CN205429201U - Unmanned aerial vehicle machine carries instrumentation test equipment - Google Patents
Unmanned aerial vehicle machine carries instrumentation test equipment Download PDFInfo
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- CN205429201U CN205429201U CN201521088935.6U CN201521088935U CN205429201U CN 205429201 U CN205429201 U CN 205429201U CN 201521088935 U CN201521088935 U CN 201521088935U CN 205429201 U CN205429201 U CN 205429201U
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- protective housing
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- aerial vehicle
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Abstract
The utility model discloses an unmanned aerial vehicle machine carries instrumentation test equipment, its portable removal protective housing will be testable machine electric interface integration in an organic whole of carrying the instrument, the industrial computer install in in the inside frame of portable removal protective housing, be connected with the operating panel who installs in portable removal protective housing front side upper portion through electric gas shift unit, the industrial computer carries on there is special test software, electric gas shift unit basis the external electric loop of signal of telecommunication automatic switch -over that the industrial computer sent, line box are installed in the lower part of portable removal protective housing, install KVM integration display at the middle part of portable removal protective housing with the mode of pull. The utility model discloses can accomplish nearly five kinds the quick -witted test who carries the instrument of unmanned aerial vehicle, optimize the inside space layout of portable removal protective housing, realize machinery and electric highly integrated to utilize electric gas shift unit to realize the directionality test of single equipment and the electric channel selection of many equipment.
Description
Technical field
This utility model relates to a kind of unmanned aerial vehicle onboard instrument test equipment, particularly relates to a kind of test equipment for testing unmanned aerial vehicle onboard instrumental function.
Background technology
Unmanned aerial vehicle onboard instrument test equipment is a kind of orthotype equipment towards unmanned aerial vehicle onboard equipment, belongs to the category of unmanned aerial vehicle safeguards system.Conventional unmanned aerial vehicle onboard instrument test equipment is divided into orthotype and universal two big classes, orthotype device structure level is distinct, often use handheld terminal or microcomputer to develop, and combine peripheral electrical and connect equipment and realize its function, but the onboard instrument kind that the type equipment is tested is single；Universal equipment is often based on high-end industrial computer, for different onboard instruments, makes specific frock, and the early-stage preparations time of the type equipment is longer, and structure is complicated higher to the requirement of operator.
Summary of the invention
In order to solve the problems referred to above, unmanned aerial vehicle onboard instrument test equipment of the present utility model is centered by high-end industrial computer, Portable movable protective housing is used to be integrated in one by the electric interfaces of five class unmanned aerial vehicle onboard instruments, enrich the kind of testable onboard instrument, the most significantly simplify the structure of system, reduce the requirement to operator simultaneously.This simple and testable onboard instrument of unmanned aerial vehicle onboard instrument test device structure up to five kinds.
nullThe Portable movable protective housing of unmanned aerial vehicle onboard instrument test equipment of the present utility model is the installation carrier of whole equipment，The electric interfaces of testable onboard instrument is integrated in one，Industrial computer is installed in the internal rack of described Portable movable protective housing，It is attached by electric conversion unit and the guidance panel being installed on described Portable movable protective housing forward upper，Identify that the push-botton operation of described guidance panel instructs and simplify electrical connection circuit，Described industrial computer is equipped with specific test and measure software，So that the model of tested onboard instrument is selected instruction morphing as the signal of telecommunication by operator，The signal of telecommunication that described electric conversion unit sends according to described industrial computer automatically switches external electric loop，The test of corresponding onboard instrument is completed in conjunction with cable connection plug and equipment plug，Line box is arranged on the bottom of described Portable movable protective housing，The adnexaes such as cable can be received，At the middle part of described Portable movable protective housing, KVM integration display is installed in the way of pull，In order to process the various test data of display.
The most described industrial computer is equipped with vertical gyro, radar altimeter, DGPS, optical fiber inertial navigation and the specific test and measure software of air data computer, it is possible to meet the test request of up to five kinds of unmanned aerial vehicle onboard instruments.
The beneficial effects of the utility model are:
1. use the structure of specific test and measure software and changeable electric loop to achieve the test request of up to five kinds of unmanned aerial vehicle onboard instruments.
2. the Portable movable protective housing parcel industrial computer used and the structure of integration display improve the mechanical integrity of equipment, and coordinate the electric integrated level of Special electric gas shift unit lifting equipment.
3. operator only need to carry out cable connect can test, enormously simplify the preparation before test.
Accompanying drawing explanation
Fig. 1 is the structure chart of unmanned aerial vehicle onboard instrument test equipment.
Fig. 2 is that industrial computer puts figure.
Fig. 3 is guidance panel schematic diagram.
Fig. 4 is cable connection figure.
Symbol description
1. Portable movable protective housing, 2. guidance panel, 3. line box, 4.KVM integration display, 5. industrial computer, 6. electric conversion unit, 7. industrial computer powers on display lamp, 8. industrial computer switch, 9. appliance icon, 10. device power supply (DPS) switch, 11. cable connection jacks, 12. main power sockets and switch, 13. cables connect plug, 14. equipment plugs
Detailed description of the invention
Below in conjunction with accompanying drawing, this utility model is further described.
The present invention include Portable movable protective housing 1, guidance panel 2, line box 3, KVM integration display 4, industrial computer 5, electric conversion unit 6, industrial computer power on display lamp 7, industrial computer switch 8, appliance icon 9, device power supply (DPS) switch 10, cable connection jacks 11, supply socket and switch 12, cable connect plug 13, equipment plug 14.
In FIG, guidance panel 2 is arranged on the upper surface of Portable movable protective housing 1, operator are facilitated to operate, line box 3 is arranged on the bottom of Portable movable protective housing 1, the adnexaes such as cable can be received, KVM integration display 4 is arranged on the middle part of Portable movable protective housing 1, carries out switching manipulation by pull, in order to process the various test data of display.
In fig. 2, guidance panel 2 is electrically connected with industrial computer 5 by electric conversion unit 6, and the button commands of guidance panel can be uploaded to industrial computer by electric conversion unit 6, it is possible to be transmitted to tested airborne equipment by sending instructions under industrial computer.Industrial computer 5 is equipped with vertical gyro, radar altimeter, DGPS, optical fiber inertial navigation and the specific test and measure software of air data computer, to select instruction morphing as the signal of telecommunication by operator to the model of tested onboard instrument.
In figure 3, supply socket and switch 12 can be accessed by 220V alternating current, power supply is provided for whole system, the unlatching of industrial computer switch 8 control industrial computer and closedown, and the state of industrial computer is shown by the industrial computer display lamp 7 that powers on, cable connection jacks 9 connecting test cable carries out the test of equipment, and is powered for equipment by the unlatching of device power supply (DPS) switch 10.
Claims (2)
- null1. a unmanned aerial vehicle onboard instrument test equipment，It is characterized in that: Portable movable protective housing is the installation carrier of whole equipment，The electric interfaces of testable onboard instrument is integrated in one，Industrial computer is installed in the internal rack of described Portable movable protective housing，It is attached by electric conversion unit and the guidance panel being installed on described Portable movable protective housing forward upper，Identify that the push-botton operation of described guidance panel instructs and simplify electrical connection circuit，Described industrial computer is equipped with specific test and measure software，So that the model of tested onboard instrument is selected instruction morphing as the signal of telecommunication by operator，The signal of telecommunication that described electric conversion unit sends according to described industrial computer automatically switches external electric loop，The test of corresponding onboard instrument is completed in conjunction with cable connection plug and equipment plug，Line box is arranged on the bottom of described Portable movable protective housing，The adnexaes such as cable can be received，At the middle part of described Portable movable protective housing, KVM integration display is installed in the way of pull，In order to process the various test data of display.
- Unmanned aerial vehicle onboard instrument test equipment the most according to claim 1, it is characterised in that: described industrial computer is equipped with vertical gyro, radar altimeter, DGPS, optical fiber inertial navigation and the specific test and measure software of air data computer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521088935.6U CN205429201U (en) | 2015-12-23 | 2015-12-23 | Unmanned aerial vehicle machine carries instrumentation test equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521088935.6U CN205429201U (en) | 2015-12-23 | 2015-12-23 | Unmanned aerial vehicle machine carries instrumentation test equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205429201U true CN205429201U (en) | 2016-08-03 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201521088935.6U Active CN205429201U (en) | 2015-12-23 | 2015-12-23 | Unmanned aerial vehicle machine carries instrumentation test equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205429201U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106681309A (en) * | 2017-02-15 | 2017-05-17 | 合肥市融宇电子有限公司 | Comprehensive test platform for unmanned aerial vehicle |
-
2015
- 2015-12-23 CN CN201521088935.6U patent/CN205429201U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106681309A (en) * | 2017-02-15 | 2017-05-17 | 合肥市融宇电子有限公司 | Comprehensive test platform for unmanned aerial vehicle |
| CN106681309B (en) * | 2017-02-15 | 2019-08-23 | 合肥市融宇电子有限公司 | A kind of unmanned plane comprehensive test platform |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20170424 Address after: 313216 Zhejiang city of Huzhou province Deqing County Qianyuan town Nanyang Road No. 58 Patentee after: Aerospace Nanyang (Zhejiang) Technology Co., Ltd. Address before: 100074 Beijing, Fengtai District Yungang West Road, No. 17 Patentee before: China Aerospace Aerodynamic Technology Institute |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20170815 Address after: 100074 Beijing, Fengtai District Yungang West Road, No. 17 Patentee after: China Aerospace Aerodynamic Technology Institute Address before: 313216 Zhejiang city of Huzhou province Deqing County Qianyuan town Nanyang Road No. 58 Patentee before: Aerospace Nanyang (Zhejiang) Technology Co., Ltd. |
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| TR01 | Transfer of patent right |