CN207180923U - A kind of tab load measurement apparatus - Google Patents
A kind of tab load measurement apparatus Download PDFInfo
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- CN207180923U CN207180923U CN201721233123.5U CN201721233123U CN207180923U CN 207180923 U CN207180923 U CN 207180923U CN 201721233123 U CN201721233123 U CN 201721233123U CN 207180923 U CN207180923 U CN 207180923U
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- tab
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- measurement apparatus
- aerostatics utricule
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Abstract
The utility model provides a kind of tab load measurement apparatus, including：Tab to be measured, aerostatics utricule and plane inflation structure, tab to be measured are fixed on aerostatics utricule；Aerostatics utricule is arranged in plane inflation structure, and aerostatics utricule forms inflatable closing space with plane inflation structure.The utility model simulates tab to be measured in actual use, the gas pressure loads in closing space that the aerostatics utricule that is subject in aerostatics is formed with plane inflation structure, realize load value true, when accurately measuring tab actual use to be measured in aerostatics.
Description
Technical field
It the utility model is related to machanical fastener field, more particularly to a kind of tab load measurement apparatus.
Background technology
Aerostatics is the aircraft that lift is provided using the gas (hydrogen, helium, hot gas etc.) for being lighter than air, stagnant by its
Long between space-time, energy-saving and environmental protection, economic dispatch advantage are widely used in military and civilian field.Aerostatics mainly has captive balloon
With two kinds of dirigible, the typically no dynamical system of captive balloon, it is connected by tether cable with ground installation or website；Dirigible has
Power, it can be remotely controlled or automatically control lower autonomous flight.
Either captive balloon or dirigible, tab are processed on aerostatics utricule, are all one indispensable zero
Part.Tab can be divided into I types tab, V-type tab, double V-shaped tab etc. according to shape, and main function is lifting, provides, be fixed
Effect, the load intensity of different function requirements tab are different.The single tab that is measured as on tab load intensity exists at present
Simple tension is carried out on tensile testing machine, and the true service condition of tab can be carried for tab by the air pressure in aerostatics utricule
Lotus, therefore conventional test can not simulate tab in actual use, the true air pressure in aerostatics.
Therefore, how providing one kind can simulate under true environment, and tab is in aerostatics by aerostatics utricule
Gas pressure loads, the true, experimental provision of accurately measure tab load value, turn into the technical problem for being currently needed for solving.
Utility model content
To solve the problems, such as that the true air pressure of aerostatics, the utility model can not be simulated during the above-mentioned measurement of tab load at present
A kind of tab load measurement apparatus is provided, including：Tab to be measured, aerostatics utricule and plane inflation structure, tab to be measured are consolidated
It is scheduled on aerostatics utricule；Aerostatics utricule is arranged in plane inflation structure, and aerostatics utricule is formed with plane inflation structure
Inflatable closing space.
Preferably, tab to be measured is fixed on aerostatics utricule by cutting, sewing or weld.
Preferably, tab to be measured is shaped as：V-type tab, I types tab or double V-shaped tab.
Preferably, tab load measurement apparatus also includes gas storage part, and plane inflation structure is provided with inflation inlet；Gas storage portion
Part is connected with the inflation inlet, and the inflatable closing formed by the inflation inlet to aerostatics utricule and plane inflation structure is empty
Interior inflatable body；Gas includes：Air, helium or nitrogen.
Preferably, tab load measurement apparatus also includes support, and plane inflation structure is fixed on support.
Preferably, tab load measurement apparatus also includes force measuring structure, and force measuring structure includes pulley and counterweight；Counterweight utilizes
Draw-gear, it is connected by pulley with tab to be measured.
Preferably, this tab load measurement apparatus also includes differential pressure pickup and industrial computer, industrial computer and differential pressure pickup
Electrically connected with gas storage part；Pressure difference mouth is also equipped with plane inflation structure, differential pressure pickup is connected with pressure difference mouth；Industrial computer leads to
Over-pressed gap sensor controls gas storage part.
Preferably, plane inflation structure also includes disc base and flange circle, aerostatics utricule be fixed on disc base and
Between flange circle.
The utility model provides a kind of tab load measurement apparatus, by the way that tab to be measured is fixed on into aerostatics utricule
On, simulate under true measuring environment, gas pressure loads of the tab to be measured by aerostatics utricule；Measure tab to be measured and aerostatics
When utricule departs from, the load value of tab to be measured, realize it is true, accurately measure during tab to be measured actually uses on aerostatics
Load value.
Brief description of the drawings
Fig. 1 is the structural representation for the tab load measurement apparatus that the preferred embodiment of the utility model one provides；
Fig. 2 is the structure top view for the tab load measurement apparatus that the preferred embodiment of the utility model one provides；
Fig. 3 is the schematic flow sheet for the tab load measuring method that the preferred embodiment of the utility model one provides；
Fig. 4 is the step flow chart for the tab load measuring method that the preferred embodiment of the utility model one provides.
Wherein：
1. the differential pressure pickup of 2. plane inflation structure of test specimen 3. to be measured
4. the industrial computer of 5. gas storage part of force measuring structure 6.
7. the aerostatics utricule of tab 9. to be measured of draw-gear 8.
10. the inflation inlet of 11. flange circle of disc base 12.
13. the differential pressure pickup of 14. support of pressure difference mouth 15.
16. the counterweight of pulley 17..
Embodiment
With reference to the accompanying drawings and examples, specific embodiment of the present utility model is described in further detail.With
Lower specific embodiment is used to illustrate the utility model, but is not limited to the scope of the utility model.
, it is necessary to explanation in description of the present utility model, term " " center ", " on ", " under ", it is "left", "right", " perpendicular
Directly ", the orientation of the instruction such as " level ", " interior ", " outer " or position relationship are based on orientation shown in the drawings or position relationship, are only
Described for the ease of description the utility model and simplifying, rather than instruction or imply signified device or element must have it is specific
Orientation, with specific azimuth configuration and affected, therefore it is not intended that to limitation of the present utility model.
, it is necessary to which explanation, unless otherwise clearly defined and limited, term " are pacified in description of the present utility model
Dress ", " connected ", " connection " should be interpreted broadly, for example, it may be fixedly connected or be detachably connected, or integratedly
Connection；It can be mechanical connection or electrical connection, can be joined directly together, can also be indirectly connected by intermediary,
It can be the connection of two element internals.For the ordinary skill in the art, above-mentioned art can be understood with concrete condition
Concrete meaning of the language in the utility model.
To aerostatics is fixed on into ground or carry gondola, fixed equipment with it, generally requiring arranging can pass
The machanical fastener with distractive load is passed, aerostatics is typically used as machanical fastener by the use of tab.The major function of tab for lifting,
Provide and fixed, the load intensity of different function requirements tab is different.Therefore, accurate measurement tab load is extremely important.At present,
It is measured as individually being connected to tab that pull test is i.e. upper to carry out simple tension on tab intensity, without considering that tab is true
In fact in use, the gas pressure loads for the aerostatics utricule that tab is subject in aerostatics utricule business.
The structural representation for the tab load measurement apparatus that Fig. 1 provides for the preferred embodiment of the utility model one, such as Fig. 1
It is shown, a kind of tab load measurement apparatus, including：Tab 8, aerostatics utricule 9 and plane inflation structure 2 to be measured, tab 8 to be measured
It is fixed on aerostatics utricule 9；Aerostatics utricule 9 is arranged in plane inflation structure 2, aerostatics utricule 9 and plane inflation knot
Structure 2 forms inflatable closing space.
Specifically, tab 8 to be measured is that the direct measurement object of load value is measured in the present embodiment.Tab 8 to be measured is fixed
On aerostatics utricule 9, tab test specimen 1 to be measured is formed.Aerostatics utricule 9 is arranged in plane inflation structure 2, by aerostatics
Utricule 9 forms inflatable closing space with plane inflation structure 2.During actual measurement, first to aerostatics utricule 9 and plane inflation
The closing space inflatable body that structure 2 is formed, working condition pressure when making the pressure in the closing space be aerostatics actual use, with
So that tab to be measured by aerostatics in normal use, gas pressure loads of the closing space to it；Then tab 8 to be measured is measured
When departing from aerostatics utricule 9, the load value of tab 8 to be measured.
, can be by aerostatics utricule 9 and plane because tab 8 to be measured is in actually measuring in the utility model embodiment
The closing space that inflation structure 2 is formed simulates tab and really held in practical service environment to its gas pressure loads
Power situation；Realize load value that is true, accurately measuring tab.
Based on above-described embodiment, tab 8 to be measured is fixed on aerostatics utricule 9 by way of cutting, sewing or weld
On.
Specifically, in order to form tab 8 to be measured in aerostatics real work by the true of the gas pressure loads of aerostatics utricule 9
Real environment is, it is necessary to which tab 8 to be measured is fixed on aerostatics utricule 9；Tab 8 to be measured can be by cutting, sewing and weld
Mode is fixed on aerostatics utricule 9, and tab 8 to be measured is closely joined together with aerostatics utricule 9, makes tab 8 to be measured accurate
Really, fully bear aerostatics utricule 9 and form the gas pressure loads of inflatable closing space with plane inflation structure 2, so that
It is true, accurate to obtain subsequently measurement.
Wherein, the shape of the tab to be measured 8 used in tab load measurement apparatus is not limited to, the shape of tab 8 to be measured
Including：V-type tab, I types tab or double V-shaped tab, can flexibly it be chosen according to actual conditions.
Specifically, Fig. 2 is that the structure for the tab load measurement apparatus that the preferred embodiment of the utility model one provides is overlooked
Figure, as shown in Fig. 2 tab 8 to be measured used in the present embodiment is shaped as V-type tab.
Based on above-described embodiment, tab load measurement apparatus also includes gas storage part 5, and plane inflation structure 2, which is provided with, fills
Gas port 12；Gas storage part 5 is connected with inflation inlet 12, and is formed by inflation inlet 12 to aerostatics utricule 9 and plane inflation structure 2
Inflatable closing space in inflatable body；Gas includes：Air, helium or nitrogen, make the gas density in the closing space
Less than atmospheric density.
What is be typically filled with aerostatics is the gas that proportion is lighter than air, atmospheric buoyancy force can be relied on to go up to the air.In electronics
It is widely used with military field.It is inflammable at present because hydrogen activity is larger, easily trigger blast and fire, therefore hydrogen is early
No longer it is applied in aerostatics.
In the present embodiment, aerostatics utricule 9 and the gas in the closing space of the formation of plane inflation structure 2 are filled with, including
Air, helium or nitrogen etc., the gas density in the closing space is less than atmospheric density, make the self gravitation of aerostatics utricule 9
It is less than buoyancy of the closing space extraneous air to aerostatics utricule 9 with the internal gas gravity sum of aerostatics utricule 9, so that
Aerostatics utricule 9 can float in atmosphere.
Further, the gas being filled with the present embodiment in the closing space does not limit to, including a kind of density is less than sky
The gas of air tightness；It is a variety of to refer to two or more or a variety of density are less than or greater than the gas of atmospheric density, make the closing
Gas density in space is less than atmospheric density.
Specifically, aerostatics utricule 9 forms an inflatable closing space with plane inflation structure 2, in plane inflation
Inflation inlet 12 is installed in structure 2；Gas storage part 5 is connected with the inflation inlet 12 in plane inflation structure 2, and passes through inflation inlet 12
Inflated in the inflatable closing space formed to aerostatics utricule 9 with plane inflation structure 2.Wherein, the gas storage energy of gas storage part 5
The standard of power is voltage endurance capability, and the internal gas of gas storage part 5 can not be used up all, should retain certain residual compression；Gas storage portion
Part 5 should keep certain safe distance with naked light, and must not close to thermal source, must not be by sunlight exposure.Preferably it is stored in and dries cool place
Place, it is impossible to hit；Gas storage part 5 in movement, park, during use, it should be noted that the protection of bottle and valve, prevent gas
Bottle is toppled over, in order to avoid cause the damage of annex.As found gas leakage in use, the valve of gas storage part 5 should be closed immediately.
Based on above-described embodiment, tab load measurement apparatus also includes support 14, and plane inflation structure 2 is fixed on support 14
On.
Specifically, for fixed and mounting plane inflation structure 2, this tab load measurement apparatus is in plane inflation structure 2
Lower section is additionally provided with support 14, and for ease of having certain height between measurement support 14 and ground, plane inflation structure 2 is fixed
On the support 14；And aerostatics utricule 9 is arranged in plane inflation structure 2, i.e., aerostatics utricule 9 passes through plane inflation structure 2
Fix on the support 14.
Based on above-described embodiment, tab load measurement apparatus also includes force measuring structure 4, and force measuring structure 4 includes the He of pulley 16
Counterweight 17；Counterweight is connected by pulley 16 with the loop head of tab 8 to be measured, is departed from for measuring tab 8 to be measured with aerostatics utricule 9
When, the load value of tab 8 to be measured.
Specifically, force measuring structure 4 is connected with the test specimen of tab 8 to be measured, and force measuring structure 4 includes pulley 16 and weight in the present embodiment
Code 17.Counterweight 17 is utilized into draw-gear 7, is connected by pulley 16 with the loop head of tab 8 to be measured, so that force measuring structure 4
It is connected with tab 8 to be measured.
In the present embodiment, pulley 16 is fixed pulley, and during dynamometry, the position of the axle of pulley 16 is fixed.Utilize cunning
Draw-gear 7 on wheel 16 draws tab 8 to be measured.The weight of counterweight 17 is stepped up, when the weight of counterweight 17 reaches certain value, is treated
Tab 8 is surveyed with aerostatics utricule 9 to depart from.It is 7 both ends equalising torques according to traction dress, by torque equilibrium equation, obtains to work as and treat
When surveying tab 8 with the disengaging of aerostatics utricule 9, the load value of tab 8 to be measured.
For example, set on draw-gear 7, the length of tab 8 loop head to pulley 16 to be measured is L1, the load value of tab to be measured 8 is
F1；Counterweight 17 to the length of pulley 16 be L2, the load value of counterweight 17 be F2；The weight of counterweight 17 is stepped up, until making tab 8 to be measured
Depart from aerostatics utricule 9.According to the both ends equalising torque of draw-gear 7, torque equilibrium equation F1*L1=F2*L2 is established,
In the case of knowing F2, L2, L1, F1 is obtained, when obtaining tab 8 to be measured with the disengaging of aerostatics utricule 9, the load value of tab 8 to be measured.
Wherein, force measuring structure is not limited to pulley and counterweight, can also use for example：Spring tension machine, force-measuring sensing
Device or force measuring machine, can flexibly it be chosen according to actual conditions.
Based on above-described embodiment, plane inflation structure 2 also includes disc base and flange circle, the part of aerostatics utricule 9
It is fixed on 11 between disc base 10 and flange circle.
Specifically, plane inflation structure 2 also includes disc base 10 and flange circle 11, and flange circle 11 is arranged on disc base
On 10.Flange circle is sealing ring, also referred to as pad.The bottom of aerostatics utricule 9 is stuck in the He of disc base 10 in the present embodiment
Between flange circle 11, then with bolt flange circle 11 is fixed, to cause aerostatics utricule 9 to be fixed in plane inflation structure 2, from
And tab 8 to be measured is set to be fixed on by aerostatics utricule 9 in plane inflation structure 2.
Based on above-described embodiment, tab load measurement apparatus also includes differential pressure pickup 15 and industrial computer 6, industrial computer 6 with
Differential pressure pickup 15 and gas storage part 5 electrically connect；Be also equipped with pressure difference mouth 13 in plane inflation structure 2, differential pressure pickup 15 with
Pressure difference mouth 13 connects；Industrial computer 6 controls gas storage part 5 by differential pressure pickup 15, for making aerostatics utricule 9 and plane inflation
The pressure in closing space that structure 2 is formed is maintained at actual condition pressure.
Further, in order to simulate the true environment of tab load measurement, aerostatics utricule 9 and the shape of plane inflation structure 2
Into closing space in pressure need to be maintained under actual condition pressure, to cause aerostatics utricule 9 that tab 8 to be measured is subject to
When pressure is aerostatics real work, gas pressure loads of the aerostatics utricule 9 to tab 8 to be measured.
Differential pressure pickup is a kind of sensor for being used for measuring difference between two pressure, is commonly used to measure a certain equipment
Or the pressure difference of part rear and front end, the operation principle of gas differential pressure sensor are that the diaphragm of sensor is directly acted on by measuring pressure
On, diaphragm is produced the micro-displacement directly proportional to air pressure, the capacitance of sensor is changed, and this is detected with electronic circuit
One change, and change the canonical measure signal of one corresponding pressure of output.In the present embodiment, installed in plane inflation structure
There is pressure difference mouth, differential pressure pickup is connected with pressure difference mouth, aerostatics utricule 9 and plane inflation knot are measured by differential pressure pickup 15
Air pressure in 2 closing spaces being configured to, with the difference between actual condition pressure.
Industrial computer is industrial control computer, is that one kind uses bus structures, production process and electromechanical equipment, technique are filled
The standby instrument assembly for carrying out Detection ＆ Controling, industrial computer have important computer attribute and feature.In the present embodiment, industrial computer
6 electrically connect with differential pressure pickup 15 and gas storage part 5 respectively, when the test specimen of tab 8 to be measured and the closing of the formation of plane inflation structure 2
When air pressure is less than actual condition pressure in space, differential pressure pickup 15 is by the test specimen of tab to be measured 8 of measurement and plane inflation structure 2
Difference signal in the closing space of formation between air pressure and actual condition pressure, and be by analog-to-digital conversion by the difference signal
Electric signal, then send the electric signal to industrial computer 6；Industrial computer 6 controls gas storage part 5 by inflation inlet 12 to the closing space
Interior inflation, until in the closing space that aerostatics utricule 9 and plane inflation structure 2 that differential pressure pickup 15 measures are formed air pressure with
Actual condition pressure is equal, and industrial computer 6 controls gas storage part 5 to stop inflating to the closing space.
The schematic flow sheet for the tab load measuring method that Fig. 3 provides for the preferred embodiment of the utility model one, such as Fig. 3
Shown, on the other hand, the utility model additionally provides a kind of tab load measurement side based on above-mentioned tab load measurement apparatus
Method, including：
S1, tab 8 to be measured is fixed on aerostatics utricule 9；
S2, by aerostatics utricule 9 be arranged on plane inflation structure on, formed to aerostatics utricule 9 and plane inflation structure
Closing space in inflatable body, make pressure in the closing space for tab to be measured actual use when working condition pressure；
When S3, acquisition tab 8 to be measured depart from aerostatics utricule 9, the load value of tab 8 to be measured.
The tab load measuring method of the present embodiment, using the tab load measurement apparatus shown in Fig. 1 and Fig. 2, pass through by
Tab 8 to be measured, which is fixed on aerostatics utricule 9 to produce, forms tab test specimen 1 to be measured, simulates the reality of the test specimen of tab 8 to be measured
Process.By the way that the test specimen of tab 8 to be measured is arranged in plane inflation structure, the plenum space of a closing is formed, is being sealed
Close interior volume and be filled with a certain amount of test gas, the gas pressure in the closing space is maintained at tab 8 to be measured actually makes
Gas pressure in, simulate the air pressure inside load from aerostatics utricule 9 that tab test specimen in true use is born.So
After when obtaining tab to be measured tab 8 to be measured and aerostatics utricule 9 and departing from, the load value of tab 8 to be measured.
Based on above-described embodiment, Fig. 4 is the tab load measuring method that the preferred embodiment of the utility model one provides
Flow chart of steps, as shown in figure 4, the step S3 of this tab load measuring method includes：
S301, by the counterweight 17 in force measuring structure 4 by pulley 16, utilize draw-gear 7 and the loop head of tab 8 to be measured to connect
Connect；
S302, the weight of counterweight 17 being stepped up in force measuring structure, incrementally increase the load value of tab 8 to be measured；
When S303, measurement tab 8 to be measured depart from aerostatics utricule 9, the load value of tab 8 to be measured.
Specifically, the step S3 of this tab load measuring method comprises the following steps：Force measuring structure 4 includes in the present embodiment
Pulley 16 and counterweight 17, draw-gear 7 use rope；Counterweight 17 is utilized into draw-gear 7, passes through pulley 16 and tab 8 to be measured
Loop head connection；The weight of counterweight 17 being stepped up in force measuring structure 4, incrementally increases the load value of tab 8 to be measured；When to be measured
When tab 8 departs from aerostatics utricule 9, according to the both ends equalising torque of draw-gear 7, torque equilibrium equation is established, is obtained now
The load value of tab 8 to be measured.
Specifically, if on draw-gear 7, the length of the loop head of tab 8 to be measured to pulley 16 is L1, the load value of tab to be measured 8
For F1；Counterweight 17 to the length of pulley 16 be L2, the load value of counterweight 17 be F2；The weight of counterweight 17 is stepped up, until making drawing to be measured
Loop 8 departs from aerostatics utricule 9.According to the both ends equalising torque of draw-gear 7, torque equilibrium equation F1*L1=F2*L2 is established,
In the case of known F2, L2, L1, F1 is obtained, when obtaining tab 8 to be measured with the disengaging of aerostatics utricule 9, tab 8 to be measured is held
Force value.
The utility model provides a kind of tab load measurement apparatus, by the way that tab 8 to be measured is fixed on into aerostatics utricule 9
On, simulate under true measuring environment, gas pressure loads of the tab 8 to be measured by aerostatics utricule 9；Tab 8 to be measured is measured with floating
When pocket utricule 9 departs from, the load value of tab 8 to be measured realizes that true, to accurately measure tab 8 to be measured real on aerostatics
Load value in the use of border.
Preferred embodiment of the present utility model is these are only, it is all in this practicality not to limit the utility model
Within new spirit and principle, any modification, equivalent substitution and improvements made etc., guarantor of the present utility model should be included in
Within the scope of shield.
Claims (8)
- A kind of 1. tab load measurement apparatus, it is characterised in that including：Tab, aerostatics utricule and plane inflation structure to be measured, The tab to be measured is fixed on the aerostatics utricule；The aerostatics utricule is arranged in the plane inflation structure, institute State aerostatics utricule and form inflatable closing space with the plane inflation structure.
- 2. a kind of tab load measurement apparatus according to claim 1, it is characterised in that the tab to be measured passes through sanction The mode cut, sew or welded, it is fixed on the aerostatics utricule.
- A kind of 3. tab load measurement apparatus according to claim 1, it is characterised in that the shape of the tab to be measured For：V-type tab, I types tab or double V-shaped tab.
- 4. a kind of tab load measurement apparatus according to claim 1, it is characterised in that described also including gas storage part Plane inflation structure is provided with inflation inlet；The gas storage part is connected with the inflation inlet, and by the inflation inlet to described Inflatable body in the inflatable closing space that aerostatics utricule is formed with the plane inflation structure；The gas includes：Air, Helium or nitrogen.
- 5. a kind of tab load measurement apparatus according to claim 1, it is characterised in that also including support, the plane Inflation structure is fixed on the bracket.
- 6. a kind of tab load measurement apparatus according to claim 1, it is characterised in that described also including force measuring structure Force measuring structure includes pulley and counterweight；The counterweight utilizes draw-gear, is connected by the pulley with the tab to be measured.
- 7. a kind of tab load measurement apparatus according to claim 4, it is characterised in that also including differential pressure pickup and work Control machine, the industrial computer electrically connect with the differential pressure pickup and the gas storage part respectively；In the plane inflation structure also Provided with pressure difference mouth, the differential pressure pickup is connected with the pressure difference mouth；The industrial computer controls institute by the differential pressure pickup State gas storage part.
- A kind of 8. tab load measurement apparatus according to claim any one of 1-7, it is characterised in that the plane inflation Structure also includes disc base and flange circle, and the aerostatics utricule is fixed between the disc base and the flange circle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721233123.5U CN207180923U (en) | 2017-09-25 | 2017-09-25 | A kind of tab load measurement apparatus |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721233123.5U CN207180923U (en) | 2017-09-25 | 2017-09-25 | A kind of tab load measurement apparatus |
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| CN207180923U true CN207180923U (en) | 2018-04-03 |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107727289A (en) * | 2017-09-25 | 2018-02-23 | 中国科学院光电研究院 | A kind of tab load measurement apparatus and method |
| CN111006805A (en) * | 2019-11-15 | 2020-04-14 | 北京空间机电研究所 | Device and method for measuring residual gas vacuum expansion force in space inflatable structure package |
| CN113218614A (en) * | 2021-05-21 | 2021-08-06 | 湘潭大学 | Device and method for testing performance of aerostat capsule pull tab |
| CN113984517A (en) * | 2021-07-28 | 2022-01-28 | 湘潭大学 | Capsule puller performance testing device |
| CN107727289B (en) * | 2017-09-25 | 2024-08-02 | 中国科学院光电研究院 | Device and method for measuring tab bearing force |
-
2017
- 2017-09-25 CN CN201721233123.5U patent/CN207180923U/en active Active
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107727289A (en) * | 2017-09-25 | 2018-02-23 | 中国科学院光电研究院 | A kind of tab load measurement apparatus and method |
| CN107727289B (en) * | 2017-09-25 | 2024-08-02 | 中国科学院光电研究院 | Device and method for measuring tab bearing force |
| CN111006805A (en) * | 2019-11-15 | 2020-04-14 | 北京空间机电研究所 | Device and method for measuring residual gas vacuum expansion force in space inflatable structure package |
| CN111006805B (en) * | 2019-11-15 | 2021-06-11 | 北京空间机电研究所 | Device and method for measuring residual gas vacuum expansion force in space inflatable structure package |
| CN113218614A (en) * | 2021-05-21 | 2021-08-06 | 湘潭大学 | Device and method for testing performance of aerostat capsule pull tab |
| CN113218614B (en) * | 2021-05-21 | 2022-04-22 | 湘潭大学 | Device and method for testing performance of aerostat capsule pull tab |
| CN113984517A (en) * | 2021-07-28 | 2022-01-28 | 湘潭大学 | Capsule puller performance testing device |
| CN113984517B (en) * | 2021-07-28 | 2024-01-09 | 湘潭大学 | Bag body tab performance testing device |
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