CN215451976U - Aviation plug adapter device for instrument detection - Google Patents

Abstract

The utility model discloses an aviation plug adapter device for instrument detection, which comprises a base plate, an adapter plate and an aviation plug, wherein the adapter plate is arranged above the edge of the base plate, a plurality of aviation sockets are fixedly arranged on the adapter plate, and the aviation plug is matched with the aviation sockets. The device is connected the aviation socket with the equipment that needs to detect, and the different signal line on the equipment is connected with the socket that corresponds respectively, then is connected aviation plug and detecting instrument, and the different detection line on the instrument respectively with the plug connection that corresponds respectively, instrument and equipment pair connection can detect this moment through plug and socket. The switching device is suitable for the process of repeated detection of large-scale equipment, and a professional person is not required to repeatedly connect the data lines.

Description

Aviation plug adapter device for instrument detection

Technical Field

The utility model relates to the technical field of aviation plug integration, in particular to an aviation plug adapter device for instrument detection.

Background

The aviation plug is one of connectors, originates from the military industry, and is named as aviation plug for short. An aviation plug is an electromechanical component that connects electrical lines. The aviation plug can also be called a plug socket, is widely applied to various electric circuits and plays a role in connecting or disconnecting a circuit. The aviation plug generally comprises a plug and a socket, wherein the plug is also called a free-end aviation plug, and the socket is also called a fixed aviation plug. The connection and disconnection of the circuit are realized by the connection and disconnection of the plug, the socket and the plug, so that various connection modes of the plug and the socket are generated. For a circular aviation plug, three modes of threaded connection, bayonet connection and pin connection are mainly adopted. The most common screw connection has the advantages of simple processing technology, low manufacturing cost, wide application range and the like, but the connection speed is lower and is not suitable for occasions requiring frequent plugging and quick connection. The bayonet connection is fast because of the long lead of its three bayonet grooves, but it is complicated to manufacture and expensive. The pin tumbler type connection is the fastest connection speed of the three connection modes, and the pin tumbler type connection can realize the functions of connection, separation and locking only by linear motion without rotating. Because it belongs to the direct push-pull type connection mode, so only be applicable to the aviation plug that total separating force is little, generally be more common in small-size aviation plug.

When data detection such as temperature, pressure and the like is carried out on equipment in the prior art, a pin type aviation plug can be used for carrying out data connection, a socket is connected with the equipment needing to be detected through a lead, and a plug is connected with a detection instrument through a lead. Therefore, before testing equipment, the equipment needs to be conveniently arranged by the data lines and connected with the socket, especially, in some factories, the equipment needs to be tested for temperature, pressure and the like for many times, the workload for arranging the data lines of the equipment becomes huge, and the data lines of the equipment need to be classified and identified by professionals during detection every time, so that the equipment is very troublesome.

SUMMERY OF THE UTILITY MODEL

The utility model aims to provide an aviation plug adapter device for instrument detection, wherein an aviation socket on an adapter plate is connected with equipment to be detected, different signal wires on the equipment are respectively connected with corresponding sockets, then an aviation plug is connected with a detection instrument, different detection wires on the instrument are respectively connected with corresponding plugs, and at the moment, the instrument and the equipment can be detected through the matching connection of the plug and the socket. When the equipment that needs to detect is more, all be connected a plurality of equipment with aviation socket, only need a detector this moment can a plurality of equipment of adaptation, avoided the process of many times repeated connection data line.

In order to achieve the purpose, the technical scheme provided by the utility model is as follows: an aviation plug adapter device for instrument detection comprises a base plate and an adapter plate arranged above the edge of the base plate, and is characterized in that a plurality of aviation sockets are fixedly mounted on the adapter plate and penetrate through the adapter plate, each aviation socket comprises a first connecting area and a first selecting area, each first connecting area is provided with a connecting rod, one side, facing the base plate, of each connecting rod is electrically connected with equipment needing to be detected, one side, opposite to the base plate, of each first selecting area is provided with at least one limiting rod, and the number of the limiting rods of the aviation sockets is different in pairs;

still include with the aviation plug of aviation socket looks adaptation, the aviation plug includes second joining region and second selection district, the second joining region be equipped with the connecting hole of connecting rod looks adaptation, the connecting hole is sleeve structure, just the sleeve tip of connecting hole is connected with the instrument electricity that is used for the detection, the second selection district be equipped with the spacing hole of spacing pole looks adaptation on the first selection district, the aviation plug inserts the looks adaptation during the aviation socket, the gag lever post inserts spacing downthehole joint is fixed, the connecting rod inserts the joint is fixed in the connecting hole.

Furthermore, a fixing device for fixing the wiring harness is further arranged on the bottom plate.

Furthermore, the fixing device comprises a first supporting plate, a second supporting plate and a pressing plate, one end of the pressing plate is hinged to the first supporting plate, a clamping block is arranged at one end, close to the second supporting plate, of the pressing plate, sleeves are arranged on two sides of the top end of the second supporting plate, one opposite sides of the sleeves are both in an open shape, sliding blocks are arranged in the sleeves, one ends of the sliding blocks are elastically connected with the inner ends of the sleeves through springs, the other ends of the sliding blocks extend out of the open ends of the sleeves, the clamping blocks can be embedded between the two sleeves, and the sliding blocks are abutted to the clamping blocks.

Further, the pressing plate is a transparent plate.

Furthermore, the bottom of the fixture block is of an isosceles trapezoid structure, and one side, close to the fixture block, of the sliding block is provided with an inclined plane matched with the trapezoid inclined plane at the bottom of the fixture block.

Furthermore, the side surfaces of two sides of the clamping block are provided with anti-skid grains.

Further, the first connecting area and the first selecting area are both of a semicircular structure.

Further, the second connecting region and the second selection region are both semi-circular structures.

The utility model has the beneficial effects that:

1. the aviation plug adapter device for instrument detection is characterized in that an aviation socket on an adapter plate is connected with equipment to be detected, different signal lines on the equipment are respectively connected with corresponding sockets, then the aviation plug is connected with a detection instrument, different detection lines on the instrument are respectively connected with corresponding plugs, and at the moment, the instrument and the equipment can be detected through the matching connection of the plugs and the sockets. When the equipment that needs to detect is more, all be connected a plurality of equipment with aviation socket, only need a detector this moment can a plurality of equipment of adaptation, avoided the process of many times repeated connection data line. Therefore, the adapter plate is suitable for the process of repeated detection of large-scale equipment, and a professional person is not required to repeatedly connect the data line.

2. The aviation plug adapter device for instrument detection provided by the utility model has the advantages that the fixing device can be used for fixing the data line connected with the equipment and the aviation socket, so that the data line is prevented from being arranged in a scattered manner. The adapter plate is simple in structure and convenient to use.

Drawings

The accompanying drawings, which are incorporated in and constitute a part of the specification, illustrate embodiments of the utility model and together with the description, serve to explain the principles of the utility model. In the drawings, like reference numerals are used to indicate like elements. The drawings in the following description are directed to some, but not all embodiments of the utility model. For a person skilled in the art, other figures can be derived from these figures without inventive effort.

FIG. 1 is a schematic top view of an exemplary embodiment of an aircraft plug adapter for instrumentation;

fig. 2 is a schematic front structural view of an interposer of an aviation plug adapter device for instrumentation according to an embodiment of the present invention;

fig. 3 is a schematic front structural view of an aviation socket and an aviation plug of an aviation plug adapter device for instrument detection according to an embodiment of the present invention;

FIG. 4 is a schematic rear view of an exemplary embodiment of an aircraft plug adapter for instrumentation;

FIG. 5 is a schematic top view of a mounting assembly for an instrumented aircraft plug adapter in accordance with an embodiment of the present invention;

fig. 6 is a schematic side view of a second support plate of an aviation plug adapter device for instrumentation according to an embodiment of the present invention.

In the figure: 1. a base plate; 2. an adapter plate; 3. an aviation socket; 4. an aviation plug; 5. a fixing device; 301. a first connection region; 302. a first selection area; 303. a limiting rod; 304. a connecting rod; 401. a second attachment zone; 402. a second selection area; 403. a limiting hole; 404. connecting holes; 501. a first support plate; 502. a second support plate; 503. pressing a plate; 504. a clamping block; 505. a sleeve; 506. and a slider.

Detailed Description

In order to more clearly illustrate the embodiments of the present invention and the technical solutions in the prior art, the following description will be made with reference to the accompanying drawings. It is to be understood that the drawings in the following description are merely exemplary of the utility model and that other drawings and embodiments can be derived by those skilled in the art without undue burden. The designation of the design orientation merely indicates the relative positional relationship between the respective members, not the absolute positional relationship.

Please refer to fig. 1, fig. 2, and fig. 3. The embodiment of the utility model provides an aviation plug adapter device for instrument detection, which comprises a base plate 1 and an adapter plate 2 arranged above the edge of the base plate 1, wherein seven aviation sockets 3 are fixedly mounted on the adapter plate 2, the aviation sockets 3 penetrate through the adapter plate 2, each aviation socket 3 comprises a first connecting area 301 and a first selecting area 302, each first connecting area 301 is provided with a connecting rod 304, one side, facing the base plate 1, of each connecting rod 304 is electrically connected with equipment needing to be detected, one side, facing away from the base plate 1, of each first selecting area 302 is provided with at least one limiting rod 303, and the number of the limiting rods 303 of the aviation sockets 3 is different from each other in pairs. Wherein the first connection region 301 and the first selection region 302 are both semi-circular structures. The semicircular structure makes the plug and the socket more beautiful.

In this embodiment of the present invention, the first connection region 301 is used for connecting to a data line of a device to be tested, and the first selection region 302 is used for distinguishing different data lines of the device. For example, when the temperature and the pressure of the operation of the equipment need to be tested, the temperature data line is connected with the first connection area 301, only one limiting rod 303 is arranged in the first selection area above the temperature data line, namely, the temperature data line of the equipment corresponds to a socket with only one limiting rod, the pressure data line is connected with the first connection area 301 of the other socket, two limiting rods 303 are arranged in the first selection area above the temperature data line, namely, the pressure data line of the equipment corresponds to the socket with two limiting rods, when the equipment needs to be tested for multiple times, the temperature and the pressure joints of the equipment can be quickly and simply distinguished through the number of the limiting rods, the repeated identification and classification of professionals are not needed, and the time of a large number of workers can be saved. In some other embodiments, three limiting rods, four limiting rods, and five limiting rods may be further disposed in the first selection area 302.

In the embodiment of the present invention, the aviation plug 4 adapted to the aviation socket 3 is further included, the aviation plug 4 includes a second connection area 401 and a second selection area 402, the second connection area 401 is provided with a connection hole 404 adapted to the connection rod 304, the connection hole 404 is of a sleeve structure, a sleeve end of the connection hole 404 is electrically connected to an instrument for detection, the second selection area 402 is provided with a limit hole 403 adapted to the limit rod 303 in the first selection area 302, when the aviation plug 4 is inserted into the aviation socket 3, the limit rod 303 is inserted into the limit hole 403 to be clamped and fixed, and the connection rod 304 is inserted into the connection hole 404 to be clamped and fixed. Wherein the second connecting region 401 and the second selection region 402 are both semi-circular structures. The semicircular structure can make the socket and the plug more beautiful and clear.

In the embodiment of the present invention, the second connection region 401 is used for connecting with a detection line of a detection instrument, and the second selection region 402 is used for distinguishing different detection lines. For example, when the temperature data line of the device is connected with the socket of only one limiting rod in the first selection area and the pressure data line of the device is connected with the socket of only two limiting rods in the first selection area, the temperature detection line of the detection instrument is connected with the plug of only one limiting hole in the second selection area, and then the pressure detection line of the detection instrument is connected with the plug of only two limiting holes in the second selection area, so that the detection line of the detection instrument and the corresponding device data line can be connected in a paired manner.

When equipment is more, the data line with many equipment is connected with the socket electricity that corresponds respectively, for example, the temperature data line of a plurality of equipment all with the socket connection of only one gag lever post in the first selection district, the pressure data line all with the socket connection of only two gag lever posts in the first selection district, after the connection is accomplished, only need a detecting instrument that corresponds can carry out the adaptation with many equipment. The detecting instrument connects the temperature detecting line with the plug of only one limiting hole in the second selection area, and the pressure detecting line is connected with the plug of only two limiting holes in the second selection area. This detecting instrument all pairs with many equipment this moment, and an instrument can carry out a lot of detections to many equipment promptly, need not the professional and carries out data line classification and discernment many times, and the detection line of instrument pairs the completion back with the data line of equipment, only needs simple plug aviation plug to detect, saves a large amount of manpower and materials.

In the embodiment of the present invention, the limiting hole 403 in the second selection area 402 needs to be matched with the limiting rod 303 on the first selection area 302, and in some other embodiments, three limiting rods, four limiting rods, and five limiting rods may be further disposed in the first selection area 302. Correspondingly, three limiting holes, four limiting holes and five limiting holes may be further disposed in the second selection area 402.

Referring to fig. 4 and 5, the bottom plate 1 is further provided with a fixing device 5 for fixing a wire harness.

In the embodiment of the present invention, the fixing device 5 includes a first support plate 501, a second support plate 502, and a pressing plate 503 with one end hinged to the first support plate 501, a fixture block 504 is disposed at one end of the pressing plate 503 close to the second support plate 502, sleeves 505 are disposed at two sides of the top end of the second support plate 502, opposite sides of the sleeves 505 at two sides are open, a sliding block 506 is disposed in the sleeve 505, one end of the sliding block 506 is elastically connected to an inner end of the sleeve 505 through a spring, the other end of the sliding block 506 extends out of an open end of the sleeve 505, the fixture block 504 can be inserted into the middle of the two sleeves 505, and the sliding block 506 abuts against the fixture block 504.

After being connected the data line of equipment and socket, the data line can be accomodate inside fixing device 5, specifically, place the data line of equipment between first backup pad 501 and second backup pad 502, then rotate clamp plate 503 presses the data line inside the device, can avoid the data line to rock at will. The sliding block 506 is pressed towards the inside of the sleeves 505, then the latch 504 is embedded into the middle of the two sleeves 505, and due to the action of the spring, the sliding block 506 is ejected and then abuts against the latch 504, so that the latch 504 is latched between the two sleeves 505, and the pressing plate 503 is fixed.

In the embodiment of the present invention, the pressing plate 503 is a transparent plate. The transparent plate facilitates direct external observation of the internal conditions of the fixing device 5.

Referring to fig. 6, the bottom of the latch 504 is an isosceles trapezoid, and an inclined surface adapted to the trapezoid inclined surface at the bottom of the latch 504 is disposed on one side of the sliding block 506 close to the latch 504. Thus, when the clamping block 504 is pressed downwards, the trapezoidal inclined surface at the bottom of the clamping block 504 is abutted to the inclined surface of the sliding block 506, and when the clamping block 504 is pressed downwards continuously, the sliding block 506 generates an inward extrusion force on the sliding block 506, so that the sliding block 506 slides in the sleeve 505, the sliding block 506 does not need to be extruded by hands, and the clamping block 504 is convenient for a worker to directly press and fix the clamping block 504.

The side surfaces of the two sides of the fixture block 504 are provided with anti-skid threads. The anti-slip threads can enhance the friction between the sliding block 506 and the latch 504, further enhancing the stability of the fixing device 5.

The above-described aspects may be implemented individually or in various combinations, and such variations are within the scope of the present invention.

It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.

The foregoing is a more detailed description of the utility model in connection with specific preferred embodiments and it is not intended that the specific embodiments of the utility model be limited to these descriptions. For those skilled in the art to which the utility model pertains, several simple deductions or substitutions can be made without departing from the spirit of the utility model, and all shall be considered as belonging to the protection scope of the utility model.

Claims (8)

1. The aviation plug adapter device for instrument detection comprises a base plate (1) and an adapter plate (2) arranged above the edge of the base plate (1), and is characterized in that a plurality of aviation sockets (3) are fixedly mounted on the adapter plate (2), the aviation sockets (3) penetrate through the adapter plate (2), each aviation socket (3) comprises a first connecting area (301) and a first selecting area (302), each first connecting area (301) is provided with a connecting rod (304), one side, facing the base plate (1), of each connecting rod (304) is electrically connected with equipment needing to be detected, one side, facing away from the base plate (1), of each first selecting area (302) is provided with at least one limiting rod (303), and the number of the limiting rods (303) of the aviation sockets (3) is different from one another in pairs;

still include with aviation plug (4) of aviation socket (3) looks adaptation, aviation plug (4) include second joining region (401) and second selection district (402), second joining region (401) be equipped with connecting hole (404) of connecting rod (304) looks adaptation, connecting hole (404) are sleeve structure, just the sleeve tip of connecting hole (404) is connected with the instrument electricity that is used for detecting, second selection district (402) be equipped with spacing hole (403) of spacing pole (303) looks adaptation on first selection district (302), aviation plug (4) insert the looks adaptation when aviation socket (3), spacing pole (303) insert the joint is fixed in spacing hole (403), connecting rod (304) insert the joint is fixed in connecting hole (404).

2. An aviation plug adapter device for instrumental testing according to claim 1, wherein the base plate (1) is further provided with fixing means (5) for fixing a wiring harness.

3. The aviation plug adapter device for instrument testing according to claim 2, the fixing device (5) comprises a first supporting plate (501), a second supporting plate (502) and a pressing plate (503) with one end hinged with the first supporting plate (501), one end of the pressure plate (503) close to the second supporting plate (502) is provided with a clamping block (504), sleeves (505) are arranged on two sides of the top end of the second supporting plate (502), one opposite side of each sleeve (505) on two sides is in an open shape, a sliding block (506) is arranged in the sleeve (505), one end of the sliding block (506) is elastically connected with the inner end part of the sleeve (505) through a spring, the other end of the sliding block (506) extends out of the opening end of the sleeve (505), the fixture block (504) can be embedded between the two sleeves (505), and the sliding block (506) is abutted against the fixture block (504).

4. The aircraft plug adapter device for instrumental testing according to claim 3, wherein the pressure plate (503) is a transparent plate.

5. The aviation plug adapter device for instrumental testing according to claim 3, wherein the bottom of the clamping block (504) is in an isosceles trapezoid structure, and an inclined surface matched with the trapezoid inclined surface at the bottom of the clamping block (504) is arranged on one side, close to the clamping block (504), of the sliding block (506).

6. The aviation plug adapter device for instrumental testing according to claim 3, wherein the side surfaces of the fixture block (504) are provided with anti-slip threads.

7. An aircraft plug adapter device for instrumental testing according to claim 1, characterised in that said first connection zone (301) and said first selection zone (302) are both of semicircular configuration.

8. An aviation plug adapter device for instrumental testing according to claim 1, wherein the second connection zone (401) and the second selection zone (402) are both semicircular in configuration.

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