.
  • the weakness of this technique is in the assumption that the static and dynamic responses of the gauge are identical. Any differences in gauge response between static (calibration) and dynamic (measurement) events will not appear utilizing this calibration technique.
  • Dynamic calibration techniques are necessary to overcome this problem. The generation of precisely known high pressure pulses, however, is not a simple matter. Three general dynamic calibration techniques have been utilized.
  • the first of these is a negative going pressure step or pulse method.
  • the gauge is exposed to a given pressure under static conditions using a hydraulic fluid.
  • the gauge is then sealed off from the hydraulic system and its output is brought to zero.
  • the pressure on the gauge is then relieved using a fast acting dump valve to bring the system to atmospheric pressure.
  • the gauge output obtained during the depressurization is assumed to be the inverse of the corresponding positive pressure pulse or step.
  • Strengths of this technique include its relative simplicity and suitability to use in calibration facilities.
  • the response of the negative step calibrator can be very quick, i.e. 100 microseconds or less.
  • the major assumption, however, that the pressure response of the gauge is equal and opposite to the negative response of the gauge, is not completely accurate. Pressure preloading of the gauge to mount interface and hysteresis causes significant differences between the responses to pressurization and depressurization pulses.
  • Another technique utilizes a ballistic pulse.
  • the gauge is mounted at the end of the tube, in contact with a hydraulic fluid confined by a movable piston.
  • the tube guides a projectile which impacts the piston to create a positive pulse in the fluid.
  • Different pressures may be achieved by varying the compressibility of the fluid, the mass of the piston, and the mass and velocity of the projectile.
  • the pulses rise within milliseconds and mimic the characteristic rising and falling of a ballistic pressure pulse.
  • the ballistic pressure method is quite useful for dynamic comparison of several different pressure gauges. Variations in projectile velocity, frictional effects on the moving piston, and other energy losses make it difficult to accurately compute the actual delivered pressures. Because the projectile is fired during the calibration process, this method requires more extensive safety provisions than are readily available in most laboratories.
  • the final dynamic calibration technique utilizes a shock tube.
  • Two general approaches are followed. In the first, the test gauge is mounted in the end wall of a closed tube and a shock wave is generated from the opposite end of the tube. The gauge output is monitored as the shock front arrives and stagnates at the end wall. In the second approach, the gauge is mounted in the side wall of the tube and its output is monitored as the shock front passes. Both methods generate rapidly rising pressure pulses that are readily calibrated using temperature and velocity measurements and gas properties.
  • Shock tube methods are being successfully used to establish the dynamic response characteristics of pressure gauges. Calibration however, is generally limited to pressures below 1,000 lbs. per square inch, whereas commercial applications required calibration up to 25,000 per square inch and defense applications up to 150,000 lbs. per square inch. Shock tubes also pose an acoustical hazard.
  • the inventive apparatus and method is capable of delivering to a pressure gauge, a precisely predictable repeatable, positive calibrated pressure step or pulse with a sub-millisecond rise time.
  • the inventive device and method are safely operated in a laboratory. Direct analysis of the gauge response curve yields the required information for gauge dynamic response characteristics.
  • pressure pulses of up to 150,000 lbs. per square inch and rise times of less than 600 microseconds can be achieved. This exceeds the practical range of a shock tube technique and represents a rise time which is faster than those produced by the ballistic pulse method.
  • the pressure and rise times achievable in the invention are comparable to those of modern guns to be tested utilizing a ballistic pressure gauge or transducer. The performance of the present invention is thus more than sufficient for calibrating the characteristics of such pressure gauges.
  • an object of the present invention is to provide a device and method for generating high pressure, short rise time pulses which comprises housing means defining a large pressure fluid chamber and a small pressure fluid chamber, a channel connected between and communicating said large and small pressure fluid chambers, valve means in said channel for opening and closing communications between said large and small pressure fluid chambers, a pressure line connected to said large pressure fluid chamber for pressurizing it with a hydraulic fluid, closure means connected to said small pressure fluid chamber for maintaining said small pressure fluid chamber in a closed condition at least when said valve means opens communication between the large and small chambers, and quick action means connected to said valve means for opening said valve means quickly to discharge pressurized fluid from said large pressure fluid chamber to said small pressure fluid chamber.
  • a still further object of the invention is to provide a method and apparatus which yields highly predictable results, the pressure step and rise being a function of the initial level of pressurization in the large chamber, system geometry, fluid bulk modulus and fluid viscosity.
  • the relationship of initial operating pressure to the step pressure is readily determined by either theoretical calculations or direct measurement.
  • the system may be measured directly using primary and secondary standard gauges attached to the large and small chambers.
  • the system is controlled by establishing an initial state of pressure which is determined within 0.1% by a secondary standard gauge.
  • the output pressure to the small chamber has been determined to be in agreement with the predicted pressure to within 0.2%. This is comparable to the results obtained with the negative pressure step method and superior to the results obtained with the ballistic pulse and shock tube methods mentioned above.
  • the system is readily calibrated because of its predictability and repeatability.
  • comparison calibration against a standard gauge is facilitated by the existence of multiple gauge ports which communicate with the small pressure fluid chamber.
  • the invention is formed of a totally enclosed hydraulic system using water and ethylene glycol glycerin, or some other safe pressure medium, it does not pose a potential blast or acoustic hazard which is presented by ballistic pulse and shock tube methods.
  • the system is safe to use in a laboratory without any special safety devices or facilities.
  • a further object of the invention is to provide a device for generatirng high pressure, short rise time pulses which is simple in design, rugged in construction and economical to manufacture.
  • FIG. 1 is a side sectional view of the inventive device for generating high pressure, short rise time pulses
  • FIG. 2 is a transverse sectional view taken through a portion of the device shown in FIG. 1;
  • FIG. 3 is a partial view similar to FIG. 1 but on an enlarged scale
  • FIG. 4 is a graph relating pressure to time for an actual run conducted in accordance with the invention.
  • FIG. 5 is a view similar to FIG. 4 showing the pressure pulse on an enlarged time scale
  • FIG. 6 is a view similar to FIG. 1 showing another run conducted in accordance with the invention.
  • FIG. 7 is a view similar to FIG. 6 of still another run conducted in accordance with the invention.
  • FIG. 8 is a view similar to FIG. 7 of a still further run conducted in accordance with the invention.
  • the inventive device generates a known pressure step in a short time. This pressure is developed in a large reservoir and then discharged into a small sampling cavity by a quick-opening ball valve. Action time is minimized by restricting the mass transfer between the two cavities.
  • the inventive device generates a known pressure step in a short time. This pressure is developed in a large buffer reservoir and then discharged into a small sampling cavity by a quickopeningball valve. Action time is minimized by restricting the mass transfer between the two cavities.
  • a ball valve 4 which provides a high pressure seal at either of two valve seats 5 located at each end of the test chamber 3.
  • Located in the side wall of the test chamber 3 are four gauge ports 6 and one vacuum line port 7 (see FIG. 2).
  • the channel 2, test chamber 3, gauge ports 6 and vacuum line port 7 are contained in a test head 8 which is connected in the housing 20.
  • the test head 8 is a monolithic assembly shown in lateral cross section in FIG. 2. The test head 8 is readily removed from the housing, allowing changing of the gauge ports 6 and the test chamber 3.
  • the ratio of the reservoir 1 volume to the test chamber 3 free volume is 197:1.
  • the channel 2 is kept short and wide to minimize retardation of fluid flow during the operating cycle.
  • An end closure for the test chamber 3 is formed by a ball valve actuator piston 9 and a piston guide bushing 10.
  • Bushing 10 also forms the lower valve seat 5.
  • the piston 9 is actuated by a quick release top-dead-center mechanism which comprises three pin joints 11 connected to two levers 21, an air controlled trigger mechanism 12, a hydraulic jack 13 and a limit stop/buffer 14.
  • the triggering mechanism 12 has a piston connected to the middle pin 11, which moves rapidly to the right in FIGS. 1 and 3 when mechanism 12 is triggered.
  • the system shown in FIG. 1 is in the cocked position with the ball 4 pressed against the upper seat 5 that isolates the test chamber 3 from the reservoir 1.
  • the jack 13 is pressurized to provide sufficient force to seal the reservoir 1 from the test chamber 3.
  • the ratio of reservoir 1 pressure to jack 13 pressure is approximately 100:1.
  • a hollow stem valve 15 connected to a vacuum/drain line is located at port 7.
  • a high pressure line 17 is connected to a port 16 at the upper end of the reservoir 1. This line connects a pressure generation system (not shown) and a pressure measurement system (not shown) to the housing 20.
  • FIG. 3 shows the invention after the trigger mechanism 12 is released.
  • the trigger 12 forces the middle pin joint 11 against the limit stop/buffer 14, relaxes the force generated by the jack 12 and withdraws the ball valve actuator piston 9 into the piston guide bushing 10.
  • Differential pressure between the reservoir 1 and the test chamber 3 forces the valve ball 4 against the lower seat 5 on the piston guide bushing 10 and allows fluid to flow from the reservoir 1 to the test chamber 3 causing the pressure in the chamber 3 to rise to approximately 98% of the original reservoir pressure.
  • the inventive device operates in the following way.
  • the top-dead-center mechanism is placed in the release position as shown in FIG. 3.
  • the high pressure line 17 is closed off and vacuum valve 15 is opened. This is done by moving the valve 15 to the left to open port 7.
  • Gauges are mounted in the gauge ports 6.
  • the system is evacuated over the vacuum/drain port 7 to a pressure of 2 Torr and the vacuum valve 15 is then closed.
  • a 50% solution of water and glycol with a rust inhibitor enters the system through the high pressure line 17.
  • the top-dead-center mechanism is cocked as shown in FIG. 1.
  • the hydraulic jack 13 is pressurized to approximately 1% of the desired reservoir pressure.
  • the pressure generator system pressurizes the reservoir 1 over line 17. Once the desired reservoir pressure has been established, the high pressure line 17 is closed off from the standard gauge and the pressure generation system. The system is now ready to be triggered.
  • test gauges and their associated recording system are triggered just prior to activation of the top-dead-center mechanism shown in FIG. 3.
  • One gauge with exceptionally good response characteristics and known history is used as an informal laboratory standard.
  • the output from this gauge is monitored for at least 10 seconds after the trigger event to observe system behavior, particularly possible pressure losses from leakage.
  • the reservoir pressure is measured by the primary or secondary gauge one to two seconds after the system is triggered to determine the final value of the step pressure.
  • the speed of the step can be measured using the time base of the recording system and the nature of the dynamic response can be checked against the response of a reliable gauge.
  • test gauges can now be replaced for further testing.
  • FIG. 4 shows a typical pressure versus time history for a 75,000 pounds per square inch pulse taken over 20 milliseconds.
  • FIG. 5 shows the pressure versus time history of the same test pulse taken over 10 seconds. These histories were acquired from a high quality laboratory pressure gauge calibrated against a controlled clearance deadweight primary pressure standard, recorded on a calibrated transient recording digital oscilloscope.
  • One important application of the step calibrator is the relative evaluation of different pressure gauges.
  • FIGS. 6 and 7 show for a positive-going 100,000 lbs. per square inch pressure pulse, the pressure versus time histories of both a piezoelectric pressure gauge and a strain-type pressure gauge.
  • FIG. 8 shows the pressure versus time history of a developmental pressure pulse.
  • the step calibrator prototype has been successfully exercised from 25,000 pounds per square inch to 150,000 pounds per inch. The repeatability achieved is 0.8% and the predictability is 0.2%. The repeatability between gauge ports is less than 0.1% based on existing data.
  • Compressed fluids either gaseous or liquid, when contained at pressure, become energy reservoirs.
  • the energy stored in the pressurized fluid contained in the large vessel 1 is transferred to the small vessel 3 upon actuation of the trigger 12.
  • Pressure equilibrium between the vessels is rapidly established, where the exact time depends on the properties of the fluid and the relative volumes of the two chambers.
  • a secondary pressure standard allows the user to accurately define the pressure history of a given system.
  • the initial pressures of both the large and small vessels are well known.
  • the small vessel is at atmospheric pressure and the large vessel's pressure is measured with a primary or secondary standard.
  • the final pressures are the same and are determined using a primary or secondary pressure standard.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Analytical Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Measuring Fluid Pressure (AREA)

Abstract

A high pressure, short rise time pulse is generated by first pressurizing aarge chamber utilizing a pressure fluid. An initially closed channel communicates the large chamber with a small test chamber that is closed except for the channel and to which one or more pressure gauges are connected. One of the pressure gauges may be utilized as a standard to indicate pressure in the chamber while another one of the gauges can be calibrated utilizing the device. The channel is abruptly opened to discharge the high pressure fluid from the large chamber to the small test chamber. Only a small amount of fluid enters the small test chamber but the pressures in the large and small chamber are equalized rapidly so that the small chamber experiences a high pressure, short rise time pulse.

Description

STATEMENT OF GOVERNMENT INTEREST
The Government has rights in this invention pursuant to contract DAAK 11-79-C-0020 awarded by the Department of the Army.
FIELD AND BACKGROUND OF THE INVENTION
The present invention relates in general to ballistic pressure transducers or gauges, and in particular to a new and useful method and apparatus for the dynamic calibration of ballistic pressure transducers. According to the invention, large positive pressure pulses are generated which have very short rise times and which can be utilized for the dynamic calibration of ballistic pressure transducers or gauges. Pressure pulses are generated which are up to 150,000 lbs. per square inch with rise times of less than 600 microseconds.
Ballistic pressure gauges are routinely calibrated statically against deadweight pressure standards to obtain pressure vs. static response characteristics. The strength of this calibration technique is its traceability to primary pressure standards. The weakness of this technique however, is in the assumption that the static and dynamic responses of the gauge are identical. Any differences in gauge response between static (calibration) and dynamic (measurement) events will not appear utilizing this calibration technique. Dynamic calibration techniques are necessary to overcome this problem. The generation of precisely known high pressure pulses, however, is not a simple matter. Three general dynamic calibration techniques have been utilized.
The first of these is a negative going pressure step or pulse method. In this technique the gauge is exposed to a given pressure under static conditions using a hydraulic fluid. The gauge is then sealed off from the hydraulic system and its output is brought to zero. The pressure on the gauge is then relieved using a fast acting dump valve to bring the system to atmospheric pressure. The gauge output obtained during the depressurization is assumed to be the inverse of the corresponding positive pressure pulse or step.
Strengths of this technique include its relative simplicity and suitability to use in calibration facilities. The response of the negative step calibrator can be very quick, i.e. 100 microseconds or less. The major assumption, however, that the pressure response of the gauge is equal and opposite to the negative response of the gauge, is not completely accurate. Pressure preloading of the gauge to mount interface and hysteresis causes significant differences between the responses to pressurization and depressurization pulses.
Another technique utilizes a ballistic pulse. In this technique the gauge is mounted at the end of the tube, in contact with a hydraulic fluid confined by a movable piston. The tube guides a projectile which impacts the piston to create a positive pulse in the fluid. Different pressures may be achieved by varying the compressibility of the fluid, the mass of the piston, and the mass and velocity of the projectile. The pulses rise within milliseconds and mimic the characteristic rising and falling of a ballistic pressure pulse.
The ballistic pressure method is quite useful for dynamic comparison of several different pressure gauges. Variations in projectile velocity, frictional effects on the moving piston, and other energy losses make it difficult to accurately compute the actual delivered pressures. Because the projectile is fired during the calibration process, this method requires more extensive safety provisions than are readily available in most laboratories.
The final dynamic calibration technique utilizes a shock tube. Two general approaches are followed. In the first, the test gauge is mounted in the end wall of a closed tube and a shock wave is generated from the opposite end of the tube. The gauge output is monitored as the shock front arrives and stagnates at the end wall. In the second approach, the gauge is mounted in the side wall of the tube and its output is monitored as the shock front passes. Both methods generate rapidly rising pressure pulses that are readily calibrated using temperature and velocity measurements and gas properties.
Shock tube methods are being successfully used to establish the dynamic response characteristics of pressure gauges. Calibration however, is generally limited to pressures below 1,000 lbs. per square inch, whereas commercial applications required calibration up to 25,000 per square inch and defense applications up to 150,000 lbs. per square inch. Shock tubes also pose an acoustical hazard.
SUMMARY OF THE INVENTION
The inventive apparatus and method is capable of delivering to a pressure gauge, a precisely predictable repeatable, positive calibrated pressure step or pulse with a sub-millisecond rise time. The inventive device and method are safely operated in a laboratory. Direct analysis of the gauge response curve yields the required information for gauge dynamic response characteristics. According to the invention, pressure pulses of up to 150,000 lbs. per square inch and rise times of less than 600 microseconds can be achieved. This exceeds the practical range of a shock tube technique and represents a rise time which is faster than those produced by the ballistic pulse method. The pressure and rise times achievable in the invention are comparable to those of modern guns to be tested utilizing a ballistic pressure gauge or transducer. The performance of the present invention is thus more than sufficient for calibrating the characteristics of such pressure gauges.
Accordingly, an object of the present invention is to provide a device and method for generating high pressure, short rise time pulses which comprises housing means defining a large pressure fluid chamber and a small pressure fluid chamber, a channel connected between and communicating said large and small pressure fluid chambers, valve means in said channel for opening and closing communications between said large and small pressure fluid chambers, a pressure line connected to said large pressure fluid chamber for pressurizing it with a hydraulic fluid, closure means connected to said small pressure fluid chamber for maintaining said small pressure fluid chamber in a closed condition at least when said valve means opens communication between the large and small chambers, and quick action means connected to said valve means for opening said valve means quickly to discharge pressurized fluid from said large pressure fluid chamber to said small pressure fluid chamber.
A still further object of the invention is to provide a method and apparatus which yields highly predictable results, the pressure step and rise being a function of the initial level of pressurization in the large chamber, system geometry, fluid bulk modulus and fluid viscosity. In a given system according to the invention, the relationship of initial operating pressure to the step pressure is readily determined by either theoretical calculations or direct measurement. The system may be measured directly using primary and secondary standard gauges attached to the large and small chambers. The system is controlled by establishing an initial state of pressure which is determined within 0.1% by a secondary standard gauge. The output pressure to the small chamber has been determined to be in agreement with the predicted pressure to within 0.2%. This is comparable to the results obtained with the negative pressure step method and superior to the results obtained with the ballistic pulse and shock tube methods mentioned above.
The system is readily calibrated because of its predictability and repeatability. In addition, comparison calibration against a standard gauge is facilitated by the existence of multiple gauge ports which communicate with the small pressure fluid chamber.
Since the invention is formed of a totally enclosed hydraulic system using water and ethylene glycol glycerin, or some other safe pressure medium, it does not pose a potential blast or acoustic hazard which is presented by ballistic pulse and shock tube methods. The system is safe to use in a laboratory without any special safety devices or facilities.
A further object of the invention is to provide a device for generatirng high pressure, short rise time pulses which is simple in design, rugged in construction and economical to manufacture.
The various features of novelty which characterize the invention are pointed out with particularity in the claims annexed to and forming a part of this disclosure. For a better understanding of the invention, its operating advantages and specific objects attained by its uses, reference is made to the accompanying drawings and descriptive matter in which a preferred embodiment of the invention is illustrated.
BRIEF DESCRIPTION OF THE DRAWINGS
In the drawings:
FIG. 1 is a side sectional view of the inventive device for generating high pressure, short rise time pulses;
FIG. 2 is a transverse sectional view taken through a portion of the device shown in FIG. 1;
FIG. 3 is a partial view similar to FIG. 1 but on an enlarged scale;
FIG. 4 is a graph relating pressure to time for an actual run conducted in accordance with the invention;
FIG. 5 is a view similar to FIG. 4 showing the pressure pulse on an enlarged time scale;
FIG. 6 is a view similar to FIG. 1 showing another run conducted in accordance with the invention;
FIG. 7 is a view similar to FIG. 6 of still another run conducted in accordance with the invention; and
FIG. 8 is a view similar to FIG. 7 of a still further run conducted in accordance with the invention.
DESCRIPTION OF THE PREFERRED EMBODIMENT
The inventive device generates a known pressure step in a short time. This pressure is developed in a large reservoir and then discharged into a small sampling cavity by a quick-opening ball valve. Action time is minimized by restricting the mass transfer between the two cavities.
The inventive device generates a known pressure step in a short time. This pressure is developed in a large buffer reservoir and then discharged into a small sampling cavity by a quickopeningball valve. Action time is minimized by restricting the mass transfer between the two cavities.
The invention, illustrated in FIG. 1 comprises a housing 20 which includes a large pressure reservoir or chamber 1 opening into a short wide channel 2 which terminates in a very small cylindrical test chamber 3. Located in the test chamber 3 is a ball valve 4 which provides a high pressure seal at either of two valve seats 5 located at each end of the test chamber 3. Located in the side wall of the test chamber 3 are four gauge ports 6 and one vacuum line port 7 (see FIG. 2). The channel 2, test chamber 3, gauge ports 6 and vacuum line port 7 are contained in a test head 8 which is connected in the housing 20. The test head 8 is a monolithic assembly shown in lateral cross section in FIG. 2. The test head 8 is readily removed from the housing, allowing changing of the gauge ports 6 and the test chamber 3. The ratio of the reservoir 1 volume to the test chamber 3 free volume is 197:1. The channel 2 is kept short and wide to minimize retardation of fluid flow during the operating cycle.
An end closure for the test chamber 3 is formed by a ball valve actuator piston 9 and a piston guide bushing 10. Bushing 10 also forms the lower valve seat 5. The piston 9 is actuated by a quick release top-dead-center mechanism which comprises three pin joints 11 connected to two levers 21, an air controlled trigger mechanism 12, a hydraulic jack 13 and a limit stop/buffer 14. The triggering mechanism 12 has a piston connected to the middle pin 11, which moves rapidly to the right in FIGS. 1 and 3 when mechanism 12 is triggered. The system shown in FIG. 1 is in the cocked position with the ball 4 pressed against the upper seat 5 that isolates the test chamber 3 from the reservoir 1. The jack 13 is pressurized to provide sufficient force to seal the reservoir 1 from the test chamber 3. The ratio of reservoir 1 pressure to jack 13 pressure is approximately 100:1.
A hollow stem valve 15 connected to a vacuum/drain line is located at port 7.
A high pressure line 17 is connected to a port 16 at the upper end of the reservoir 1. This line connects a pressure generation system (not shown) and a pressure measurement system (not shown) to the housing 20.
FIG. 3 shows the invention after the trigger mechanism 12 is released. The trigger 12 forces the middle pin joint 11 against the limit stop/buffer 14, relaxes the force generated by the jack 12 and withdraws the ball valve actuator piston 9 into the piston guide bushing 10. Differential pressure between the reservoir 1 and the test chamber 3 forces the valve ball 4 against the lower seat 5 on the piston guide bushing 10 and allows fluid to flow from the reservoir 1 to the test chamber 3 causing the pressure in the chamber 3 to rise to approximately 98% of the original reservoir pressure.
The inventive device operates in the following way.
Starting with a drained system, the top-dead-center mechanism is placed in the release position as shown in FIG. 3. The high pressure line 17 is closed off and vacuum valve 15 is opened. This is done by moving the valve 15 to the left to open port 7. Gauges are mounted in the gauge ports 6. The system is evacuated over the vacuum/drain port 7 to a pressure of 2 Torr and the vacuum valve 15 is then closed. A 50% solution of water and glycol with a rust inhibitor enters the system through the high pressure line 17. When the system is filled and stabilized at atmospheric pressure, the top-dead-center mechanism is cocked as shown in FIG. 1. The hydraulic jack 13 is pressurized to approximately 1% of the desired reservoir pressure. Monitored by a primary or secondary gauge (not shown) the pressure generator system pressurizes the reservoir 1 over line 17. Once the desired reservoir pressure has been established, the high pressure line 17 is closed off from the standard gauge and the pressure generation system. The system is now ready to be triggered.
The test gauges and their associated recording system are triggered just prior to activation of the top-dead-center mechanism shown in FIG. 3. One gauge with exceptionally good response characteristics and known history is used as an informal laboratory standard. The output from this gauge is monitored for at least 10 seconds after the trigger event to observe system behavior, particularly possible pressure losses from leakage. The reservoir pressure is measured by the primary or secondary gauge one to two seconds after the system is triggered to determine the final value of the step pressure. The speed of the step can be measured using the time base of the recording system and the nature of the dynamic response can be checked against the response of a reliable gauge.
At the completion of the test, the top-dead-center mechanism is recocked, the test chamber 3 is drained through the vacuum valve 15, and the pressure is relaxed in the reservoir 1. The test gauges can now be replaced for further testing.
FIG. 4 shows a typical pressure versus time history for a 75,000 pounds per square inch pulse taken over 20 milliseconds. FIG. 5 shows the pressure versus time history of the same test pulse taken over 10 seconds. These histories were acquired from a high quality laboratory pressure gauge calibrated against a controlled clearance deadweight primary pressure standard, recorded on a calibrated transient recording digital oscilloscope. One important application of the step calibrator is the relative evaluation of different pressure gauges. FIGS. 6 and 7 show for a positive-going 100,000 lbs. per square inch pressure pulse, the pressure versus time histories of both a piezoelectric pressure gauge and a strain-type pressure gauge. FIG. 8 shows the pressure versus time history of a developmental pressure pulse. The step calibrator prototype has been successfully exercised from 25,000 pounds per square inch to 150,000 pounds per inch. The repeatability achieved is 0.8% and the predictability is 0.2%. The repeatability between gauge ports is less than 0.1% based on existing data.
The preceding description of the successful prototype of this invention uses a specific example that illustrates the principles of the device. Changes in the chamber ratio, addition of temperature sensors, the substitution of different valves make the invention useful in conducting other dynamic pressure tests. For example, the measurement of fundamental thermo-dynamic data such as adiabatic effects can be successfully achieved.
Compressed fluids, either gaseous or liquid, when contained at pressure, become energy reservoirs. The energy stored in the pressurized fluid contained in the large vessel 1 is transferred to the small vessel 3 upon actuation of the trigger 12. Pressure equilibrium between the vessels is rapidly established, where the exact time depends on the properties of the fluid and the relative volumes of the two chambers.
The use of a secondary pressure standard allows the user to accurately define the pressure history of a given system. Before the trigger is released, the initial pressures of both the large and small vessels are well known. The small vessel is at atmospheric pressure and the large vessel's pressure is measured with a primary or secondary standard. After the trigger is released the final pressures are the same and are determined using a primary or secondary pressure standard.
While a specific embodiment of the invention has been shown and described in detail to illustrate the application of the principles of the invention, it will be understood that the invention may be embodied otherwise without departing from such principles.

Claims (16)

What is claimed is:
1. A device for generating high pressure, short rise time pulses, comprising:
housing means defining a large pressure chamber, a small pressure chamber and a channel communicating said large and small pressure chambers;
a high pressure line connected to said large pressure chamber for supplying a pressurized fluid to said large pressure chamber;
valve means movable in said housing means for closing said channel to permit pressurization of said large pressure chamber through said high pressure line, and for opening said channel for discharging high pressure fluid from said large pressure chamber to said small pressure chamber;
at least one gauge port connected to said small pressure chamber for communication between said small pressure chamber and pressure gauge to be exposed to pressure in said small pressure chamber; and
closure means for closing said small pressure chamber except for communication with said at least one gauge port and said channel and at least when said valve means opens said channel for confining pressurized fluid entering said small pressure chamber from said large pressure chamber.
2. A device according to claim 1, wherein said valve means comprises a valve member movable into and out of engagement with said channel and a trigger mechanism engaged with said valve member for permitting rapid movement of said valve member away from said channel to open communication between said large and small pressure chambers.
3. A device according to claim 2, wherein said valve member comprises a ball movable in said small pressure chamber, said channel having a valve seat for engagement by said ball for closing communication between said channel and said small pressure chamber, and a top-dead-center mechanism connected between said trigger mechanism and said ball for pressing said ball against said valve seat to close said channel and for rapidly releasing said ball for movement away from said valve seat with triggering of said trigger mechanism.
4. A device according to claim 3, wherein said top-dead-center mechanism comprises a piston movable in said housing means and into said small pressure chamber into engagement against said ball, a pair of levers connected to each other at a middle lever pin, one lever being connected to said piston at an upper lever pin, a hydraulic jack having a piston connected to the other lever at a lower lever pin, said trigger mechanism having a piston engaged with said middle lever pin for holding said middle lever pin in a position to transmit force of said hydraulic jack piston to said piston which is movable in said housing means, said trigger mechanism activated to move its piston so that said middle lever pin is moved into a position releasing pressure of said hydraulic jack piston from said piston which is movable in said housing means to release said ball and open said valve seat.
5. A device according to claim 4, including a bushing fixed in said housing means and slidably receiving said piston which is movable in said housing means, said bushing defining a second valve seat communicating with said small pressure chamber and engageable by said ball, said first mentioned and second valve seats being spaced apart to permit movement of said ball away from said first mentioned seat and into engagement with said second valve seat with actuation of said trigger mechanism.
6. A device according to claim 5, including a vacuum port communicating with said small pressure chamber and a vacuum valve movable in said vacuum port for opening and closing said vacuum port to vent pressure fluid from said small pressure chamber.
7. A device according to claim 1, including a vacuum port communicating with said small pressure chamber and a vacuum valve movable in said vacuum port for opening and closing said vacuum port to vent pressure fluid from said small pressure chamber.
8. A device according to claim 1, including a plurality of gauge ports communicating with said small pressure chamber for establishing communication between said small pressure chamber and a plurality of pressure gauges.
9. A device according to claim 1, wherein said housing means includes a housing having a cavity defining said large pressure chamber and a further cavity, a removable head seated in said further cavity and containing a small pressure chamber, said channel and said at least one gauge port.
10. A method of generating high pressure, short rise time pulses, comprising:
pressurizing a large pressure chamber with a pressure fluid;
discharging the pressurized high pressure fluid from the large pressure chamber through a channel into a small pressure chamber having a volume which is a small fraction of the volume of said large pressure chamber;
confining the pressurized fluid coming from said large pressure chamber in said small pressure chamber to establish a rapid rise in pressure in said small pressure chamber to a point equaling the pressure initially established in said large pressure chamber; and
communicating to a pressure gauge the pressure rise in said small pressure chamber.
11. A method according to claim 10, including evacuating said small pressure chamber to atmospheric pressure when said large pressure chamber is being pressurized and before communication is established between said large and small pressure chamber.
12. A method according to claim 11, including closing said channel using a valve member which is held against said channel to block communication between said large and small pressure chambers, holding said valve member using a hydraulic jack to exert a force on said valve member, and releasing the force on said valve member to establish communication between said large and small pressure chambers.
13. A method according to claim 12, wherein said large pressure chamber with said channel closed is pressurized to a pressure level which is 100 to 1 with respect to a pressure of said jack exerted against said valve member.
14. A method according to claim 10, including closing communication between said large and small pressure chambers by pressing a ball against a valve seat on said channel, and releasing said ball to permit it to move away from said valve seat and to establish communication between said large and small pressure chambers.
15. A method according to claim 14, including pressing said ball against said valve seat using a piston moving through a bushing, said bushing defining a second valve seat communicating with said small pressure chamber and withdrawing said piston to permit movement of said ball away from said first mentioned valve seat and into engagement with said second valve seat.
16. A method according to claim 10, including measuring a pressure in said large pressure chamber after it is pressurized with pressure fluid, connecting a standard pressure gauge to said small pressure chamber to be exposed to the pressure rise in said small pressure chamber, and connecting a pressure gauge to be calibrated to said small pressure chamber.
US06/835,857 1986-02-10 1986-02-10 Dynamic pressure calibrator Abandoned USH206H (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US06/835,857 USH206H (en) 1986-02-10 1986-02-10 Dynamic pressure calibrator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/835,857 USH206H (en) 1986-02-10 1986-02-10 Dynamic pressure calibrator

Publications (1)

Publication Number Publication Date
USH206H true USH206H (en) 1987-02-03

Family

ID=25270633

Family Applications (1)

Application Number Title Priority Date Filing Date
US06/835,857 Abandoned USH206H (en) 1986-02-10 1986-02-10 Dynamic pressure calibrator

Country Status (1)

Country Link
US (1) USH206H (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004079017A2 (en) * 2003-02-26 2004-09-16 Co2 Solutions, Llc System to produce sugar from sugar beets
US20050103092A1 (en) * 2003-11-19 2005-05-19 Chiarito Vincent P. Portable system for measuring dynamic pressure in situ and method of employment therefor
US8904912B2 (en) 2012-08-16 2014-12-09 Omax Corporation Control valves for waterjet systems and related devices, systems, and methods
US20150234089A1 (en) * 2014-02-14 2015-08-20 Ocean Networks Canada Society Hydrophone calibration system
US12064893B2 (en) 2020-03-24 2024-08-20 Hypertherm, Inc. High-pressure seal for a liquid jet cutting system

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004079017A2 (en) * 2003-02-26 2004-09-16 Co2 Solutions, Llc System to produce sugar from sugar beets
WO2004079017A3 (en) * 2003-02-26 2005-08-18 Co2 Solutions Llc System to produce sugar from sugar beets
US20050103092A1 (en) * 2003-11-19 2005-05-19 Chiarito Vincent P. Portable system for measuring dynamic pressure in situ and method of employment therefor
US7266986B2 (en) * 2003-11-19 2007-09-11 The United States Of America As Represented By The Secretary Of The Army Portable system for measuring dynamic pressure in situ and method of employment therefor
US8904912B2 (en) 2012-08-16 2014-12-09 Omax Corporation Control valves for waterjet systems and related devices, systems, and methods
US9610674B2 (en) 2012-08-16 2017-04-04 Omax Corporation Control valves for waterjet systems and related devices, systems, and methods
US10864613B2 (en) 2012-08-16 2020-12-15 Omax Corporation Control valves for waterjet systems and related devices, systems, and methods
US20150234089A1 (en) * 2014-02-14 2015-08-20 Ocean Networks Canada Society Hydrophone calibration system
US9746585B2 (en) * 2014-02-14 2017-08-29 Ocean Networks Canada Society Hydrophone calibration system
US12064893B2 (en) 2020-03-24 2024-08-20 Hypertherm, Inc. High-pressure seal for a liquid jet cutting system

Similar Documents

Publication Publication Date Title
US4646556A (en) Process and apparatus for testing a pilot-operated safety valve
US5184499A (en) Testing device with acceleration tube
US6354137B1 (en) Inertial confinement cylinder for explosive characterization
USH206H (en) Dynamic pressure calibrator
KR850000833B1 (en) Apparatus for cheeking the set pressure of a safety valve
KR100536959B1 (en) True triaxial compression test system
US8910505B2 (en) System and method for simulating primary and secondary blast
CN110411869B (en) Hydropneumatic medium strain rate tensile test device and method
US3338092A (en) Dynamic biaxial testing machine
JPH0249984A (en) Pump testing device
US3404562A (en) High-strain-rate tester
IE42575B1 (en) Apparatus for testing or measuring deformation and fracture of test-pieces under multiaxial tension or compression
US3548646A (en) Tensile test apparatus
SU1647313A1 (en) Device for dynamometer dynamic calibration
US3237443A (en) Dynamic pressure generator for calibration
US3527570A (en) Stopped flow reaction kinetic system
US3473366A (en) Pressure pulse generator
US3492862A (en) Apparatus for tensile testing
US3750459A (en) Hydro-dynamic testing apparatus
RU135745U1 (en) STAND FOR TESTS OF THE LIQUID INHIBITOR AND THE SEALING MEMBRANE CONSIDERED BY THEIR VOLUME
Esparza et al. Measurement of Blast Waves from Bursting Pressureized Frangible Spheres
SU1021982A1 (en) Plant for investigating material tubular specimen complex stressed state
KR102642062B1 (en) Apparatus for testing the crash characteristics of crashing bodies
Jones Tensile testing of elastomers at ultra‐high strain rates
US3399562A (en) Method and test assembly for testing viscoelastic materials

Legal Events

Date Code Title Description
STCF Information on status: patent grant

Free format text: PATENTED CASE

AS Assignment

Owner name: UNITED STATES OF AMERICA THE, AS REPRESENTED BY TH

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST. SUBJECT TO LICENSE RECITED;ASSIGNOR:HARWOOD ENGINEERING CO.;REEL/FRAME:004656/0317

Effective date: 19851119