CN201589824U - Comprehensive detecting system of airborne equipment - Google Patents

Comprehensive detecting system of airborne equipment Download PDF

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Publication number
CN201589824U
CN201589824U CN2009203151116U CN200920315111U CN201589824U CN 201589824 U CN201589824 U CN 201589824U CN 2009203151116 U CN2009203151116 U CN 2009203151116U CN 200920315111 U CN200920315111 U CN 200920315111U CN 201589824 U CN201589824 U CN 201589824U
Authority
CN
China
Prior art keywords
card
adapter
airborne equipment
bus
cpu
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.)
Expired - Lifetime
Application number
CN2009203151116U
Other languages
Chinese (zh)
Inventor
余永奎
龚尚权
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SICHUAN HAITE HIGH-TECH CO LTD
Original Assignee
SICHUAN HAITE HIGH-TECH CO LTD
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by SICHUAN HAITE HIGH-TECH CO LTD filed Critical SICHUAN HAITE HIGH-TECH CO LTD
Priority to CN2009203151116U priority Critical patent/CN201589824U/en
Application granted granted Critical
Publication of CN201589824U publication Critical patent/CN201589824U/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Abstract

The utility model discloses a comprehensive detecting system of airborne equipment. The detecting system comprises a main case; a CPU is arranged in the main case and connected with a keyboard, a mouse, a hard disk, a floppy, a display and a printer respectively; the CPU is connected with a bus card, a D/S card, an S/D card, a DMS card and an AX5488 card through a multi-slot expansion baseplate; the bus card, the D/S card, the S/D card and the DMS card in the main case are connected with a terminal block; the terminal block is connected with a connector socket; and a special adapter is accessed between the terminal block and the connector socket. The utility model has the advantage that the detecting system can complete maintenance, troubleshooting, and performance detection to MCP, and can ensure real-time accurate and precious detection of the airborne MCP.

Description

The airborne equipment comprehensive detection system
Technical field
The utility model relates to a kind of checkout equipment, especially relates to a kind of airborne equipment comprehensive detection system.
Background technology
The serviceability rate of airborne equipment is the key factor that ensures the aircraft normal flight.Past is that the airborne equipment manufacturer directly provides relevant detection equipment always, and main product is the manual checkout equipment of single cover still.The major defect that exists in the use is that complicated operation, function singleness, test period are long, and expense is higher, can not satisfy the demand of present civil aviaton, air force, Lu Hang, Hainan Airlines far away.
The airborne equipment comprehensive detection system at home and abroad is an emerging project, and its purpose is exactly the problems that exist in the checkout equipment of will solving over.At present, resemble large-scale synthesis checkout equipments such as ATEC6000 in the world, it adopts the vxi bus technology, uses supporting software, the detection of finishing multiple airborne equipment that can be automatic/semi-automatic.Advantage is that test item is many, efficient is high, but also have price high, the maintenance troubleshooting in problems such as service efficiency is low.
The utility model content
The utility model has overcome shortcoming of the prior art, the airborne equipment comprehensive detection system of a kind of maximization, synthesization is provided, can provide complete maintenance, troubleshooting and detection to airborne equipment, and can satisfy the detection of Boeing-737 NG aircraft airborne specialized equipment.
The technical solution of the utility model is: a kind of airborne equipment comprehensive detection system, comprise mainframe box, in described mainframe box, CPU is arranged, described CPU is connected with keyboard, mouse, hard disk, floppy drive, display and printer respectively, and described CPU is connected with bus card, D/S card, S/D card, DMS card, AX5488 card by the multiple-grooved telescopic backboard; The bus card of described mainframe box, D/S card, S/D card, DMS card are connected with terminal strip, and described terminal strip is connected with interface socket.
Between described terminal strip and interface socket, insert private adapter.
Described private adapter comprises signal adapter circuit and modulate circuit, the signal adapter circuit is used for measured piece is inserted test circuit, modulate circuit is used for and will adjusts to suitable amplitude from the straight signal of friendship of the next varying level of special test interface, sends into circuitry for signal measurement.
Described terminal strip comprises bus adapter, and the oscillograph and the digital multimeter that are connected with bus adapter respectively.
Compared with prior art, the utility model has the advantages that: the utility model can be finished maintenance, troubleshooting, the Performance Detection of MCP, its advanced person's automatic control function, sophisticated software system, guaranteed real-time, accurate, the accurate detection of airborne MCP, and have self-checking function, can guarantee that system self works reliably.Use this airborne equipment comprehensive detection system, can improve maintenance, detection efficiency guarantees the integrity that civil aviaton is equipped, and ensures aircraft safety, high efficiency flight.Native system extends to Civil Aviation System, can satisfy civil aviaton's engineering, civil aviaton boat and repair the maintenance demand of unit such as factory to airborne MCP.
Description of drawings
The utility model will illustrate by example and with reference to the mode of accompanying drawing, wherein:
Fig. 1 is a structural representation of the present utility model.
Embodiment
Disclosed all features in this instructions, or the step in disclosed all methods or the process except mutually exclusive feature and/or step, all can make up by any way.
Disclosed arbitrary feature in this instructions (comprising any accessory claim, summary and accompanying drawing) is unless special narration all can be replaced by other equivalences or the alternative features with similar purpose.That is, unless special narration, each feature is an example in a series of equivalences or the similar characteristics.
As shown in Figure 1, a kind of airborne equipment comprehensive detection system comprises mainframe box 1, terminal strip 2, private adapter 3 and interface socket 4, wherein:
Mainframe box: comprise industrial computer, industrial computer is connected with keyboard, mouse, hard disk, floppy drive, display, printer and multiple-grooved telescopic backboard respectively, and the multiple-grooved telescopic backboard is used to connect 429 bus cards, D/S card, S/D card, DMS card, AX5488 card etc.
Terminal strip: comprise bus adapter, and the oscillograph and the digital multimeter that are connected with bus adapter respectively.
For the signal that guarantees system's distinct interface, cable all can insert general purpose test equipment and need not to change the general purpose test equipment circuit, test macro adopts private adapter to connect measured piece 5 and general purpose test equipment.The special test adapter comprises signal adapter circuit (relay switch array) and modulate circuit, the signal adapter circuit switches by relay, each parts of system both can be interconnected by former complete machine connected mode, arbitrary parts can be inserted test circuit separately again.When switch arrays n-1 and switch arrays n '-1 closure and switch arrays n-2 and switch arrays n '-2 open, can directly connect by one group of lead between parts n and the n ', by this mode each parts is communicated with by former complete machine connected mode.If when the switch arrays n-1 of only closed certain parts n and switch arrays n-2, the cable of these parts is connected to the signal adapter output interface by the signal adapter special purpose interface, can make the interface of unit under test be connected to modulate circuit by universal test interface by the pilot relay action like this.Modulate circuit will be adjusted to suitable amplitude from the straight signal of friendship of the next varying level of special test interface, send into circuitry for signal measurement.
The above only is preferred embodiment of the present utility model; not in order to restriction the utility model; all any modifications of within spirit of the present utility model and principle, being done, be equal to and replace and improvement etc., all should be included within the protection domain of the present utility model.

Claims (4)

1. airborne equipment comprehensive detection system, it is characterized in that: comprise mainframe box, in described mainframe box, CPU is arranged, described CPU is connected with keyboard, mouse, hard disk, floppy drive, display and printer respectively, and described CPU is connected with bus card, D/S card, S/D card, DMS card, AX5488 card by the multiple-grooved telescopic backboard; The bus card of described mainframe box, D/S card, S/D card, DMS card are connected with terminal strip, and described terminal strip is connected with interface socket.
2. airborne equipment comprehensive detection system according to claim 1 is characterized in that: insert private adapter between described terminal strip and interface socket.
3. airborne equipment comprehensive detection system according to claim 2, it is characterized in that: described private adapter comprises signal adapter circuit and modulate circuit, the signal adapter circuit is used for measured piece is inserted test circuit, modulate circuit is used for and will adjusts to suitable amplitude from the straight signal of friendship of the next varying level of special test interface, sends into circuitry for signal measurement.
4. airborne equipment comprehensive detection system according to claim 1 is characterized in that: described terminal strip comprises bus adapter, and the oscillograph and the digital multimeter that are connected with bus adapter respectively.
CN2009203151116U 2009-11-18 2009-11-18 Comprehensive detecting system of airborne equipment Expired - Lifetime CN201589824U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2009203151116U CN201589824U (en) 2009-11-18 2009-11-18 Comprehensive detecting system of airborne equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2009203151116U CN201589824U (en) 2009-11-18 2009-11-18 Comprehensive detecting system of airborne equipment

Publications (1)

Publication Number Publication Date
CN201589824U true CN201589824U (en) 2010-09-22

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN2009203151116U Expired - Lifetime CN201589824U (en) 2009-11-18 2009-11-18 Comprehensive detecting system of airborne equipment

Country Status (1)

Country Link
CN (1) CN201589824U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102419402A (en) * 2011-08-23 2012-04-18 株洲高新技术产业开发区壹星科技有限公司 Locomotive comprehensive detection method and system device
CN103135012A (en) * 2012-12-21 2013-06-05 中国飞行试验研究院 Airplane direct current appliance function detector

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102419402A (en) * 2011-08-23 2012-04-18 株洲高新技术产业开发区壹星科技有限公司 Locomotive comprehensive detection method and system device
CN102419402B (en) * 2011-08-23 2015-06-24 株洲高新技术产业开发区壹星科技有限公司 Locomotive comprehensive detection method and system device
CN103135012A (en) * 2012-12-21 2013-06-05 中国飞行试验研究院 Airplane direct current appliance function detector

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GR01 Patent grant
C14 Grant of patent or utility model
CX01 Expiry of patent term

Granted publication date: 20100922

CX01 Expiry of patent term