CN209321283U - A kind of aircraft maintenance interconnecting device - Google Patents

A kind of aircraft maintenance interconnecting device Download PDF

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Publication number
CN209321283U
CN209321283U CN201821682264.XU CN201821682264U CN209321283U CN 209321283 U CN209321283 U CN 209321283U CN 201821682264 U CN201821682264 U CN 201821682264U CN 209321283 U CN209321283 U CN 209321283U
Authority
CN
China
Prior art keywords
fixedly connected
interconnecting device
boxcar
steering column
aircraft maintenance
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 - Fee Related
Application number
CN201821682264.XU
Other languages
Chinese (zh)
Inventor
王卫章
陈少东
陈跃
傅勇
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.)
Suqian Taida Airport Equipment Co Ltd
Original Assignee
Suqian Taida Airport Equipment 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 Suqian Taida Airport Equipment Co Ltd filed Critical Suqian Taida Airport Equipment Co Ltd
Priority to CN201821682264.XU priority Critical patent/CN209321283U/en
Application granted granted Critical
Publication of CN209321283U publication Critical patent/CN209321283U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of aircraft maintenance interconnecting devicies, it is related to aircraft maintenance technical field, including interconnecting device, the inside of interconnecting device is fixedly connected with measurement terminal, the both ends of interconnecting device are fixedly connected with one end of boxcar, it is opened up in the middle part of boxcar fluted, sliding rail is fixedly connected in groove, sliding rail upper end is connected with adjusting block, conductor block is fixedly connected in the middle part of adjusting block, one end of conductor block is fixedly connected with one end of connecting terminal by electric wire, the other end of connecting terminal is fixedly connected through successively boxcar and interconnecting device and with measurement terminal, the other end of boxcar is fixedly connected with one end of cable, the other end of cable is fixedly connected with connector.The aircraft maintenance interconnecting device can have the function that be connected to connector lug and connecting terminal by setting adjusting block and conductor block, play the role of access, by setting adjusting block and sliding rail, different cables can be converted, the purpose of multi-functional connection is realized.

Description

A kind of aircraft maintenance interconnecting device
Technical field
The utility model relates to aircraft maintenance technical field, specially a kind of aircraft maintenance interconnecting device.
Background technique
When airborne equipment breaks down, technical staff would generally speculate the event of product according to schematic diagram, combination failure phenomenon Hinder reason, then dismount product and be modified, then upper machine verifying, if the non-troubleshooting of failure, needs suspected fault reason again. Since aircraft airborne equipment constitutes a complexity and huge system, each airborne equipment influence each other, and rely solely on schematic diagram Method with phenomenon of the failure suspected fault principle is very inefficient.In addition, technical staff often goes on business troubleshooting in outfield, Portable detection device and number of devices are limited, more increase the difficulty of troubleshooting work, and frequently dismounting product also leaves The hidden danger of damage product.In order to solve the above problem, originally practical to provide a kind of aircraft maintenance interconnecting device.
A kind of aircraft maintenance use disclosed in 204473170 U of Chinese utility model patent ublic specification of application CN Interconnecting device, the interconnecting device, although avoiding the maintenance mode frequently dismounted, the interconnecting device is inconvenient, function It is incomplete, it is unfavorable for promoting the use of.
Utility model content
(1) the technical issues of solving
In view of the deficiencies of the prior art, the utility model provides a kind of aircraft maintenance interconnecting device, solves existing Aircraft electrical inconvenient maintenance the problem of.
(2) technical solution
In order to achieve the above object, the utility model is achieved by the following technical programs: a kind of aircraft maintenance switching Equipment, including interconnecting device, the inside of the interconnecting device are fixedly connected with measurement terminal, and the both ends of the interconnecting device are fixedly connected with One end of boxcar, opens up in the middle part of the boxcar fluted, and sliding rail, the sliding rail upper end are fixedly connected in the groove It is connected with adjusting block, conductor block is fixedly connected in the middle part of the adjusting block, one end of the conductor block is solid by electric wire Surely one end of connecting terminal is connected, the other end of the connecting terminal is through successively boxcar and interconnecting device and solid with measurement terminal Fixed connection, the other end of the boxcar are fixedly connected with one end of cable, and the other end of the cable is fixedly connected with company The junction of connector, the cable and boxcar is fixedly connected with connector lug, and one end and the cable of the connector lug are fixed The other end of connection, the connector lug through boxcar and is located in groove;
The inside of the interconnecting device is equipped with steering column, and the bottom of the steering column is fixedly connected with revolving part, the steering Connectivity slot is offered in the middle part of column, is equipped with electric wire in the connectivity slot, the both ends of the electric wire are fixedly connected to limited block, institute One end that support rod is fixedly connected on the outside of limited block is stated, the other end of the support rod runs through steering column and the company of being fixedly connected with Fishplate bar, the support rod are circumferentially with rubber pad, and one end of the rubber pad is fixedly connected with connecting plate, the rubber pad The other end is fixedly connected with steering column.
Optionally, the adjusting block, connector lug, support rod, limited block and connecting plate are conductor, and the interconnecting device turns Changing box, adjusting block and steering column is insulator.
Optionally, the cable has two, and two cables are respectively two-phase electric wire and three-phase wire.
Optionally, the junction of the connector lug and conductor block is arc, and the connector lug and conductor block are fitted and connected, institute State conductor block at least there are three.
Optionally, through-hole is offered inside the measurement terminal, the connecting plate is arc, the connecting plate and measurement end Son is fitted and connected.
Optionally, the upper end of the steering column is fixedly connected with handle, and the handle is rectangle, and the handle is insulation material Material.
Optionally, the measurement terminal has multiple, and multiple measurement terminal rectangular array distributions, the steering column is located at each Between the every two measurement terminal of row.
(3) beneficial effect
The utility model provides a kind of aircraft maintenance interconnecting device, have it is following the utility model has the advantages that
(1), the aircraft maintenance interconnecting device, by setting adjusting block and conductor block, can reach connection connector lug and The effect of connecting terminal, plays the role of access, by setting adjusting block and sliding rail, can convert different cables, real The purpose of multi-functional connection is showed.
(2), the aircraft maintenance interconnecting device, by be arranged steering column, realize every two measurement terminal access and The effect of open circuit plays the role of compression and buffering, in this way simple design method, a side by the way that rubber pad is arranged Face realizes the purpose of switching, has on the other hand achieved the effect that just to operate, and solves existing aircraft electrical inconvenient maintenance Problem.
Detailed description of the invention
FIG. 1 is a schematic structural view of the utility model;
Fig. 2 is the structural profile illustration of the utility model boxcar;
Fig. 3 is the structural profile illustration of the utility model interconnecting device;
Fig. 4 is the structural profile illustration of the utility model steering column.
In figure: interconnecting device 1, measurement terminal 101, boxcar 2, groove 201, sliding rail 202, adjusting block 3, connecting terminal 301, Electric wire 302, conductor block 303, cable 4, connector 401, connector lug 402, steering column 5, revolving part 501, connectivity slot 502, branch Strut 6, limited block 601, connecting plate 602, rubber pad 603.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole Embodiment.
In the description of the present invention, it should be understood that term " center ", " length ", " width ", " thickness ", The side of the instructions such as "upper", "lower", "front", "rear", "vertical", "horizontal", "top", "bottom", "inner", "outside", " axial direction ", " circumferential direction " Position or positional relationship are to be based on the orientation or positional relationship shown in the drawings, and are merely for convenience of description the utility model and simplification is retouched It states, rather than the device or element of indication or suggestion meaning must have a particular orientation, be constructed and operated in a specific orientation, Therefore it should not be understood as limiting the present invention.
In the present invention unless specifically defined or limited otherwise, term " setting ", " connected ", " connects " installation " Connect ", the terms such as " fixation " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection;It can be machine Tool connection;It can be directly connected, it can also be indirectly connected through an intermediary.For those of ordinary skill in the art and Speech, can understand the concrete meaning of above-mentioned term in the present invention as the case may be.
The meaning of " plurality " is two or more in the description of the present invention, unless otherwise clearly specific It limits.
Fig. 1-4 is please referred to, the utility model provides a kind of technical solution: a kind of aircraft maintenance interconnecting device, including turn Box 1 is connect, the inside of interconnecting device 1 is fixedly connected with measurement terminal 101, and the both ends of interconnecting device 1 are fixedly connected with the one of boxcar 2 End, the middle part of boxcar 2 open up fluted 201, and sliding rail 202 is fixedly connected in groove 201, and 202 upper end of sliding rail is flexibly connected There is adjusting block 3, by setting adjusting block 3 and sliding rail 202, different cables 4 can be converted, realize the mesh of multi-functional connection The middle part of adjusting block 3 be fixedly connected with conductor block 303, by setting adjusting block 3 and conductor block 303, connection can be reached and connect The effect of the end of a thread 402 and connecting terminal 301, plays the role of access, and one end of conductor block 303 connects by the way that electric wire 302 is fixed One end of connecting terminal 301 is connect, the other end of connecting terminal 301 is through successively boxcar 2 and interconnecting device 1 and and measurement terminal 101 are fixedly connected, and the other end of boxcar 2 is fixedly connected with one end of cable 4, and the other end of cable 4 is fixedly connected with company The junction of connector 401, cable 4 and boxcar 2 is fixedly connected with connector lug 402, one end of connector lug 402 and cable 4 It is fixedly connected, the other end of connector lug 402 through boxcar 2 and is located in groove 201;
The inside of interconnecting device 1 is equipped with steering column 5, by the way that steering column 5 is arranged, realizes the logical of every two measurement terminal 101 The effect on road and open circuit, the bottom of steering column 5 are fixedly connected with revolving part 501, and the middle part of steering column 5 offers connectivity slot 502, Electric wire 302 is equipped in connectivity slot 502, the both ends of electric wire 302 are fixedly connected to limited block 601, and the outside of limited block 601 is fixed The other end of one end of connection support bar 6, support rod 6 through steering column 5 and is fixedly connected with connecting plate 602, the week of support rod 6 To rubber pad 603 is equipped with, by the way that rubber pad 603 is arranged, play the role of compression and buffering, one end of rubber pad 603 and company Fishplate bar 602 is fixedly connected, and the other end of rubber pad 603 is fixedly connected with steering column 5, in this way simple design method, and one Aspect realizes the purpose of switching, has on the other hand achieved the effect that just to operate, and solves existing aircraft electrical inconvenient maintenance The problem of.
A kind of optional technical solution as the utility model: adjusting block 3, connector lug 402, support rod 6, limited block 601 It is conductor with connecting plate 602, interconnecting device 1, boxcar 2, adjusting block 3 and steering column 5 are insulator.
A kind of optional technical solution as the utility model: cable 4 has two, and two cables 4 are respectively two-phase Electric wire and three-phase wire, multiple and different routes, which is arranged, can connect a variety of power lugs, reach multi-functional purpose.
A kind of optional technical solution as the utility model: the junction of connector lug 402 and conductor block 303 is arc, Connector lug 402 and conductor block 303 are fitted and connected, conductor block 303 at least there are three, set connector lug 402 and conductor block 303 to Arc compares fastening in connection, it is not easy to loosen.
A kind of optional technical solution as the utility model: through-hole, connecting plate 602 are offered inside measurement terminal 101 For arc, connecting plate 602 is fitted and connected with measurement terminal 101.
A kind of optional technical solution as the utility model: the upper end of steering column 5 is fixedly connected with handle, and handle is square Shape, handle are insulating materials, and setting insulating materials can prevent from leaking electricity, and improve safety.
A kind of optional technical solution as the utility model: measurement terminal 101 has multiple, and multiple measurement terminals 101 are in Rectangular array distribution, steering column 5 are located between the every two measurement terminal 101 of each row.
In conclusion the aircraft maintenance interconnecting device, when in use, first according to the connector of maintenance to connector 401 into Row selection, by connector 401, with aircraft and more exchange device is connect after choosing, then slidable adjustment block 3, the general of adjusting block 3 Connector lug 402 is connected to connecting terminal 301, and the steering column 5 of the position selection different location then measured as needed makes to turn to Column 5 is rotated by 90 °, and is made 101 open circuit of measurement terminal at 5 both ends of steering column, is then accessed other equipment and repair detection, wherein The upper end of steering column 5 is fixedly connected with handle, and handle is rectangle, and handle is insulating materials, and setting insulating materials being capable of anti-leak-stopping Electricity, improves safety, and measurement terminal 101 has multiple, and multiple 101 rectangular arrays of measurement terminal distributions, steering column 5 is located at each Between the every two measurement terminal 101 of row, the junction of connector lug 402 and conductor block 303 is arc, by connector lug 402 and is led Body block 303 is set as arc, compares fastening in connection, it is not easy to loosen, cable 4 has two, and two cables 4 are respectively Two-phase electric wire and three-phase wire, multiple and different routes, which is arranged, can connect a variety of power lugs, reach multi-functional purpose, branch Strut 6 is circumferentially with rubber pad 603, by setting rubber pad 603, plays the role of compression and buffering, rubber pad 603 One end is fixedly connected with connecting plate 602, and the other end of rubber pad 603 is fixedly connected with steering column 5, in this way simple design Method, on the one hand realizes the purpose of switching, has on the other hand achieved the effect that just to operate, and solves existing aircraft electrical dimension Repair inconvenient problem.
It should be noted that in the present invention unless specifically defined or limited otherwise, fisrt feature is in the second spy It can be that the first and second features directly contact or the first and second features are connect indirectly by intermediary "above" or "below" sign Touching.Moreover, fisrt feature can be above the second feature " above ", " above " and " above " fisrt feature right above second feature or Oblique upper, or first feature horizontal height is merely representative of higher than second feature.Fisrt feature second feature " under ", " lower section " " following " can be fisrt feature and be directly under or diagonally below the second feature, or is merely representative of first feature horizontal height and is less than Second feature.
The preferable specific embodiment of the above, only the utility model, but the protection scope of the utility model is not It is confined to this, anyone skilled in the art is within the technical scope disclosed by the utility model, practical according to this Novel technical solution and its utility model design are subject to equivalent substitution or change, should all cover the protection model in the utility model Within enclosing.

Claims (7)

1. a kind of aircraft maintenance interconnecting device, including interconnecting device (1), it is characterised in that: the inside of the interconnecting device (1) is fixed It is connected with measurement terminal (101), the both ends of the interconnecting device (1) are fixedly connected with one end of boxcar (2), the boxcar (2) it opens up fluted (201), is fixedly connected with sliding rail (202) in the groove (201), sliding rail (202) upper end in the middle part of It is connected with adjusting block (3), is fixedly connected with conductor block (303) in the middle part of the adjusting block (3), the conductor block (303) One end be fixedly connected with one end of connecting terminal (301) by electric wire (302), the other end of the connecting terminal (301) runs through It successively boxcar (2) and interconnecting device (1) and is fixedly connected with measurement terminal (101), the other end of the boxcar (2) is fixed to be connected Connect one end of cable (4), the other end of the cable (4) is fixedly connected with connector (401), the cable (4) with The junction of boxcar (2) is fixedly connected with connector lug (402), and one end and cable (4) of the connector lug (402) are fixed to be connected It connects, the other end of the connector lug (402) through boxcar (2) and is located in groove (201);
The inside of the interconnecting device (1) is equipped with steering column (5), and the bottom of the steering column (5) is fixedly connected with revolving part (501), it is offered connectivity slot (502) in the middle part of the steering column (5), is equipped with electric wire (302) in the connectivity slot (502), institute The both ends for stating electric wire (302) are fixedly connected to limited block (601), are fixedly connected with support rod on the outside of the limited block (601) (6) other end of one end, the support rod (6) through steering column (5) and is fixedly connected with connecting plate (602), the support Bar (6) is circumferentially with rubber pad (603), and one end of the rubber pad (603) is fixedly connected with connecting plate (602), the rubber The other end of rubber mat (603) is fixedly connected with steering column (5).
2. a kind of aircraft maintenance interconnecting device according to claim 1, it is characterised in that: the adjusting block (3), wiring Head (402), support rod (6), limited block (601) and connecting plate (602) are conductor, and the interconnecting device (1), is adjusted boxcar (2) Locking nub (3) and steering column (5) are insulator.
3. a kind of aircraft maintenance interconnecting device according to claim 1, it is characterised in that: the cable (4) has two Item, two cables (4) are respectively two-phase electric wire and three-phase wire.
4. a kind of aircraft maintenance interconnecting device according to claim 1, it is characterised in that: the connector lug (402) and The junction of conductor block (303) is arc, and the connector lug (402) and conductor block (303) are fitted and connected, the conductor block (303) there are three at least.
5. a kind of aircraft maintenance interconnecting device according to claim 1, it is characterised in that: the measurement terminal (101) Inside offers through-hole, and the connecting plate (602) is arc, and the connecting plate (602) is fitted and connected with measurement terminal (101).
6. a kind of aircraft maintenance interconnecting device according to claim 1, it is characterised in that: the steering column (5) it is upper End is fixedly connected with handle, and the handle is rectangle, and the handle is insulating materials.
7. a kind of aircraft maintenance interconnecting device according to claim 1, it is characterised in that: the measurement terminal (101) Have multiple, multiple measurement terminal (101) rectangular arrays distribution, the steering column (5) is located at the every two measurement terminal of each row (101) between.
CN201821682264.XU 2018-10-17 2018-10-17 A kind of aircraft maintenance interconnecting device Expired - Fee Related CN209321283U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821682264.XU CN209321283U (en) 2018-10-17 2018-10-17 A kind of aircraft maintenance interconnecting device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821682264.XU CN209321283U (en) 2018-10-17 2018-10-17 A kind of aircraft maintenance interconnecting device

Publications (1)

Publication Number Publication Date
CN209321283U true CN209321283U (en) 2019-08-30

Family

ID=67708238

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201821682264.XU Expired - Fee Related CN209321283U (en) 2018-10-17 2018-10-17 A kind of aircraft maintenance interconnecting device

Country Status (1)

Country Link
CN (1) CN209321283U (en)

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GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20190830

Termination date: 20201017

CF01 Termination of patent right due to non-payment of annual fee