CN109029967A - A kind of strength test device for aerostatics connector - Google Patents
A kind of strength test device for aerostatics connector Download PDFInfo
- Publication number
- CN109029967A CN109029967A CN201811157262.3A CN201811157262A CN109029967A CN 109029967 A CN109029967 A CN 109029967A CN 201811157262 A CN201811157262 A CN 201811157262A CN 109029967 A CN109029967 A CN 109029967A
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- pulley
- fixed
- strength test
- test
- rack
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M13/00—Testing of machine parts
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N3/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N3/02—Details
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N3/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N3/08—Investigating strength properties of solid materials by application of mechanical stress by applying steady tensile or compressive forces
- G01N3/10—Investigating strength properties of solid materials by application of mechanical stress by applying steady tensile or compressive forces generated by pneumatic or hydraulic pressure
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- General Physics & Mathematics (AREA)
- Health & Medical Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Chemical & Material Sciences (AREA)
- Analytical Chemistry (AREA)
- Biochemistry (AREA)
- General Health & Medical Sciences (AREA)
- Immunology (AREA)
- Pathology (AREA)
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
Abstract
The invention belongs to aerostatics to test field, and in particular to a kind of strength test device for aerostatics connector.There is presently no the Special testing devices dedicated for aerostatics typical case's connector strength test.The purpose of the present invention is to change the disadvantages of occupied ground is big, installation effectiveness is low, the test period is long, poor repeatability in existing test method.Fixed module is strained and fixed to the edge of base fabric on fixed rack；Different location at the fixed rack edge is additionally provided with horizontal addload pulley；Pulley guide rails are fixed on the top of fixed rack by load rack by loading module, equipped with moveable vertical load pulley in pulley guide rails；The loading module also has cylinder, and hawser one end is connect with the cylinder；The other end is connected by load pulley with cloth is connect.The automation for realizing test installation and load, is greatly improved test efficiency.The experimental rig is all carried out automatically controlling using program from load is installed to, test efficiency is greatly improved.
Description
Technical field
The invention belongs to aerostatics to test field, and in particular to a kind of strength test device for aerostatics connector.
Background technique
Have a large amount of typical connector on aerostatics, such as the bowknot form that the connection of hawser and utricule uses, keel with
The cloth set form etc. that utricule connection uses.These typical connectors must pass through strength test on ground.It is making a strength test
When, for simulation truth and meet correlation test standard, testpieces base fabric is subjected to twin shaft tensioning, and to meet different angles
The load requirement of degree and different rates.This just needs one kind that can quickly be tensioned testpieces and can satisfy different angle adduction
The experimental rig that different rates load requires, there is presently no the dedicated examinations dedicated for aerostatics typical case's connector strength test
Experiment device, existing test method is all made of to be tested in load track, and occupied ground is big, needs to reinstall before test every time
Test fixture, testpieces tensioning are carried out by the way of manual tension, and poor repeatability, installation effectiveness is lower, and the test period is longer.
Summary of the invention
The purpose of the present invention is to change, occupied ground is big, installation effectiveness is low, the test period is long, again in existing test method
The disadvantages of renaturation is poor.Improve aerostatics typical case connector Strength Testing Methods.
A kind of strength test device for aerostatics connector, for the connection to being made of base fabric and connection cloth hot weld
Part carries out peeling strength test, which includes the fixed module of bottom and the loading module on top, wherein
The fixed module is strained and fixed to the edge of base fabric on fixed rack；Difference at the fixed rack edge
Position is additionally provided with horizontal addload pulley；
Pulley guide rails are fixed on the top of fixed rack by load rack by the loading module, are filled in pulley guide rails
There is moveable vertical load pulley；The loading module also has cylinder, and hawser one end is connect with the cylinder；
When applying horizontal direction pulling force to connection cloth, the hawser other end connects by horizontal addload pulley with cloth is connect
It connects；When to cloth application vertical direction pulling force is connected, the hawser other end is connected by vertical load pulley with cloth is connect.
The fixed module has several dovetail groove guide rails of horizontal and vertical distribution, and a pair of lateral T-type card slot is removable
It is mounted on longitudinal dovetail groove guide rail dynamicly, a pair of longitudinal T-type card slot is movably mounted at lateral dovetail groove guide rail
On, four edges of T-type card slot and base fabric connect；On the fixed rack also transversely and be longitudinally provided with ball-screw and
Corresponding servo motor, ball-screw have opposite thread rotary orientation in two sides, are threadedly coupled respectively with corresponding T-type card slot.
The horizontal addload pulley includes that first pulley, second pulley and third pulley, wherein second pulley and third are sliding
It takes turns the two sides in square edge and moves.
The vertical load pulley includes above the 4th pulley and connection cloth of its positioning action, is fixed in pulley guide rails
The 6th pulley.
The fixed rack and load rack all have adjustable support leg.
The servo motor is connect by retarder with ball-screw.
The utility model has the advantages that
1, the experimental rig can auto-tensioning testpieces as required, it is quick for installation, it is easily operated；Using conventional approach into
When row aerostatics typical case's connector strength test, testpieces is tensioned by the way of manually adjusting, complicated for operation, efficiency
Lowly, and there is no Special test rack, since the randomness installed every time causes test repeatability poor.The experimental rig passes through
The ball-screw of transverse and longitudinal both direction adds servo motor and control program, realizes the auto-tensioning of testpieces, quick for installation, easily
It is reproducible in operation.
2, the experimental rig can be realized the tensioning of twin shaft fast quantification；The experimental rig on mounting plane by being arranged phase
Mutually vertical twin shaft tensioning apparatus, may be implemented the tensile force synchronous tension on planar biaxially oriented by setting, preferably
Applying working condition under simulation test piece installation state.
3, the experimental rig can satisfy testpieces of different sizes, universal relatively strong；The experimental rig can meet centainly
The test demand of different size testpieces in range.
4, the experimental rig can satisfy the load demand of different angle；The experimental rig can be quickly real by pulley system
The demand of existing multi-angle load.
5, it is adjustable to can be realized loading speed for the experimental rig；The experimental rig is by process control for the electronic of load
Cylinder meets requirement of the testing standard to loading speed, it can be achieved that rate of extension accurately controls.
6, the experimental rig can be automatically controled, and realizes the automation of test installation and load, test efficiency is greatly improved.
The experimental rig is all carried out automatically controlling using program from load is installed to, test efficiency is greatly improved.
Detailed description of the invention
Fig. 1 is the isometric side view of experimental rig of the present invention；
Fig. 2 is the isometric side view of fixed module；
Fig. 3 is the isometric side view of loading module.
1-base fabric；2-fixed racks；3-dovetail groove guide rails；4-T-type card slots；5-ball-screws；6-servo motors；
7-first pulleys；8-second pulleys；9-third pulleys；10- adjustable support leg；11-retarders；12-load racks；13—
Pulley guide rails；14-cylinders；15-the four pulley；16-the five pulley；17-the six pulley；18- connection cloth
Specific embodiment
Testpieces is fixed and is tensioned by testing fixed module when test, by test loading module to testpieces
It is loaded, entire experimental rig is self-balance structure, without additionally constraining it.
A kind of strength test device for aerostatics connector, for being constituted to by base fabric 1 and connection cloth 18 hot weld
Connector carries out peeling strength test, which includes the fixed module of bottom and the loading module on top, wherein
The fixed module is strained and fixed to the edge of base fabric 1 on fixed rack 2；At 2 edge of fixed rack
Different location is additionally provided with horizontal addload pulley；
The top that pulley guide rails 13 are fixed on fixed rack 2 by loading rack 12 by the loading module, leads in pulley
Equipped with moveable vertical load pulley on rail 13；The loading module also has cylinder 14, hawser one end and the cylinder
14 connections；
When to connection cloth 18 apply horizontal direction pulling force when, the hawser other end by horizontal addload pulley with connect cloth
18 connections；When applying vertical direction pulling force to connection cloth 18, the hawser other end by vertical load pulley with connect cloth
18 connections.
The fixed module has several dovetail groove guide rails 3 of horizontal and vertical distribution, and a pair of lateral T-type card slot 4 can
It removably mounts on longitudinal dovetail groove guide rail 3, a pair of longitudinal T-type card slot 4 is movably mounted at lateral dovetail groove
On guide rail 3, T-type card slot 4 is connect with four edges of base fabric 1；Also transversely and rolling is longitudinally provided on the fixed rack 2
Ballscrew 5 and corresponding servo motor 6, ball-screw 5 two sides have opposite thread rotary orientation, respectively with corresponding T-type card
Slot 4 is threadedly coupled.
The horizontal addload pulley includes first pulley 7, second pulley 8 and third pulley 9, wherein second pulley 8 and
Three pulleys 9 are in the two sides of square edge and removable.
The vertical load pulley includes 18 top of the 4th pulley 15 and connection cloth of its positioning action, is fixed on pulley and leads
The 6th pulley 17 on rail 13.
The fixed rack 2 and load rack 12 all have adjustable support leg 10.
The servo motor 6 is connect by retarder 11 with ball-screw 5.
The device is successfully applied in Multiple Type aerostatics typical case's connector strength test, and test effect is greatly improved
Rate demonstrates the bearing capacity of various typical connectors.
Claims (6)
1. a kind of strength test device for aerostatics connector, for being constituted to by base fabric (1) and connection cloth (18) hot weld
Connector carry out peeling strength test, it is characterised in that: the device includes the fixed module of bottom and the loading module on top,
Wherein
The fixed module is strained and fixed to the edge of base fabric (1) on fixed rack (2)；At the fixed rack (2) edge
Different location be additionally provided with horizontal addload pulley；
The top that pulley guide rails (13) are fixed on fixed rack (2) by loading rack (12) by the loading module, in pulley
Equipped with moveable vertical load pulley on guide rail (13)；The loading module also has cylinder (14), hawser one end with it is described
Cylinder (14) connection；
When to connection cloth (18) apply horizontal direction pulling force when, the hawser other end by horizontal addload pulley with connect cloth
(18) it connects；When applying vertical direction pulling force to connection cloth (18), the hawser other end is by vertical load pulley and company
Connect cloth (18) connection.
2. strength test device according to claim 1, it is characterised in that: the fixed module has horizontal and vertical point
Several dovetail groove guide rails (3) of cloth, a pair of lateral T-type card slot (4) are movably mounted at longitudinal dovetail groove guide rail (3)
On, a pair of longitudinal T-type card slot (4) is movably mounted on lateral dovetail groove guide rail (3), T-type card slot (4) and base fabric
(1) four edges connection；Also transversely and ball-screw (5) and corresponding is longitudinally provided on the fixed rack (2)
Servo motor (6), ball-screw (5) have opposite thread rotary orientation in two sides, connect respectively with corresponding T-type card slot (4) screw thread
It connects.
3. strength test device according to claim 2, it is characterised in that: the horizontal addload pulley includes first pulley
(7), second pulley (8) and third pulley (9), wherein second pulley (8) and third pulley (9) square edge two sides and can
It is mobile.
4. strength test device according to claim 3, it is characterised in that: the vertical load pulley includes that its positioning is made
Above 4th pulley (15) and connection cloth (18), the 6th pulley (17) that is fixed on pulley guide rails (13).
5. strength test device according to claim 4, it is characterised in that: the fixed rack (2) and load rack
(12) all there are adjustable support leg (10).
6. strength test device according to claim 5, it is characterised in that: the servo motor (6) passes through retarder
(11) it is connect with ball-screw (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811157262.3A CN109029967B (en) | 2018-09-30 | 2018-09-30 | A strength test device for aerostatics connecting piece |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811157262.3A CN109029967B (en) | 2018-09-30 | 2018-09-30 | A strength test device for aerostatics connecting piece |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109029967A true CN109029967A (en) | 2018-12-18 |
| CN109029967B CN109029967B (en) | 2020-06-09 |
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ID=64615828
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811157262.3A Active CN109029967B (en) | 2018-09-30 | 2018-09-30 | A strength test device for aerostatics connecting piece |
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| Country | Link |
|---|---|
| CN (1) | CN109029967B (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110361187A (en) * | 2019-08-21 | 2019-10-22 | 合肥工业大学 | A kind of flexible structure test pneumatic load test device |
| CN112067332A (en) * | 2020-08-28 | 2020-12-11 | 合肥工业大学 | Experimental concentrated force loading test device of airship flexible structure |
| CN112326436A (en) * | 2020-10-29 | 2021-02-05 | 合肥工业大学 | Device and method for testing mechanical properties of inner curtain cloth assembly of airship |
| CN113232889A (en) * | 2021-06-11 | 2021-08-10 | 湖南航天远望科技有限公司 | Aerostat capsule soft accessory test system and test method |
| CN113494996A (en) * | 2020-04-07 | 2021-10-12 | 中国航天科工飞航技术研究院（中国航天海鹰机电技术研究院） | A intensity test system for suspending induction system |
| CN113494995A (en) * | 2020-04-07 | 2021-10-12 | 中国航天科工飞航技术研究院（中国航天海鹰机电技术研究院） | A intensity test system for suspending induction system |
Citations (4)
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| DE102011017564A1 (en) * | 2011-04-26 | 2012-10-31 | Aerospy Sense & Avoid Technology Gmbh | Method and system for inspecting a surface for material defects |
| CN102829988A (en) * | 2012-08-13 | 2012-12-19 | 清华大学 | Testing device for vertical and continuous loading at optional position of numerical control moving table |
| CN103913285A (en) * | 2012-12-31 | 2014-07-09 | 北京建筑工程学院 | Device for testing mechanical properties |
| CN105806718A (en) * | 2016-03-08 | 2016-07-27 | 中国地质大学（武汉） | Structural surface direct shear test device for accurately controlling normal stress application process |
-
2018
- 2018-09-30 CN CN201811157262.3A patent/CN109029967B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102011017564A1 (en) * | 2011-04-26 | 2012-10-31 | Aerospy Sense & Avoid Technology Gmbh | Method and system for inspecting a surface for material defects |
| CN102829988A (en) * | 2012-08-13 | 2012-12-19 | 清华大学 | Testing device for vertical and continuous loading at optional position of numerical control moving table |
| CN103913285A (en) * | 2012-12-31 | 2014-07-09 | 北京建筑工程学院 | Device for testing mechanical properties |
| CN105806718A (en) * | 2016-03-08 | 2016-07-27 | 中国地质大学（武汉） | Structural surface direct shear test device for accurately controlling normal stress application process |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110361187A (en) * | 2019-08-21 | 2019-10-22 | 合肥工业大学 | A kind of flexible structure test pneumatic load test device |
| CN113494996A (en) * | 2020-04-07 | 2021-10-12 | 中国航天科工飞航技术研究院（中国航天海鹰机电技术研究院） | A intensity test system for suspending induction system |
| CN113494995A (en) * | 2020-04-07 | 2021-10-12 | 中国航天科工飞航技术研究院（中国航天海鹰机电技术研究院） | A intensity test system for suspending induction system |
| CN112067332A (en) * | 2020-08-28 | 2020-12-11 | 合肥工业大学 | Experimental concentrated force loading test device of airship flexible structure |
| CN112326436A (en) * | 2020-10-29 | 2021-02-05 | 合肥工业大学 | Device and method for testing mechanical properties of inner curtain cloth assembly of airship |
| CN113232889A (en) * | 2021-06-11 | 2021-08-10 | 湖南航天远望科技有限公司 | Aerostat capsule soft accessory test system and test method |
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| Publication number | Publication date |
|---|---|
| CN109029967B (en) | 2020-06-09 |
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