CN206787954U - For detecting the detection device of aircraft skin coating shock resistance - Google Patents
For detecting the detection device of aircraft skin coating shock resistance Download PDFInfo
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- CN206787954U CN206787954U CN201720354943.3U CN201720354943U CN206787954U CN 206787954 U CN206787954 U CN 206787954U CN 201720354943 U CN201720354943 U CN 201720354943U CN 206787954 U CN206787954 U CN 206787954U
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- CN
- China
- Prior art keywords
- cavity
- detection device
- shock resistance
- workbench
- aircraft skin
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Abstract
The utility model discloses a kind of detection device for being used to detect aircraft skin coating shock resistance,Including workbench,Workbench left lower is provided with remote controllers,Connected between remote controllers and workbench by wire,Workbench top is provided with cavity,Cavity is cut into by integral compo pipe,Cylinder driver is provided with the right side of cavity,Cylinder driver and cavity are nested encryptions,Measuring head is provided with the right side of cylinder driver,Measuring head is that rivet welding is connected with cylinder driver,This kind is used for the detection device for detecting aircraft skin coating shock resistance,It is provided with remote control device,Considerably reduce the injury that may be brought in knockout process to staff,With greatly security,And overall construction design is relatively reasonable,And cost is relatively low,It is convenient for volume production,Device designs more firm in itself,It can be tested for a long time,And test result is more accurate,With very big application value.
Description
Technical field
Detection device technical field is the utility model is related to, is specially that one kind is used to detect aircraft skin coating impact resistance
The detection device of energy.
Background technology
Airplane dope manufacturer goes out new coating manufacture rear, it is necessary to which a kind of device enters to the shock resistance of coating
Row test, the anti corrosion test in terms of current existing device carries out some chemistry both for coating mostly are slight with some
The strength test of the artificial physics impact of intensity, this test can not draw the shock proof performance of the limit of material, and existing
The shock resistance test of some high intensity can cause the irregular large deformation of material mostly, be difficult to measure standard because deformation is uneven
Exact figures value.
So how to design a kind of detection device for being used to detect aircraft skin coating shock resistance, turn into us and work as
Before to solve the problems, such as.
Utility model content
The purpose of this utility model is to provide a kind of detection device for being used to detect aircraft skin coating shock resistance,
To solve the problems, such as that the degree of accuracy of the test proposed in above-mentioned background technology is not high.
To achieve the above object, the utility model provides following technical scheme：One kind resists for detecting aircraft skin coating
The detection device of impact property, including workbench, the workbench left lower are provided with remote controllers, the remote controllers
It is connected between the workbench by wire, the workbench top is provided with cavity, and the cavity is cut by integral compo pipe
Cut and be made, cylinder driver is provided with the right side of the cavity, the cylinder driver and the cavity are nested encryptions, described
Measuring head is provided with the right side of cylinder driver.
Further, motor is provided with the middle part of the cavity, the motor is into the motor is left by efficient electric mechanism
Side is to be connected by PLC control circuits, the PLC control circuits with the motor signal.
Further, some bearing shafts being provided with the downside of the cavity, the bearing shaft is made up of high-quality mild steel turning,
The cavity left lower is provided with pulley, and the pulley is that bolt is fixedly connected with the bearing shaft, is provided with the downside of the pulley
Track, the track are made up of cuts in metallic pipe, and track support is provided with the downside of the track.
Further, cavity is provided with the right side of the measuring head, the cavity is made up of sheet metal punching press, on the cavity
Portion is provided with some pressing blocks, and the pressing block is made up of heavy alloy turning, and the fast top of punching press is provided with optoelectronic induction
Device, the photoelectric sensor are that screw connection is fixed with the cavity.
Further, transmission line is provided with the top of the remote controllers, the transmission line is made up of high-quality copper cash, described
Remote controllers top is provided with display screen, and the display screen is made up of high-resolution liquid crystal screen, on the right side of the remote controllers
Bottom is provided with master switch, is provided with speed regulator on the left of the master switch, the speed regulator is made up of stepless time adjustment knob.
Compared with prior art, the beneficial effects of the utility model are：The device is while impact test is carried out, to keep away
Exempt from excessively deformation and cause the inaccuracy of measurement data, have also been devised and slow down the device of deformation and be easy to measure, and devise long-range
Remote control, the injury that may be brought in knockout process to staff is considerably reduced, there is greatly security；And
Overall construction design is relatively reasonable, and cost is relatively low, is convenient for volume production, facilitates the quick cost-recovering of manufacturer, device sheet
Body design is more firm, can be tested for a long time, and test result is more accurate, has very big application value.
Brief description of the drawings
Fig. 1 is the integrally-built schematic diagram of the utility model；
Fig. 2 is measuring head structural representation of the present utility model；
Fig. 3 is remote controllers structural representation of the present utility model；
In figure：1- cavitys；2- motors；3- workbench；4- bearing shafts；5-PLC control circuits；6- measuring heads；7- cylinders drive
Dynamic device；8- track supports；9- remote controllers；10- tracks；11- pulleys；12- cavitys；13- pressing blocks；14- optoelectronic inductions
Device；15- transmission lines；16- speed regulators；17- display screens；18- master switch.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole
Embodiment, based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belong to the scope of the utility model protection.
Fig. 1-3 are referred to, the utility model provides a kind of technical scheme：One kind is used to detect aircraft skin coating shock resistance
The detection device of performance, including workbench 3, the left lower of workbench 3 are provided with remote controllers 9, the remote controllers 9
It is connected between the workbench 3 by wire, the top of workbench 3 is provided with cavity 1, and the cavity 1 is by integral alloy
Pipe is cut into, will not be jagged, influences to use, and the right side of cavity 1 is provided with cylinder driver 7, the cylinder driving dress
It is nested encryptions that 7, which are put, with the cavity 1, and the right side of cylinder driver 7 is provided with measuring head 6, and the measuring head 6 can be right
Impact property is detected.
Further, the middle part of the cavity 1 is provided with motor 2, and the motor 2 is into the electricity by efficient electric mechanism
The left side of machine 2 is to be connected by PLC control circuits 5, the PLC control circuits 5 with the signal of motor 2, and then can be effectively and straight
The running of the controlled motor 2 connect.
Further, the downside of cavity 1 is provided with some bearing shafts 4, and the bearing shaft 4 is by high-quality mild steel turning system
Into the left lower of cavity 1 is provided with pulley 11, and the pulley 11 is that bolt is fixedly connected with the bearing shaft 4, the cunning
The downside of wheel 11 is provided with track 10, and the track 10 is made up of cuts in metallic pipe, and the downside of track 10 is provided with track support 8,
The track support 8 is that set weldering is connected with the track, is connected using set weldering mode, not only ensure that overall stabilization
Property, it also ensure that in test process and do not shift.
Further, the right side of measuring head 6 is provided with cavity 12, and the cavity 12 is made up of sheet metal punching press, described
The top of cavity 12 is provided with some pressing blocks 13, and the pressing block 13 is made up of heavy alloy turning, in the punching press fast 13
Portion is provided with photoelectric sensor 14, and the photoelectric sensor 14 is to be screwed to be connected with the cavity 1, is not only conveniently torn open
Unload, and will not hinder to run in a device.
Further, the top of remote controllers 9 is provided with transmission line 15, and the transmission line 15 is by high-quality copper cash system
Into the top of remote controllers 9 is provided with display screen 17, and the display screen 17 is made up of high-resolution liquid crystal screen, described remote
The lower right side of range controller 9 is provided with master switch 18, and the left side of master switch 18 is provided with speed regulator 16, the speed regulator 16 be by
Stepless speed regulation knob is made, and stepless speed regulation knob is adapted to various careful rate requests, and instruction is accurately passed to electricity
Machine 2, action effect is obvious.
Operation principle：First, the workbench 3 of device is placed in the broad interior conveniently tested, will participate in surveying
The right side for the measuring head 6 that the aircraft skin coating article of examination is placed on the right side of device and fixation, then tester hold long-range control
To safety zone, opening master switch 18 and adjusting speed regulator 16 to required speed, instruction can be reached device 9 processed by transmission line 15
Motor 2, motor 2 reach corresponding speed, drive bearing shaft 8 and cylinder driver 7, and then whole cavity 1 is transported on track 10
Dynamic to rush at object under test, air cylinder device, which excites, while reaching before object releases measuring head 6, when hitting object under test,
Pressing block 13, which is formed, to be destroyed, and the record of photoelectric sensor 14 hits the extent of damage, is difficult to measure in order to avoid object under test is badly deformed, recessed
Chamber 12 reduces destruction by way of increasing contact area, and photoelectric sensor 14 passes real-time monitoring data back remote controllers 9,
This detection device has the degree of accuracy of conspicuousness compared to legacy equipment, and reasonable in design, is convenient to tester and enters
Row is securely and reliably tested.
While there has been shown and described that embodiment of the present utility model, for the ordinary skill in the art,
It is appreciated that these embodiments can be carried out with a variety of changes in the case where not departing from principle of the present utility model and spirit, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (5)
1. a kind of detection device for being used to detect aircraft skin coating shock resistance, including workbench (3), it is characterised in that：
Workbench (3) left lower is provided with remote controllers (9), leads between the remote controllers (9) and the workbench (3)
Wire connection is crossed, workbench (3) top is provided with cavity (1), and the cavity (1) is cut into by integral compo pipe, institute
To state and cylinder driver (7) is provided with the right side of cavity (1), the cylinder driver (7) and the cavity (1) they are nested encryptions,
Measuring head (6) is provided with the right side of the cylinder driver (7).
2. a kind of detection device for being used to detect aircraft skin coating shock resistance according to claim 1, its feature
It is：Motor (2) is provided with the middle part of the cavity (1), the motor (2) is into the motor (2) is left by efficient electric mechanism
Side is to be connected by PLC control circuits (5), the PLC control circuits (5) with the motor (2) signal.
3. a kind of detection device for being used to detect aircraft skin coating shock resistance according to claim 1, its feature
It is：Some bearing shafts (4) are provided with the downside of the cavity (1), the bearing shaft (4) is made up of high-quality mild steel turning, institute
State cavity (1) left lower and be provided with pulley (11), the pulley (11) is that bolt is fixedly connected with the bearing shaft (4), described
Track (10) is provided with the downside of pulley (11), the track (10) is made up of cuts in metallic pipe, is provided with the downside of the track (10)
Track support (8).
4. a kind of detection device for being used to detect aircraft skin coating shock resistance according to claim 1, its feature
It is：Cavity (12) is provided with the right side of the measuring head (6), the cavity (12) is made up of sheet metal punching press, the cavity
(12) top is provided with some pressing blocks (13), and the pressing block (13) is made up of heavy alloy turning, the pressing block
(13) top is provided with photoelectric sensor (14), and the photoelectric sensor (14) and the cavity (1) are that screw connection is fixed.
5. a kind of detection device for being used to detect aircraft skin coating shock resistance according to claim 1, its feature
It is：Transmission line (15) is provided with the top of the remote controllers (9), the transmission line (15) is made up of high-quality copper cash, described
Remote controllers (9) top is provided with display screen (17), and the display screen (17) is made up of high-resolution liquid crystal screen, described long-range
Controller (9) lower right side is provided with master switch (18), and speed regulator (16), the speed regulator are provided with the left of the master switch (18)
(16) it is made up of stepless time adjustment knob.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720354943.3U CN206787954U (en) | 2017-04-06 | 2017-04-06 | For detecting the detection device of aircraft skin coating shock resistance |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720354943.3U CN206787954U (en) | 2017-04-06 | 2017-04-06 | For detecting the detection device of aircraft skin coating shock resistance |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206787954U true CN206787954U (en) | 2017-12-22 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720354943.3U Expired - Fee Related CN206787954U (en) | 2017-04-06 | 2017-04-06 | For detecting the detection device of aircraft skin coating shock resistance |
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| Country | Link |
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| CN (1) | CN206787954U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108044271A (en) * | 2018-01-11 | 2018-05-18 | 上海振华重工(集团)股份有限公司 | A kind of abnormity weight pound plate automatic turning-over device |
-
2017
- 2017-04-06 CN CN201720354943.3U patent/CN206787954U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108044271A (en) * | 2018-01-11 | 2018-05-18 | 上海振华重工(集团)股份有限公司 | A kind of abnormity weight pound plate automatic turning-over device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20190524 Address after: 333000 Lumengchanghe Flight Test Station, Jingdezhen High-tech Zone, Jiangxi Province (High-tech Development Zone) Patentee after: Jiangxi Changhe Agost Helicopter Co.,Ltd. Address before: 330038 No.899 Xuefu Avenue, Honggutan New District, Nanchang City, Jiangxi Province Patentee before: NANCHANG ZHIKU INTELLECTUAL PROPERTY SERVICE CO.,LTD. |
|
| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20171222 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |