CN212064034U - Aviation bus tester - Google Patents

Aviation bus tester Download PDF

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Publication number
CN212064034U
CN212064034U CN202021069318.2U CN202021069318U CN212064034U CN 212064034 U CN212064034 U CN 212064034U CN 202021069318 U CN202021069318 U CN 202021069318U CN 212064034 U CN212064034 U CN 212064034U
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China
Prior art keywords
module
interface
tester
connector
bus
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Active
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CN202021069318.2U
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Chinese (zh)
Inventor
荣彬杰
吴东
夏思宇
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Chengdu Punuo Technology Co ltd
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Chengdu Punuo Technology Co ltd
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Priority to CN202021069318.2U priority Critical patent/CN212064034U/en
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Abstract

The utility model discloses an aviation bus tester, which comprises a signal processing unit, a communication module, a storage module, a display unit, a power supply module and a bus support plate; the bus carrier plate is provided with a connector; the connector is connected with a test interface, a data transmission interface and a network interface. The utility model discloses can communicate with external equipment; the input and output interfaces of the whole tester are led out from the carrier plate, so that the volume is reduced; the power module supplies power to each module through the connector, and each module is interconnected through the support plate, can realize miniaturized tester, has simple structure, light in weight, low-power consumption's characteristics.

Description

Aviation bus tester
Technical Field
The utility model relates to the field of electronic technology, especially, relate to aviation bus tester.
Background
The traditional aviation bus adopts a plurality of processors, and the tester has large volume and poor flexibility and is inconvenient to carry and use on site; in addition, the traditional processor has high power consumption, low test efficiency and poor expandability; and the traditional tester does not have the function of data exchange with external equipment.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the above problems and provide an aviation bus tester, which comprises a signal processing unit, a communication module, a storage module, a display unit, a power supply module and a bus carrier plate; the bus carrier plate is provided with a connector; the connector is connected with a test interface, a data transmission interface and a network interface; the signal processing unit is connected with the communication module, the storage module and the display unit through the connector; the power supply module is connected with the communication module, the storage module and the display unit through connectors; the power module is connected with a power interface, and the power interface is used for connecting an external input power supply.
The beneficial effects of the utility model reside in that: the utility model discloses can communicate with external equipment; the input and output interfaces of the whole tester are led out from the carrier plate, so that the volume is reduced; the power module supplies power to each module through the connector, and each module is interconnected through the support plate, can realize miniaturized tester, has simple structure, light in weight, low-power consumption's characteristics.
Drawings
FIG. 1 is a schematic diagram of the system of the present invention;
fig. 2 is a schematic diagram of an embodiment.
Detailed Description
The present invention will be further explained with reference to the accompanying drawings:
as shown in the attached drawing 1, the utility model discloses an aviation bus tester, including signal processing unit, communication module, storage module, display element, power module and bus support plate; the bus carrier plate is provided with a connector; the connector is connected with a test interface, a data transmission interface and a network interface; the signal processing unit is connected with the communication module, the storage module and the display unit through the connector; the power supply module is connected with the communication module, the storage module and the display unit through connectors; the power module is connected with a power interface, and the power interface is used for connecting an external input power supply.
Specifically, the signal processing unit comprises an ARM processor and an FPGA module; the ARM processor is connected with the FPGA module; the ARM processor and the FPGA module are respectively connected with the connector.
Specifically, the signal processing unit adopts a ZYNQ7000 processor.
Specifically, the communication module adopts a 1553B communication module.
Specifically, the test interface adopts an X718 test interface.
Specifically, the data transmission interface adopts a USB interface.
Specifically, the communication module is a 1553B communication module.
The network interface adopts a gigabit Ethernet interface, the display unit adopts an LCD display screen, and the test result can be displayed through the display screen. The signal processing unit adopts a ZYNQ7000 chip, an ARM chip and an FPGA module are integrated in the SOC chip, and the ARM end is provided with a USB interface, an I2C interface and a serial port; the FPGA end can directly lead out an LCD display bus, an I/O control line and a 1553B data bus. The ZYNQ7000 chip has the characteristics of low power consumption and miniaturization, and can realize a tester which is more flexible and has stronger expansibility.
The memory module adopts an EMMC memory. The tester can be externally connected with a storage disk through a USB interface.
By adopting the carrier plate, the input and output interfaces of the tester are all led out from the carrier plate, all modules are interconnected and communicated through the connector on the carrier plate, and the carrier plate can be provided with a conditioning circuit, a resistance testing circuit and the like, so that the space can be saved.
The utility model discloses can communicate with external equipment; the input and output interfaces of the whole tester are led out from the carrier plate, so that the volume is reduced; the power module supplies power for each module through the connector, and each module passes through the support plate interconnection, can realize miniaturized tester, has the characteristics of low-power consumption.
The technical scheme of the utility model is not limited to the restriction of above-mentioned specific embodiment, all according to the utility model discloses a technical scheme makes technical deformation, all falls into within the protection scope of the utility model.

Claims (7)

1. The aviation bus tester is characterized by comprising a signal processing unit, a communication module, a storage module, a display unit, a power supply module and a bus carrier plate; the bus carrier plate is provided with a connector; the connector is connected with a test interface, a data transmission interface and a network interface; the signal processing unit is connected with the communication module, the storage module and the display unit through the connector; the power supply module is connected with the communication module, the storage module and the display unit through connectors; the power module is connected with a power interface, and the power interface is used for connecting an external input power supply.
2. The aircraft bus tester as recited in claim 1, wherein the signal processing unit comprises an ARM processor and an FPGA module; the ARM processor is connected with the FPGA module; the ARM processor and the FPGA module are respectively connected with the connector.
3. The aircraft bus tester as recited in claim 2, wherein the signal processing unit employs a ZYNQ7000 processor.
4. The aeronautical bus tester of claim 1, wherein the communication module is a 1553B communication module.
5. The aircraft bus tester as recited in claim 1, wherein the test interface is an X718 test interface.
6. The aircraft bus tester as recited in claim 1, wherein the data transfer interface is a USB interface.
7. The aeronautical bus tester of claim 1, wherein the communication module is a 1553B communication module.
CN202021069318.2U 2020-06-11 2020-06-11 Aviation bus tester Active CN212064034U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202021069318.2U CN212064034U (en) 2020-06-11 2020-06-11 Aviation bus tester

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202021069318.2U CN212064034U (en) 2020-06-11 2020-06-11 Aviation bus tester

Publications (1)

Publication Number Publication Date
CN212064034U true CN212064034U (en) 2020-12-01

Family

ID=73513449

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202021069318.2U Active CN212064034U (en) 2020-06-11 2020-06-11 Aviation bus tester

Country Status (1)

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CN (1) CN212064034U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115269490A (en) * 2022-07-15 2022-11-01 湖北三江航天万峰科技发展有限公司 Onboard integrated control system and device based on SOC and FPGA integration

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115269490A (en) * 2022-07-15 2022-11-01 湖北三江航天万峰科技发展有限公司 Onboard integrated control system and device based on SOC and FPGA integration

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