CN215121469U - Integrated testing device of aviation simulation testing equipment - Google Patents
Integrated testing device of aviation simulation testing equipment Download PDFInfo
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- CN215121469U CN215121469U CN202121218764.XU CN202121218764U CN215121469U CN 215121469 U CN215121469 U CN 215121469U CN 202121218764 U CN202121218764 U CN 202121218764U CN 215121469 U CN215121469 U CN 215121469U
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- heat dissipation
- battery
- heat
- battery compartment
- testing machine
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Abstract
The utility model discloses an integral type testing arrangement of aviation simulation test equipment, be in including the test machine body, can dismantle the setting the battery compartment body and the setting on the test machine body outer wall are in radiator unit on the battery compartment body, the internal storage of battery compartment is provided with the group battery, radiator unit dispels the heat to the group battery in the internal chamber of battery compartment, correspond to on the wall body of the battery compartment body air intake and air outlet have been seted up to radiator unit. Through setting up DC power supply and test machine body integration, can make whole volume littleer, and lifting means wholeness promotes the convenience of use, convenient transportation and transport.
Description
Technical Field
The utility model belongs to aviation simulation test field, in particular to integral type testing arrangement of aviation simulation test equipment.
Background
At present, a direct current power supply needs to be connected to the simulation testing device during testing, the direct current power supply and the simulation testing machine body are arranged in a split independent mode, and the simulation testing device is very inconvenient to transport, transport and the like.
Disclosure of Invention
The purpose of the invention is as follows: in order to overcome the not enough of existence among the prior art, the utility model provides an aviation simulation test equipment's integral type testing arrangement promotes the equipment wholeness, promotes the convenience in use.
The technical scheme is as follows: in order to achieve the above purpose, the technical scheme of the utility model is as follows:
the integrated testing device of the aviation simulation testing equipment comprises a testing machine body, a battery compartment body and a heat dissipation assembly, wherein the battery compartment body is detachably arranged on the outer wall of the testing machine body, the heat dissipation assembly is arranged on the battery compartment body, a battery pack is contained in the battery compartment body, the heat dissipation assembly dissipates heat of the battery pack in an inner cavity of the battery compartment body, and an air inlet and an air outlet are formed in the wall body of the battery compartment body and correspond to the heat dissipation assembly.
Further, the radiating assembly comprises a radiating fan and a radiating partition plate, the radiating partition plate is arranged between the air inlet and the air outlet respectively, the radiating partition plate forms a plurality of air cooling channels in the same direction as the radiating direction, and the radiating fan is arranged at one end of the air cooling channel corresponding to the air inlet.
Furthermore, a dustproof filter screen is arranged between the heat dissipation fan and the air inlet.
Furthermore, the battery compartment body is a box structure with an opening at one side, the opening side of the battery compartment body is covered on the wall body of the testing machine body, a heat-conducting plate is arranged on the opening side of the battery compartment body, a plurality of heat dissipation partition plates are arranged on the heat-conducting plate corresponding to one side wall of the battery pack, and the heat dissipation partition plates are pressed against the battery pack.
Furthermore, the heat conducting plate is arranged in a manner that one side wall of the heat conducting plate, which is deviated from the battery pack, is in contact with the wall body of the testing machine body, and heat conducting silicone grease is filled between the heat conducting plate and the testing machine body.
Furthermore, an inner support frame is arranged in the inner cavity of the battery bin body corresponding to the heat-conducting plate, and the heat-conducting plate is detachably arranged on the inner support frame through a fixing structure.
Has the advantages that: the utility model discloses set up DC power supply and test machine body integration, can make whole volume littleer, and the lifting means wholeness promotes the convenience of use, convenient transportation and transport.
Drawings
FIG. 1 is a perspective view of the overall structure of the present invention;
fig. 2 is a schematic three-dimensional structure diagram of the battery compartment body and the heat dissipation assembly of the present invention;
FIG. 3 is a front view of the internal structure of the battery compartment body of the present invention;
fig. 4 is a schematic view of a half-section of the internal structure a-a of the battery compartment body of the present invention.
Detailed Description
The present invention will be further described with reference to the accompanying drawings.
As shown in fig. 1 to 4, an integrated testing device of an aviation simulation testing device comprises a testing machine body 1, a battery compartment body 2 detachably arranged on the outer wall of the testing machine body 1, and a heat dissipation assembly 3 arranged on the battery compartment body 2, wherein a battery pack is accommodated in the battery compartment body 2 and is a direct current power supply, the heat dissipation assembly 3 dissipates heat of the battery pack in the inner cavity of the battery compartment body 2, an air inlet 4 and an air outlet 5 are formed in the wall body of the battery compartment body 2 corresponding to the heat dissipation assembly 3, and the direct current power supply and the testing machine body are integrally arranged, so that the overall size is smaller, the integrity of the testing machine is improved, the convenience in use is improved, and the transportation are convenient.
And a dustproof filter screen 8 is arranged between the heat dissipation fan 6 and the air inlet 4 to reduce dust entering the battery compartment.
The battery bin body 2 is a box body structure with an opening at one side, the opening side of the battery bin body 2 is covered on the wall body of the testing machine body 1, a heat conducting plate 9 is arranged on the opening side of the battery bin body 2, a plurality of heat dissipation partition plates 7 are arranged on one side wall of the heat conducting plate 9 corresponding to the battery pack, and the heat dissipation partition plates 7 are pressed on the battery pack. The heat conducting plate 9 is arranged in a manner that a side wall departing from the battery pack is in contact with a wall body of the testing machine body 1, and heat conducting silicone grease is filled between the heat conducting plate 9 and the testing machine body 1. The heat on the battery bin body and the testing machine body 1 is conducted into the heat conducting plate and the heat dissipation partition plate through the heat conducting plate 9, and heat dissipation is carried out through the heat dissipation fan 6, so that the overall heat dissipation and cooling effects are improved.
An inner support frame 10 is arranged in the inner cavity of the battery bin body 2 corresponding to the heat-conducting plate 9, the heat-conducting plate 9 and the heat-radiating fan 6 are detachably arranged on the inner support frame 10 through fixing structures, and the fixing structures are bolt screws and the like.
The above description is only a preferred embodiment of the present invention, and it should be noted that: for those skilled in the art, without departing from the principle of the present invention, several improvements and modifications can be made, and these improvements and modifications should also be considered as the protection scope of the present invention.
Claims (6)
1. The utility model provides an aviation simulation test equipment's integral type testing arrangement which characterized in that: the testing machine comprises a testing machine body (1), a battery bin body (2) detachably arranged on the outer wall of the testing machine body (1) and a heat dissipation assembly (3) arranged on the battery bin body (2), wherein a battery pack is contained in the battery bin body (2), the heat dissipation assembly (3) dissipates the heat of the battery pack in the inner cavity of the battery bin body (2), and an air inlet (4) and an air outlet (5) are formed in the wall body of the battery bin body (2) corresponding to the heat dissipation assembly (3).
2. The integrated test device of the aviation simulation test equipment as claimed in claim 1, wherein: radiating component (3) are including heat dissipation fan (6) and heat dissipation baffle (7), and are a plurality of heat dissipation baffle (7) set up respectively between air intake and air-out, and are a plurality of heat dissipation baffle (7) constitute a plurality of syntropy in the forced air cooling passageway of heat dissipation direction, heat dissipation fan (6) set up the one end at the forced air cooling passageway corresponding to air intake (4).
3. The integrated test device of the aviation simulation test equipment as claimed in claim 2, wherein: and a dustproof filter screen (8) is arranged between the heat dissipation fan (6) and the air inlet (4).
4. The integrated test device of the aviation simulation test equipment as claimed in claim 2, wherein: the battery compartment body (2) is of a box body structure with an opening at one side, the opening side cover of the battery compartment body (2) is arranged on the wall body of the testing machine body (1), a heat conducting plate (9) is arranged on the opening side of the battery compartment body (2), a plurality of heat dissipation partition plates (7) are arranged on one side wall of the heat conducting plate (9) corresponding to the battery pack, and the heat dissipation partition plates (7) are abutted against the battery pack.
5. The integrated test device of the aviation simulation test equipment as claimed in claim 4, wherein: the heat conduction plate (9) is arranged in a manner that one side wall departing from the battery pack is in contact with the wall body of the testing machine body (1), and heat conduction silicone grease is filled between the heat conduction plate (9) and the testing machine body (1).
6. The integrated test device of the aviation simulation test equipment as claimed in claim 4, wherein: an inner support frame (10) is arranged in the inner cavity of the battery bin body (2) corresponding to the heat conducting plate (9), and the heat conducting plate (9) is detachably arranged on the inner support frame (10) through a fixing structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121218764.XU CN215121469U (en) | 2021-06-02 | 2021-06-02 | Integrated testing device of aviation simulation testing equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121218764.XU CN215121469U (en) | 2021-06-02 | 2021-06-02 | Integrated testing device of aviation simulation testing equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215121469U true CN215121469U (en) | 2021-12-10 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121218764.XU Active CN215121469U (en) | 2021-06-02 | 2021-06-02 | Integrated testing device of aviation simulation testing equipment |
Country Status (1)
| Country | Link |
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| CN (1) | CN215121469U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113466580A (en) * | 2021-06-02 | 2021-10-01 | 无锡市航鹄科技有限公司 | Test method and integrated test equipment of aviation simulation test system |
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2021
- 2021-06-02 CN CN202121218764.XU patent/CN215121469U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113466580A (en) * | 2021-06-02 | 2021-10-01 | 无锡市航鹄科技有限公司 | Test method and integrated test equipment of aviation simulation test system |
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