CN212780909U - Be used for space flight electronic components test fixture device - Google Patents
Be used for space flight electronic components test fixture device Download PDFInfo
- Publication number
- CN212780909U CN212780909U CN202021390523.9U CN202021390523U CN212780909U CN 212780909 U CN212780909 U CN 212780909U CN 202021390523 U CN202021390523 U CN 202021390523U CN 212780909 U CN212780909 U CN 212780909U
- Authority
- CN
- China
- Prior art keywords
- fixedly connected
- electronic components
- clamping bar
- base
- gas tank
- 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.)
- Active
Links
Images
Landscapes
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
Abstract
The utility model discloses a be used for space flight electronic components test fixture device, the on-line screen storage device comprises a base, the last fixed surface of base is connected with the bracing piece, the last fixed surface of base is connected with the mounting panel is kept away from to the bracing piece, the last fixed surface of mounting panel is connected with the cylinder, the output fixedly connected with connecting rod of cylinder, the one end fixedly connected with clamp plate of cylinder is kept away from to the connecting rod, the lower fixed surface of clamp plate is connected with the cushion. The utility model discloses, through being provided with gas tank and a plurality of clamping bars, can make the clamping bar press from both sides tightly electronic components, press from both sides tightly through gas, can make the clamping bar press from both sides tightly the components and parts of different shapes, and the range of application is comparatively extensive, through being provided with the pin groove, whether normal work of test components and parts is convenient for, through being provided with pressure sensor, the pressure that understanding electronic components that can be clear received, the highest pressure of the normal work of electronic components is convenient for detect.
Description
Technical Field
The utility model relates to an electronic components detection area especially relates to a be used for space flight electronic components test fixture device.
Background
The electronic components are components of electronic elements and small machines and instruments, are usually composed of a plurality of parts and can be commonly used in similar products; it is a general name of electronic devices such as capacitor, transistor, balance spring and spiral spring. Commonly, there are diodes, etc., elements: products that a factory does not alter the molecular composition of the raw material during processing may be referred to as components, devices: products in which the factory changes the molecular structure of the raw material during the manufacturing process are called devices.
In the aerospace industry, electronic components are widely applied, and in order to ensure normal operation of aerospace, manufactured components need to be detected, and during detection, the components need to be clamped, so that detection is convenient, and in the aerospace industry, the components need to be subjected to pressure detection, so that whether the electronic components can normally work under high pressure is detected.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the defects existing in the prior art and providing a clamp device for testing aerospace electronic components.
In order to achieve the above purpose, the utility model adopts the following technical scheme: a test fixture device for aerospace electronic components comprises a base, wherein a supporting rod is fixedly connected to the upper surface of the base, a mounting plate is fixedly connected to the upper surface of the supporting rod, which is far away from the base, an air cylinder is fixedly connected to the upper surface of the mounting plate, a connecting rod is fixedly connected to the output end of the air cylinder, a pressing plate is fixedly connected to one end, which is far away from the air cylinder, of the connecting rod, a cushion is fixedly connected to the lower surface of the pressing plate, an air pump is fixedly connected to the upper surface of the base, which is positioned on the right side of the supporting rod, an electronic valve is fixedly connected to the output end of the air pump, a vent pipe is fixedly connected to one end, which is far away from the air pump, of the electronic valve, a placing block is arranged on the upper surface of the base, which is positioned on the right side, the inside of clamp splice is provided with the gas tank, the inside of gas tank is provided with the clamping bar, the interior bottom fixedly connected with electro-magnet of gas tank, clamping bar one end fixed connection rubber pad, the one end fixedly connected with pressure sensor that the rubber pad was kept away from to the clamping bar.
As a further description of the above technical solution:
the breather pipe is kept away from the one end of electronic valve and is connected with the gas tank, the gas tank is total two, and is located the front and back both sides of recess.
As a further description of the above technical solution:
the position of cushion is located the lead foot groove directly over, the one end that pressure sensor was kept away from to the clamping bar extends to the inside of recess.
As a further description of the above technical solution:
the junction of clamping bar and gas tank is provided with the sealing washer, the one end that the cylinder was kept away from to the connecting rod extends to the below of mounting panel.
As a further description of the above technical solution:
the position of the electromagnet is located at the tail end of the clamping rod, and the clamping rod is made of magnetic metal.
As a further description of the above technical solution:
the pressing plate is of a hollow structure, and the bottom of the groove is arc-shaped.
The utility model discloses following beneficial effect has:
1. compared with the prior art, this be used for space flight electronic components test fixture device through being provided with gas tank and a plurality of clamping bar, can make the clamping bar press from both sides tight electronic components, presss from both sides tightly through gas, can make the clamping bar press from both sides tightly the components and parts of different shapes, and the range of application is comparatively extensive.
2. Compared with the prior art, this be used for space flight electronic components test fixture device through being provided with the pin groove, is convenient for be connected with the external world, tests whether components and parts normally work, through being provided with pressure sensor, the highest pressure that understanding electronic components that can be clear received is convenient for detect the normal work of electronic components.
Drawings
Fig. 1 is a schematic overall structure diagram of a fixture device for testing aerospace electronic components according to the present invention;
fig. 2 is a schematic view of an internal structure of a clamping block of the clamp device for testing aerospace electronic components according to the present invention;
fig. 3 is the utility model provides a clamp plate structure chart for space flight electronic components test fixture device.
Illustration of the drawings:
1. a base; 2. a support bar; 3. mounting a plate; 4. a cylinder; 5. a connecting rod; 6. pressing a plate; 7. a soft cushion; 8. an air pump; 9. a breather pipe; 10. placing the blocks; 11. a clamping block; 12. a groove; 13. a gas tank; 14. a clamping bar; 15. a seal ring; 16. an electromagnet; 17. a rubber pad; 18. a lead groove; 19. an electronic valve; 20. a pressure sensor.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention; the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance, and furthermore, unless otherwise explicitly stated or limited, the terms "mounted," "connected," and "connected" are to be construed broadly and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Referring to fig. 1-3, the utility model provides a pair of be used for space flight electronic components test fixture device: comprises a base 1 and a supporting clamp, wherein a supporting rod 2 is fixedly connected to the upper surface of the base 1, a mounting plate 3 is fixedly connected to the upper surface of the supporting rod 2 far away from the base 1, a mounting cylinder 4 is arranged, a cylinder 4 is fixedly connected to the upper surface of the mounting plate 3 and provides power for the vertical movement of the pressing plate 6, a connecting rod 5 is fixedly connected to the output end of the cylinder 4, one end of the connecting rod 5 far away from the cylinder 4 is fixedly connected with the pressing plate 6 and presses pins tightly, so that the pins are not randomly moved, a cushion 7 is fixedly connected to the lower surface of the pressing plate 6 and damages the pins are prevented from being caused by the pressing, an air pump 8 is fixedly connected to the upper surface of the base 1 and positioned on the right side of the supporting rod 2 and provides power for air intake, an electronic valve 19 is fixedly connected to the output end of the air pump 8 and, place last fixed surface of piece 10 and be connected with clamp splice 11, press from both sides tight electronic component, the upper surface of clamp splice 11 is provided with recess 12, place electronic component, the upper surface of clamp splice 11 and the both sides that are located recess 12 are provided with pin groove 18, place the pin, the inside of clamp splice 11 is provided with gas tank 13, provide atmospheric pressure, the inside of gas tank 13 is provided with clamping bar 14, press from both sides tight electronic component, the interior bottom fixedly connected with electro-magnet 16 of gas tank 13, conveniently make clamping bar 14 return, clamping bar 14 one end fixedly connected with rubber pad 17, protection components and parts, clamping bar 14 keeps away from one end fixedly connected with pressure sensor 20 of rubber pad 17, detect pressure.
One end that electronic valve 19 was kept away from to breather pipe 9 is connected with gas tank 13, gas tank 13 is total two, and be located the front and back both sides of recess 12, carry out two-way clamp, the position of cushion 7 is located pin groove 18 directly over, it is convenient to press from both sides the pin tightly, the one end that pressure sensor 20 was kept away from to clamping bar 14 extends to the inside of recess 12, the junction of clamping bar 14 and gas tank 13 is provided with sealing washer 15, prevent that atmospheric pressure from revealing, the one end that cylinder 4 was kept away from to connecting rod 5 extends to the below of mounting panel 3, the position of electro-magnet 16 is located the tail end of clamping bar 14, conveniently carry out the return, the material of clamping bar 14 is magnetic metal, clamp plate 6 adopts hollow structure, conveniently observe electronic components's state, the bottom shape of recess 12 is the arc, conveniently.
The working principle is as follows: through placing electronic components in recess 12, lead out the pin through pin groove 18 and pass through start cylinder 4, fall clamp plate 6, compress tightly the pin, through starting air pump 8 and electronic valve 19, aerify gas tank 13, make clamping bar 14 remove through atmospheric pressure, press from both sides tightly electronic components, through the pin that exposes, be connected with the external world, detect electronic components's work, it is gaseous to last to rush into gas tank 13 through air pump 8, increase pressure, make clamping bar 14 increase electronic components's pressure, the maximum pressure that test electronic components can bear under normal operating condition.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications and variations can be made in the embodiments or in part of the technical features of the embodiments without departing from the spirit and the scope of the invention.
Claims (6)
1. The utility model provides a be used for space flight electronic components test fixture device, includes base (1), its characterized in that: the air pump is characterized in that a supporting rod (2) is fixedly connected to the upper surface of the base (1), a mounting plate (3) is fixedly connected to the upper surface of the supporting rod (2) far away from the base (1), an air cylinder (4) is fixedly connected to the upper surface of the mounting plate (3), a connecting rod (5) is fixedly connected to the output end of the air cylinder (4), a pressing plate (6) is fixedly connected to one end, far away from the air cylinder (4), of the connecting rod (5), a cushion (7) is fixedly connected to the lower surface of the pressing plate (6), an air pump (8) is fixedly connected to the right side of the supporting rod (2) and the upper surface of the base (1), an electronic valve (19) is fixedly connected to the output end of the air pump (8), a vent pipe (9) is fixedly connected to one end, far away from the air pump (8), of the electronic valve (, the upper surface fixedly connected with clamp splice (11) of placing piece (10), the upper surface of clamp splice (11) is provided with recess (12), the upper surface of clamp splice (11) and the both sides that are located recess (12) are provided with pin groove (18), the inside of clamp splice (11) is provided with gas tank (13), the inside of gas tank (13) is provided with clamping bar (14), interior bottom fixedly connected with electro-magnet (16) of gas tank (13), clamping bar (14) one end fixed connection rubber pad (17), the one end fixedly connected with pressure sensor (20) of rubber pad (17) are kept away from in clamping bar (14).
2. The clamp device for testing the aerospace electronic components as claimed in claim 1, wherein: one end of the vent pipe (9) far away from the electronic valve (19) is connected with the air boxes (13), and the number of the air boxes (13) is two, and the air boxes are positioned on the front side and the rear side of the groove (12).
3. The clamp device for testing the aerospace electronic components as claimed in claim 1, wherein: the position of the soft pad (7) is positioned right above the pin groove (18), and one end of the clamping rod (14) far away from the pressure sensor (20) extends to the inside of the groove (12).
4. The clamp device for testing the aerospace electronic components as claimed in claim 1, wherein: the junction of clamping bar (14) and gas tank (13) is provided with sealing washer (15), the one end that cylinder (4) were kept away from in connecting rod (5) extends to the below of mounting panel (3).
5. The clamp device for testing the aerospace electronic components as claimed in claim 1, wherein: the position of the electromagnet (16) is located at the tail end of the clamping rod (14), and the clamping rod (14) is made of magnetic metal.
6. The clamp device for testing the aerospace electronic components as claimed in claim 1, wherein: the pressing plate (6) is of a hollow structure, and the bottom of the groove (12) is arc-shaped.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021390523.9U CN212780909U (en) | 2020-07-15 | 2020-07-15 | Be used for space flight electronic components test fixture device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021390523.9U CN212780909U (en) | 2020-07-15 | 2020-07-15 | Be used for space flight electronic components test fixture device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212780909U true CN212780909U (en) | 2021-03-23 |
Family
ID=75077775
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021390523.9U Active CN212780909U (en) | 2020-07-15 | 2020-07-15 | Be used for space flight electronic components test fixture device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212780909U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113211353A (en) * | 2021-05-24 | 2021-08-06 | 衢州市得意居家私有限公司 | Clamping tool and clamping method for furniture production |
-
2020
- 2020-07-15 CN CN202021390523.9U patent/CN212780909U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113211353A (en) * | 2021-05-24 | 2021-08-06 | 衢州市得意居家私有限公司 | Clamping tool and clamping method for furniture production |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN212780909U (en) | Be used for space flight electronic components test fixture device | |
| CN209802593U (en) | Battery shell leakage detection device | |
| CN205102985U (en) | Check out test set is revealed to multistation wet -type | |
| CN105547610A (en) | Air tightness testing machine | |
| CN211877311U (en) | Composite detection tool combining leakage test clamp with error-proof detection tool | |
| CN215263880U (en) | Pedal switch electricity life-span testboard | |
| CN210664911U (en) | End cover gas tightness detection device | |
| CN211603281U (en) | Automatic clamping fixture of flying probe testing machine | |
| CN210741766U (en) | Convenient fixed gas tightness testboard for denso oxygen sensor | |
| CN218885329U (en) | Gas microleakage detecting system | |
| CN207649491U (en) | Pipe fitting hole location tolerance detection device | |
| CN208140079U (en) | A kind of flatness detecting tool for automobile manifold flange | |
| CN212351755U (en) | Clamp structure for processing electronic component | |
| CN216589408U (en) | Overflow valve block testing device | |
| CN210909641U (en) | Clamp on accessory detection device | |
| CN218018559U (en) | Engine cylinder block robot clamp | |
| CN217123102U (en) | Frock clamp of auto-parts processing usefulness | |
| CN210323278U (en) | Novel chip test adsorption structure | |
| CN110887612A (en) | Camshaft shroud water (gas) seal detection device | |
| CN216082953U (en) | 5G paster small metal filter testing arrangement | |
| CN218567538U (en) | Prevent folding board test jig | |
| CN219757645U (en) | Crystal oscillator detection device | |
| CN220751510U (en) | Engine water pump airtight test tool convenient to it is fixed | |
| CN213149010U (en) | Test fixture | |
| CN214309342U (en) | Airtight detection clamp of non-standard leakage calibration piece |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |