阅读说明：本技术 一种飞机维修检测用辅助装置 (Auxiliary device for aircraft maintenance and detection ) 是由 赵艳启 于 2020-08-11 设计创作，主要内容包括：本发明公开了一种便于飞机维修检测用辅助测量设备,包括电脑设备壳体、插头底座以及检测测量板；插头底座设置在电脑设备壳体的底部面上,并通过铆钉孔洞使用铆钉铆接固定,其中铆钉孔洞分布在四个角,每个角各一个；在电脑设备壳体的中部固定安装一个凹形线束固定支架并同时设置一个L形固定卡扣与之搭配使用；在电脑设备壳体的前部固定安装有把手和标识牌；电脑设备壳体通过多根航空专用导线与检测测量板连接；航空专用导线的一端通过压接航空插钉导入到插头底座中,航空专用导线的另一端通过压接航空插孔导入到检测测量板中的检测插孔里面,使之能够完整的导通。设备的使用能够快速、方便、准确的完成测量。(The invention discloses auxiliary measuring equipment convenient for aircraft maintenance and detection, which comprises a computer equipment shell, a plug base and a detection measuring plate, wherein the plug base is provided with a plug hole; the plug base is arranged on the bottom surface of the computer equipment shell and is riveted and fixed by rivets through rivet holes, wherein the rivet holes are distributed at four corners, and one is arranged at each corner; the middle part of the computer equipment shell is fixedly provided with a concave wiring harness fixing bracket and is also provided with an L-shaped fixing buckle for matching use; the front part of the computer equipment shell is fixedly provided with a handle and a signboard; the computer equipment shell is connected with the detection measuring plate through a plurality of aviation special wires; one end of the aviation dedicated wire is led into the plug base through the crimping aviation plug pin, and the other end of the aviation dedicated wire is led into the detection jack in the detection measuring plate through the crimping aviation jack, so that the aviation dedicated wire can be completely conducted. The use of the device can complete the measurement quickly, conveniently and accurately.)

1. An auxiliary device for aircraft maintenance inspection, comprising: a special lead, a computer equipment shell and a detection measuring board, wherein the computer equipment shell is connected with the detection measuring board through the special lead,

the computer equipment shell is an L-shaped opening box body, a rivet hole is arranged on the inner side surface of the computer equipment shell and used for fixing the plug base through the matching of rivets, a fixing support is arranged in the middle of the side surface of the bottom surface of the computer equipment shell, two ends of the top surface of the fixing support are respectively provided with a groove and a bulge, the middle of the fixing support is U-shaped, the groove and the bulge are matched with the fixing buckle, the front side surface of the outer side of the computer equipment shell is sequentially provided with a handle and a signboard from top to bottom,

the utility model discloses a portable electronic device, including detection measuring plate, digital identification area, middle equidistance, a plurality of lines detection jack, it is equipped with light illumination case to detect measuring plate upper end, both ends side is equipped with detection jack apron about detecting measuring plate one side, and the centre is equipped with english identification area, it vertically is equipped with digital identification area to detect measuring plate one end, and middle equidistance is equipped with the detection jack, a plurality of lines detect the horizontal setting of jack, are the diagonal direction setting of array, it is equipped with the solid fixed ring of pencil in the middle of the detection measuring plate another side, the solid.

2. An auxiliary device for aircraft maintenance inspection according to claim 1, wherein: the special wire is formed by winding five wires into one wire through an insulating tape, and the two ends of the special wire are respectively provided with a crimping aviation plug pin and a crimping aviation jack.

3. An auxiliary device for aircraft maintenance inspection according to claim 1, wherein: the light illumination box is characterized in that a battery box is arranged on the inner side face of the light illumination box, a light strip is arranged on the bottom face of the light illumination box, a battery cover plate is arranged at a position, corresponding to the battery box, on the outer side face of the light illumination box, and a jack is arranged above the battery cover plate in an inclined mode.

The technical field is as follows:

the invention belongs to the field of auxiliary devices for aircraft maintenance, and particularly relates to an auxiliary device for aircraft maintenance detection.

Background art:

at present, in the maintenance of an airplane, a great number of test works need to be completed by maintenance personnel, so that on the premise of ensuring safety, it is very important to complete each detection in the shortest time and quickly obtain feedback, and the length of maintenance work hours is also very important to the operation of an airline company. However, in the actual airplane maintenance test work, many problems exist, such as narrow maintenance detection position, insufficient light, short multi-department coordination work time, lack of equipment and the like, which greatly affect the maintenance detection work, lead to the reduction of work efficiency, increase of airplane maintenance time and delay of company operation. In ordinary maintenance and detection work, a maintenance worker needs to drill into an electronic equipment cabin (the space is very narrow and the light is insufficient and the noise is huge), pull out a computer, measure data such as inductance and resistance between jacks on a plug behind an airplane-end computer by using a multimeter and an LCR detector according to a work card, and judge whether related systems are good or bad according to data results. Therefore, when the maintenance and measurement work is performed in the narrow space, the light is insufficient, the body is curled, the time is long, the noise is large, and the number of disturbance factors is excessive, which may cause inaccurate measurement results, distorted detection data, and repeated detection. And only one person can operate, and the mutual inspection work of the work is very difficult to execute.

The invention content is as follows:

in order to solve the above technical problem, the present invention provides an auxiliary device for aircraft maintenance and inspection, including: a special lead, a computer equipment shell and a detection measuring board, wherein the computer equipment shell is connected with the detection measuring board through the special lead,

the computer equipment shell is an L-shaped opening box body, a rivet hole is arranged on the inner side surface of the computer equipment shell and used for fixing the plug base through the matching of rivets, a fixing support is arranged in the middle of the side surface of the bottom surface of the computer equipment shell, two ends of the top surface of the fixing support are respectively provided with a groove and a bulge, the middle of the fixing support is U-shaped, the groove and the bulge are matched with the fixing buckle, the front side surface of the outer side of the computer equipment shell is sequentially provided with a handle and a signboard from top to bottom,

the utility model discloses a portable electronic device, including detection measuring plate, digital identification area, middle equidistance, a plurality of lines detection jack, it is equipped with light illumination case to detect measuring plate upper end, both ends side is equipped with detection jack apron about detecting measuring plate one side, and the centre is equipped with english identification area, it vertically is equipped with digital identification area to detect measuring plate one end, and middle equidistance is equipped with the detection jack, a plurality of lines detect the horizontal setting of jack, are the diagonal direction setting of array, it is equipped with the solid fixed ring of pencil in the middle of the detection measuring plate another side, the solid.

According to the technical scheme, the special wire is formed by winding five wires into one wire through an insulating tape, and the two ends of the special wire are respectively provided with a crimping aviation plug pin and a crimping aviation jack.

According to the technical scheme, a battery box is arranged on the inner side face of the lamplight illumination box, a lamplight strip is arranged on the bottom face of the lamplight illumination box, a battery cover plate is arranged at the position, corresponding to the battery box, of the outer side face of the lamplight illumination box, and a jack is arranged above the battery cover plate in an inclined mode.

Compared with the prior art, the invention has the beneficial effects that: the computer equipment shell reduces the weight of the computer equipment shell, facilitates observation of internal connecting circuits and single-person operation; the arrangement of the concave wire harness fixing support and the L-shaped fixing buckle greatly facilitates the replacement requirement of the later-stage wires, and meanwhile, the wire harness fixing support adopts a concave design, so that the wire harness sinks, and the wire harness is firmer and durable, and the wire harness is ensured to be twisted back and forth in the using process without damage; the design of the aviation special wire can transfer maintenance and detection work which needs to be finished in an electronic cabin for a long time to the ground, thereby greatly reducing factors which are not beneficial to the maintenance and detection work, and ensuring the accuracy of a detection data result and the development of mutual detection work; in addition, the design of the light illumination box can facilitate the completion of maintenance and detection work under the condition of insufficient ground light, such as at night and other scenes without extra light setting, and the attention of maintenance personnel of the engineering can not be dispersed; the design of the detection jack cover plate can effectively avoid the entering of foreign objects, and the cover plate slides down to cover the detection jack when not in use.

Description of the drawings:

the accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the principles of the invention and not to limit the invention. In the drawings:

FIG. 1 is a schematic view of the overall structure of the present invention;

FIG. 2 is a schematic view of the connection of the wire and the plug pin receptacle of the present invention;

FIG. 3 is a rear view of a test measurement plate of the present invention;

FIG. 4 is a schematic view of the internal structure of the box for lighting of the present invention;

FIG. 5 is a schematic view of the identification of the detection measurement plate of the present invention;

FIG. 6 is a schematic view of the wrapping of the wire harness protective tape of the present invention;

FIG. 7 is a schematic view of the assembly and use of the computer device case of the present invention;

in the drawings: 1-special lead, 2-fixed bracket, 3-fixed buckle, 4-computer equipment shell, 5-plug base, 6-rivet hole, 7-handle, 8-signboard, 9-detection measuring plate, 11-detection jack cover plate, 12-detection jack, 13-light illumination box, 14-funnel-shaped wire harness bracket, 15-wire harness fixing ring, 16-compression aviation plug nail, 17-compression aviation jack, 18-battery cover plate, 19-battery box, 20-light strip, 21-insulating tape, 22-rivet, 23-English identification area and 24-digital identification area.

The specific implementation mode is as follows:

as shown in the drawings, an auxiliary device for aircraft maintenance detection includes: a special lead 1, a computer equipment shell 4 and a detection measuring board 9, wherein the computer equipment shell 4 is connected with the detection measuring board 9 through the special lead 1,

computer equipment casing 4 is L shape opening box, 4 medial surfaces of computer equipment casing are equipped with rivet hole 6, rivet hole 6 passes through rivet 22's cooperation stationary plug base 5, be equipped with fixed bolster 2 in the middle of 4 bottom surfaces of computer equipment casing, 2 top surfaces of fixed bolster both ends are equipped with recess and arch respectively, and the centre is the U-shaped, recess and arch are matchd with fixed buckle 3, fixed buckle 3 is L shape, 4 outside leading flank of computer equipment casing is equipped with from last to being equipped with handle 7 and signboard 8 down in proper order.

The detection and measurement device is characterized in that a lamplight illumination box 13 is arranged at the upper end of the detection and measurement plate 9, a battery box 19 is arranged on the inner side surface of the lamplight illumination box 13, a lamplight strip 20 is arranged on the bottom surface of the lamplight illumination box 13, a battery cover plate 18 is arranged at the position, corresponding to the battery box 19, on the outer side surface of the lamplight illumination box 13, a crimping aviation jack 17 is arranged obliquely above the battery cover plate 18, detection jack cover plates 11 are arranged on the upper and lower side surfaces of one side of the detection and measurement plate 9, an English identification area 23 is arranged in the middle of the detection and measurement plate, a digital identification area 24 is longitudinally arranged at one end of the detection and measurement plate 9, detection jacks 12 are arranged in the middle of the detection and measurement plate at equal intervals, the detection jacks 12 are transversely arranged in the diagonal direction of an array,

the special conductor 1 is formed by winding five conductors into one piece through an insulating tape 21, crimping aviation plug pins 16 and crimping aviation jacks 17 are respectively arranged at two ends of the special conductor 1, and the crimping aviation jacks 17 are connected with jacks.

The working principle is as follows: when in use, the computer to be measured is found strictly according to the instruction of the work list, and then the computer is pulled out and arranged. Then, a computer equipment shell 4 of the equipment is installed in a computer sliding groove at the end of an airplane, and a plug base 5 of the computer equipment shell 10 is connected with a plug at the end of the airplane in a matching mode. Then pick up and detect measuring board 9, slide the jack cover board spout 10 of detecting upwards, if light is dim, turn on light and carry out auxiliary lighting, follow the instruction according to the work order and carry out with corresponding instrument and find the jack that corresponds in the identification area that detects measuring board 9, then measure relevant data can.

The technical means disclosed by the scheme of the invention are not limited to the technical means disclosed by the technical means, and also comprise the technical scheme formed by equivalent replacement of the technical features. The present invention is not limited to the details given herein, but is within the ordinary knowledge of those skilled in the art.