CN105004521B - It is a kind of to be used for the device of aircraft quick-detachable lock durability and slow test - Google Patents
It is a kind of to be used for the device of aircraft quick-detachable lock durability and slow test Download PDFInfo
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- CN105004521B CN105004521B CN201510506820.2A CN201510506820A CN105004521B CN 105004521 B CN105004521 B CN 105004521B CN 201510506820 A CN201510506820 A CN 201510506820A CN 105004521 B CN105004521 B CN 105004521B
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Abstract
The present invention relates to a kind of for aircraft quick-detachable lock durability and the device of slow test, clamped one time is easy to operate, and test efficiency and measuring accuracy are high.On main base multiple main base hole clippings are provided with along X-direction；Rotating disk is rotatably connected on support for rotary disc；Multiple turret apertures are provided with rotating disk；On Mobile base Mobile base neck is provided with along Y direction；Lower rotation seat is rotatably installed on Mobile base；Upper rotation seat is rotatably installed on lower rotation seat；Mounting bracket neck is connected with upper rotation seat；Connecting rod is rotatably installed on mounting bracket；Driver slot and connecting rod fixing hole are provided with drive rod；Driver slot is connected with rotating disk pin slide；Connecting rod fixing hole is multiple, along the axially arranged of drive rod；A number reference test bar and No. two reference test bars are arranged in connecting rod；The bottom of a number reference test bar and No. two reference test bars is located at the top of installation cavity；A number reference test bar and No. two reference test bars are located at the both sides of the rotation axis of connecting rod respectively.
Description
Technical field
The present invention relates to a kind of for aircraft quick-detachable lock durability and the device of slow test.
Background technology
Aircraft quick-detachable lock is a kind of lockset on aircraft, such as the Chinese patent institute of Application No. 201310145260.3
Show.Aircraft quick-detachable lock needs to carry out durability and slow test, and prior art needs two covering devices when being tested, and one packs into
Row endurancing, a set of carry out slow test, thus will clamping repeatedly, operate it is out of the ordinary just, and experiment can be influenceed to imitate
Rate and measuring accuracy.
The content of the invention
It is an object of the invention to overcome above shortcomings in the prior art, and provide a kind of reasonable in design
For aircraft quick-detachable lock durability and the device of slow test, clamped one time is easy to operate, and test efficiency and measuring accuracy are high.
The present invention the used technical scheme that solves the above problems is：One kind is used for aircraft quick-detachable lock durability and static(al) is tried
The device tested, the X-axis of the space coordinates of the device, Y-axis, Z axis setting are as follows：With from the point of view of the facing of the device, X-axis horizontal pendulum
Put, in the lateral direction；Y-axis level is put, and points to fore-and-aft direction；Z axis vertical display, points to above-below direction；
It is characterized in that：Described device includes main base, rotating disk mechanism, mechanism for testing and position adjusting mechanism；
Rotating disk mechanism includes rotating disk, support for rotary disc, electric machine support and rotating disk bearing pin；It is provided with main base along X-direction many
Individual main base hole clipping, support for rotary disc can be connected from different main base hole clippings；Rotating disk is rotatably connected on support for rotary disc, its
Rotation axis is along Y direction；Multiple turret apertures, the distance not all phase of the rotation axis of turret apertures to rotating disk are provided with rotating disk
Deng rotating disk bearing pin can be connected from different turret apertures；
Position adjusting mechanism includes Mobile base, lower rotation seat and upper rotation seat；On Mobile base Mobile base is provided with along Y direction
Neck, Mobile base neck is connected with main base；Lower rotation seat is rotatably installed on Mobile base, and its rotation axis is along X-axis side
To；Upper rotation seat is rotatably installed on lower rotation seat, and its rotation axis is along Z-direction；Installation cavity and work are provided with upper rotation seat
Part fixing hole；
Mechanism for testing includes drive rod, connecting rod, a reference test bar, No. two reference test bars and mounting bracket；Along Z axis on mounting bracket
Direction is provided with mounting bracket neck, and mounting bracket neck is connected with upper rotation seat；Connecting rod is rotatably installed on mounting bracket, and it revolves
Shaft axis are along Y direction；Driver slot and connecting rod fixing hole are provided with drive rod；Driver slot is connected with rotating disk pin slide；Even
Extension bar fixing hole is multiple, and along the axially arranged of drive rod, connecting rod can be connected from different connecting rod fixing holes；No. one
Reference test bar and No. two reference test bars are arranged in connecting rod, and both arrange along X-direction；The bottom of a number reference test bar and No. two reference test bars
Portion is located at the top of installation cavity；A number reference test bar and No. two reference test bars are located at the both sides of the rotation axis of connecting rod respectively.
Position adjusting mechanism of the present invention also includes rotary shaft；Lower rotation seat is rotatably installed in Mobile base with rotary shaft
On, rotary shaft is set along X-direction.
Workpiece fixing hole of the present invention is multiple, is set along Z-direction.
The present invention compared with prior art, with advantages below and effect：Reasonable in design, it is only necessary to this hair
It is bright, and clamping once can be carried out lock durability and slow test, easy to operate, test efficiency and measuring accuracy are high.
Brief description of the drawings
Fig. 1 is the A-A cross section structure diagrams faced cross section structure diagram, be also Fig. 4 of the embodiment of the present invention.
Fig. 2 is the left view structural representation of the embodiment of the present invention.
Fig. 3 is the backsight structural representation of the embodiment of the present invention.
Fig. 4 is the overlooking the structure diagram of the embodiment of the present invention.
Fig. 5 regards cross section structure diagram for the right side of the embodiment of the present invention, is also Fig. 4 B-B cross section structure diagrams.
Fig. 6 is the dimensional structure diagram of the embodiment of the present invention.
Embodiment
Below in conjunction with the accompanying drawings and the present invention is described in further detail by embodiment, following examples are to this hair
Bright explanation and the invention is not limited in following examples.
Referring to Fig. 1~Fig. 6, the embodiment of the present invention includes main base 1, rotating disk mechanism 2, mechanism for testing 3 and position adjustment machine
Structure 4.
The X-axis of the space coordinates of the device, Y-axis, Z axis setting are as follows：With facing for the device（That is Fig. 1）From the point of view of, X-axis
Level is put, in the lateral direction；Y-axis level is put, and points to fore-and-aft direction；Z axis vertical display, points to above-below direction.
Rotating disk mechanism 2 includes rotating disk 21, support for rotary disc 22, electric machine support 23 and rotating disk bearing pin 24.
On main base 1 multiple main base hole clippings are provided with along X-direction.Support for rotary disc 22 can connect from different main base hole clippings
Fixation is connect, position of the support for rotary disc 22 on main base 1 can be so adjusted.
Rotating disk 21 is rotatably connected on support for rotary disc 22, and its rotation axis is along Y direction, and such rotating disk 21 is in support for rotary disc
It can be rotated on 22 around Y-axis.Multiple turret apertures 211, the distance of the rotation axis of turret apertures 211 to rotating disk 21 are provided with rotating disk 21
Not all equal, rotating disk bearing pin 24 can be connected from different turret apertures 211, can so adjust rotating disk bearing pin 24 in rotating disk 21
On position.
Position adjusting mechanism 4 includes Mobile base 41, lower rotation seat 42, rotary shaft 43 and upper rotation seat 44.
Mobile base neck 411 is provided with along Y direction on Mobile base 41, Mobile base neck 411 is connected with main base 1
It is fixed so that Mobile base 41 is fixed on main base 1, and by the position between Mobile base neck 411 and bolt, Mobile base 41 exists
Position on main base 1 can be adjusted along Y direction.
Lower rotation seat 42 is rotatably installed on Mobile base 41 with rotary shaft 43, and rotary shaft 43 is set along X-direction, i.e., lower turn
The rotation axis of dynamic seat 42 so descends rotation seat 42 to be rotated on Mobile base 41 around X-axis, can so adjusted along X-direction
The position on Mobile base 41 of rotation seat 42.
Upper rotation seat 44 is rotatably installed on lower rotation seat 42, and its rotation axis is along Z-direction, and such upper rotation seat 44 exists
It can about the z axis be rotated on lower rotation seat 42, can so adjust position of the upper rotation seat 44 on lower rotation seat 42.
Installation cavity 451 and workpiece fixing hole 452, installation cavity 451 and the phase of workpiece fixing hole 452 are provided with upper rotation seat 44
It is logical.
Installation cavity 451 is used for laying quick-detachable lock.
Workpiece fixing hole 452 is used for installing the fixing bolt of quick-detachable lock, and quick-detachable lock is fixedly clamped in peace by the fixing bolt
It behave affectedly in 451.Workpiece fixing hole 452 is multiple, is set along Z-direction, is so suitable for the quick-detachable lock of different size.
Mechanism for testing 3 includes drive rod 31, connecting rod 32, reference test bar 33a, a No. two reference test bar 33b and mounting bracket 34.
Mounting bracket neck 341 is provided with along Z-direction on mounting bracket 34, mounting bracket neck 341 uses bolt with upper rotation seat 44
It is connected so that mounting bracket 34 is fixed in upper rotation seat 44, passes through the position between mounting bracket neck 341 and bolt, peace
Shelving 34 positions in upper rotation seat 44 can be adjusted along Z-direction.
Connecting rod 32 is rotatably installed on mounting bracket 34, and its rotation axis is along Y direction, and such connecting rod 32 is in mounting bracket
It can be rotated on 34 around Y-axis.
Driver slot 311 and connecting rod fixing hole 312 are provided with drive rod 31.
Driver slot 311 is slidably connected with rotating disk bearing pin 24.
Connecting rod fixing hole 312 is multiple, along the axially arranged of drive rod 31.Connecting rod 32 can be solid from different connecting rods
Determine hole 312 to be connected, can so adjust position of the connecting rod 32 on drive rod 31.
A number reference test bar 33a and No. two reference test bar 33b are arranged in connecting rod 32, and both arrange along X-direction.A number survey
Bar 33a and No. two reference test bar 33b bottom are located at the top of installation cavity 451.A number reference test bar 33a and No. two reference test bar 33b
It is located at the both sides of the rotation axis of connecting rod 32 respectively, such connecting rod 32 is when mounting bracket 34 is rotated, similar to lever, No. one
Reference test bar 33a and No. two reference test bar 33b are located at the two ends of lever.
When carrying out durability test, quick-detachable lock is placed in installation cavity 451, large and small lock collar is upward.By consolidating for quick-detachable lock
Determine bolt to put into workpiece fixing hole 452, quick-detachable lock is fixedly clamped in installation cavity 451 by the fixing bolt.Under adjusting respectively
The position of position and upper rotation seat 44 on lower rotation seat 42 on Mobile base 41 of rotation seat 42 so that the large and small lock of quick-detachable lock
Disk is vertical upward, and the large and small lock collar stress of such quick-detachable lock is downwards, Pass Test requires；Support for rotary disc is adjusted respectively
Position of position, mounting bracket 34 of 22 position, connecting rod 32 on main base 1 on drive rod 31 in upper rotation seat 44,
Position of the Mobile base 41 on main base 1 so that a reference test bar 33a and No. two reference test bar 33b respectively positioned at quick-detachable lock it is big,
The surface of small lock collar；Adjust 24 position on rotating disk 21 of rotating disk bearing pin so that the rotational angle of connecting rod 32 meets the requirements.
By the motor with counter on the electric machine support 23, motor driving rotating disk 21 carries out rotating and reverse repeatedly, rotating disk 21
Driving drive rod 31 is rotated, and such connecting rod 32 carries out rotating and reverse repeatedly on mounting bracket 34, a reference test bar 33a and
No. two reference test bar 33b just promote the large and small lock collar of quick-detachable lock respectively, have thus carried out durability test.General test 1500
It is secondary.
When the large and small lock collar of quick-detachable lock is arranged in installation cavity 451, and it is vertical upward after, slow test can also be carried out.
Dismantle mechanism for testing 3, slow test is carried out to the large and small lock collar of quick-detachable lock with static test device.
Furthermore, it is necessary to explanation, the specific embodiment described in this specification, is named the shape of its parts and components
Title etc. can be different, and the above content described in this specification is only to structure example explanation of the present invention.
Claims (3)
1. it is a kind of for aircraft quick-detachable lock durability and the device of slow test, the X-axis of the space coordinates of the device, Y-axis, Z
Axle setting is as follows：So that from the point of view of the facing of the device, X-axis level is put, in the lateral direction；Y-axis level is put, and points to front and back
To；Z axis vertical display, points to above-below direction；
It is characterized in that：Described device includes main base, rotating disk mechanism, mechanism for testing and position adjusting mechanism；
Rotating disk mechanism includes rotating disk, support for rotary disc, electric machine support and rotating disk bearing pin；On main base multiple masters are provided with along X-direction
Base hole clipping, support for rotary disc can be connected from different main base hole clippings；Rotating disk is rotatably connected on support for rotary disc, and it rotates
Axis is along Y direction；Multiple turret apertures are provided with rotating disk, the distance of the rotation axis of turret apertures to rotating disk is not all equal, turned
Disk bearing pin can be connected from different turret apertures；
Position adjusting mechanism includes Mobile base, lower rotation seat and upper rotation seat；On Mobile base Mobile base card is provided with along Y direction
Groove, Mobile base neck is connected with main base；Lower rotation seat is rotatably installed on Mobile base, and its rotation axis is along X-direction；
Upper rotation seat is rotatably installed on lower rotation seat, and its rotation axis is along Z-direction；Installation cavity and workpiece are provided with upper rotation seat
Fixing hole；
Mechanism for testing includes drive rod, connecting rod, a reference test bar, No. two reference test bars and mounting bracket；Along Z-direction on mounting bracket
Mounting bracket neck is provided with, mounting bracket neck is connected with upper rotation seat；Connecting rod is rotatably installed on mounting bracket, its rotary shaft
Line is along Y direction；Driver slot and connecting rod fixing hole are provided with drive rod；Driver slot is connected with rotating disk pin slide；Connecting rod
Fixing hole is multiple, and along the axially arranged of drive rod, connecting rod can be connected from different connecting rod fixing holes；A number test
Bar and No. two reference test bars are arranged in connecting rod, and both arrange along X-direction；The bottom position of a number reference test bar and No. two reference test bars
In the top of installation cavity；A number reference test bar and No. two reference test bars are located at the both sides of the rotation axis of connecting rod respectively.
2. it is according to claim 1 for aircraft quick-detachable lock durability and the device of slow test, it is characterised in that：It is described
Position adjusting mechanism also include rotary shaft；Lower rotation seat is rotatably installed on Mobile base with rotary shaft, and rotary shaft is along X-direction
Set.
3. it is according to claim 1 for aircraft quick-detachable lock durability and the device of slow test, it is characterised in that：It is described
Workpiece fixing hole to be multiple, set along Z-direction.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510506820.2A CN105004521B (en) | 2015-08-18 | 2015-08-18 | It is a kind of to be used for the device of aircraft quick-detachable lock durability and slow test |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510506820.2A CN105004521B (en) | 2015-08-18 | 2015-08-18 | It is a kind of to be used for the device of aircraft quick-detachable lock durability and slow test |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105004521A CN105004521A (en) | 2015-10-28 |
| CN105004521B true CN105004521B (en) | 2017-08-25 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201510506820.2A Active CN105004521B (en) | 2015-08-18 | 2015-08-18 | It is a kind of to be used for the device of aircraft quick-detachable lock durability and slow test |
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Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107084834B (en) * | 2017-04-21 | 2019-03-26 | 西北工业大学 | It is able to achieve the uplock reliability test of lock ring lateral position adjustment |
| CN109946177B (en) * | 2019-04-04 | 2024-05-07 | 广东电网有限责任公司 | Test workpiece and test method for detecting wing-shaped card |
| CN114112272B (en) * | 2021-12-06 | 2024-04-05 | 信阳星宇航天标准件制造有限公司 | Vibration test tool for quick-release lock of sealing pin and mounting method of vibration test tool |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2008216160A (en) * | 2007-03-07 | 2008-09-18 | Sumitomo Precision Prod Co Ltd | Landing device testing apparatus of flying body and quick release mechanism |
| KR101245172B1 (en) * | 2011-10-13 | 2013-03-19 | (주) 코스텍 | Durability test apparatus for push-push latch |
| CN102865961A (en) * | 2012-09-17 | 2013-01-09 | 贵州航锐航空精密零部件制造有限公司 | Test method capable of improving accuracy of initial tension of quick-release lock |
| CN103698111B (en) * | 2013-11-22 | 2016-12-07 | 宁波拓普集团股份有限公司 | The straight line of a kind of tubing lining and testing torsional fatigue frock |
| CN104344950A (en) * | 2014-10-17 | 2015-02-11 | 中国航空综合技术研究所 | Small-size force bearing fast dismounting lock service life detection device |
| CN204924638U (en) * | 2015-08-18 | 2015-12-30 | 浙江国检检测技术有限公司 | A device that is used for aircraft quick -release lock durability and static test |
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Address after: 314300, 2 East Road, 211 salt North Road, Wuyuan street, Haiyan County, Zhejiang, Jiaxing Applicant after: ZHEJIANG GUOJIAN TESTING TECHNOLOGY CO., LTD. Address before: 314300, 2 East Road, 211 salt North Road, Wuyuan street, Haiyan County, Zhejiang, Jiaxing Applicant before: ZHEJIANG GUOJIAN TESTING TECHNOLOGY CO., LTD. |
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