Aviation part hole groove size detection device

Abstract

The utility model provides an aviation part hole groove size detection device comprising a measuring scale. One end of the measuring scale is fixedly connected with a conical hopper, the two sides of the other end of the measuring scale are fixedly connected with sheets respectively, one side of the measuring scale is provided with a first graduated scale, the other side of the measuring scale is provided with a sliding groove, and the outer surface of the measuring scale is slidably connected with an aperture measuring assembly; the hole diameter measuring assembly comprises a sliding part, the outer surface of the measuring scale is connected with the sliding part in a sliding mode, the two sides of the sliding part are connected with a first measuring part and a second measuring part respectively, a first locking part is installed on one side of the first measuring part, and a second locking part is installed on one side of the second measuring part. According to the utility model, through the mutual cooperation of the measuring scale, the conical hopper, the sheet and the aperture measuring assembly, the aperture and the aperture depth can be measured.

Description

Technical Field

[0001] This utility model relates to the field of hole and groove size detection technology for parts, and specifically to a device for detecting hole and groove size of aerospace parts. Background Technology

[0002] Currently, when inspecting the dimensions of holes and grooves in aerospace components, workers generally use vernier calipers. This is because vernier calipers reduce errors, and commercially available vernier calipers can measure not only hole depth and inner diameter but also outer diameter, and are inexpensive and portable. However, when using vernier calipers on workpieces with annular grooves on the inner wall of the hole, the workpiece... Figure 7 As shown in the half-section, the vernier caliper's jaws cannot reach into the hole to accurately measure the depth, resulting in poor adaptability of the vernier caliper during measurement. Utility Model Content

[0003] To address the shortcomings of existing technologies, this utility model provides a device for detecting the dimensions of holes and slots in aerospace components, thus solving the problems mentioned in the background art.

[0004] To achieve the above objectives, this utility model provides the following technical solution:

[0005] An aerospace component hole and slot size detection device includes a measuring ruler; one end of the measuring ruler is fixedly connected to a conical bucket, and the other end of the measuring ruler is fixedly connected to two thin plates on both sides. A first scale is provided on one side of the measuring ruler, and a sliding groove is provided on the other side of the measuring ruler. An aperture measuring component is slidably connected to the outer surface of the measuring ruler; the aperture measuring component includes a sliding component, and the outer surface of the measuring ruler is slidably connected to the sliding component. A first measuring component and a second measuring component are respectively connected to both sides of the sliding component. A first locking component is installed on one side of the first measuring component, and a second locking component is installed on one side of the second measuring component.

[0006] Furthermore, the sliding component includes a mouth-shaped block, the mouth-shaped block is slidably connected to the outer surface of the measuring ruler, a sliding block is fixedly connected to the inner surface of the mouth-shaped block, the sliding block slides within the sliding groove, and a locking bolt is threadedly connected to the sliding block, one end of the locking bolt being in contact with one side of the measuring ruler.

[0007] Furthermore, the sliding component also includes a connecting groove and a disc. Connecting grooves are provided on both sides of the mouth-shaped block. A first measuring component and a second measuring component are respectively connected to both sides of the mouth-shaped block through the connecting grooves. A disc is fixedly connected to both ends of one side of the mouth-shaped block. A first slot and a second slot are provided on one side of the disc.

[0008] Furthermore, the first measuring component includes a measuring rod, which is rotatably connected in the connecting groove. The top surface of the measuring rod is provided with a moving groove, and a second scale is provided on one side of the measuring rod. A pull rod is slidably connected inside the measuring rod, and a stop bar is fixedly connected to one end of the pull rod. A third scale is provided on one side of the pull rod, and a positioning bolt is threaded inside the measuring rod. One end of the positioning bolt is in contact with one side of the pull rod.

[0009] Furthermore, the second measuring component adopts the same structure as the first measuring component and is installed symmetrically.

[0010] Furthermore, the first locking component includes a rectangular plate, a rectangular plate is fixedly connected to one side of the measuring rod, an insert rod is slidably connected inside the rectangular plate, one end of the insert rod is respectively inserted into the first slot or the second slot, a reset damping rod is fixedly connected to one side of the rectangular plate, and one end of the reset damping rod is fixedly connected to the insert rod.

[0011] Furthermore, the second locking component adopts the same structure as the first locking component and is installed symmetrically.

[0012] This utility model provides a device for detecting the dimensions of holes and slots in aerospace components. Compared with the prior art, it has the following advantages:

[0013] 1. The depth of conical holes and cylindrical holes can be measured by using a measuring ruler in conjunction with a conical bucket. The height of the annular groove opened on the inner wall of the hole can be easily measured by using a measuring ruler in conjunction with a thin plate.

[0014] 2. By unfolding the first and second measuring components, it is convenient to detect the inner and outer apertures later.

[0015] 3. By cooperating with the first locking component and the second locking component, the first measuring component and the second measuring component can be unfolded and stored, which facilitates later carrying and measurement. Attached Figure Description

[0016] To more clearly illustrate the technical solutions in the embodiments of this utility model or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0017] Figure 1 A schematic diagram of the overall structure of this utility model is shown;

[0018] Figure 2This diagram shows another view of the overall structure of the present invention;

[0019] Figure 3 A schematic diagram of the aperture measuring component of this utility model is shown;

[0020] Figure 4 This diagram shows another perspective of the aperture measuring component of this invention.

[0021] Figure 5 A schematic diagram of the structure of the first measuring component and the sliding component of this utility model is shown;

[0022] Figure 6 A schematic diagram of the structure of the first measuring component of this utility model is shown;

[0023] Figure 7 A schematic diagram of the half-section structure of the workpiece to be tested according to this utility model is shown;

[0024] The figure shows: 1. Measuring ruler; 2. Conical bucket; 3. Thin plate; 4. First scale; 5. Sliding groove; 6. Aperture measuring assembly; 61. Sliding component; 611. Mouth-shaped block; 612. Sliding block; 613. Locking bolt; 614. Connecting groove; 615. Disc; 616. First slot; 617. Second slot; 62. First measuring component; 621. Measuring rod; 622. Moving groove; 623. Second scale; 624. Pull rod; 625. Stop bar; 626. Third scale; 627. Positioning bolt; 63. Second measuring component; 64. First locking component; 641. Rectangular plate; 642. Insert rod; 643. Reset damping rod; 65. Second locking component. Detailed Implementation

[0025] To make the objectives, technical solutions, and advantages of the embodiments of this utility model clearer, the technical solutions in the embodiments of this utility model are described clearly and completely. Obviously, the described embodiments are only some embodiments of this utility model, not all embodiments. Based on the embodiments of this utility model, all other embodiments obtained by those skilled in the art without creative effort are within the protection scope of this utility model.

[0026] Example 1

[0027] To address the technical problems in the background section, the following device for detecting the dimensions of holes and slots in aerospace components is provided:

[0028] Combination Figures 1-6As shown, the aerospace component hole and slot size detection device provided by this utility model includes a measuring ruler 1; a conical bucket 2 is fixedly connected to one end of the measuring ruler 1, and thin plates 3 are fixedly connected to both sides of the other end of the measuring ruler 1, a first scale 4 is provided on one side of the measuring ruler 1, a sliding groove 5 is provided on the other side of the measuring ruler 1, and a hole diameter measuring component 6 is slidably connected to the outer surface of the measuring ruler 1; the hole diameter measuring component 6 includes a sliding component 61, the sliding component 61 is slidably connected to the outer surface of the measuring ruler 1, a first measuring component 62 and a second measuring component 63 are respectively connected to both sides of the sliding component 61, a first locking component 64 is installed on one side of the first measuring component 62, and a second locking component 65 is installed on one side of the second measuring component 63. The sliding component 61 includes a bevel block 611, which is slidably connected to the outer surface of the measuring ruler 1. A sliding block 612 is fixedly connected to the inner surface of the bevel block 611. The sliding block 612 slides within the sliding groove 5. A locking bolt 613 is threaded into the sliding block 612, and one end of the locking bolt 613 contacts one side of the measuring ruler 1. The sliding component 61 also includes a connecting groove 614 and a disc 615. Connecting grooves 614 are respectively provided on both sides of the bevel block 611. A first measuring component 62 and a second measuring component 63 are respectively connected to both sides of the bevel block 611 through the connecting grooves 614. A disc 615 is fixedly connected to both ends of one side of the bevel block 611. A first slot 616 and a second slot 617 are respectively provided on one side of the disc 615.

[0029] The depth of conical holes and cylindrical holes can be measured by using measuring ruler 1 in conjunction with conical bucket 2. The height of the annular groove opened on the inner wall of the hole can be easily measured by using measuring ruler 1 in conjunction with thin plate 3.

[0030] Example 2

[0031] like Figures 1-6 As shown, based on the above embodiments, this embodiment further provides the following:

[0032] The first measuring component 62 includes a measuring rod 621, which is rotatably connected within a connecting groove 614. A moving groove 622 is provided on the top surface of the measuring rod 621. A second scale 623 is provided on one side of the measuring rod 621. A pull rod 624 is slidably connected within the measuring rod 621. A stop bar 625 is fixedly connected to one end of the pull rod 624. A third scale 626 is provided on one side of the pull rod 624. A positioning bolt 627 is threaded into the measuring rod 621, with one end of the positioning bolt 627 contacting one side of the pull rod 624. The second measuring component 63 adopts the same structure as the first measuring component 62 and is symmetrically installed.

[0033] By unfolding the first measuring component 62 and the second measuring component 63, it is convenient to detect the inner and outer apertures later.

[0034] Example 3

[0035] like Figures 1-6 As shown, based on the above embodiments, this embodiment further provides the following:

[0036] The first locking component 64 includes a rectangular plate 641. The rectangular plate 641 is fixedly connected to one side of the measuring rod 621. A plug rod 642 is slidably connected inside the rectangular plate 641. One end of the plug rod 642 is inserted into either the first slot 616 or the second slot 617. A reset damping rod 643 is fixedly connected to one side of the rectangular plate 641, and one end of the reset damping rod 643 is fixedly connected to the plug rod 642. The second locking component 65 adopts the same structure as the first locking component 64 and is symmetrically installed.

[0037] By cooperating with the first locking component 64 and the second locking component 65, the first measuring component 62 and the second measuring component 63 can be unfolded and stored, making it convenient for later carrying and measurement.

[0038] Working principle and usage process of this utility model:

[0039] In use:

[0040] In use, firstly, move the insertion rod 642. As the insertion rod 642 moves, it stretches the reset damping rod 642. As the insertion rod 642 moves, one end of it disengages from the second slot 617. After disengagement, rotate the first measuring component 62 and the second measuring component 63. When the first measuring component 62 and the second measuring component 63 are perpendicular to the measuring scale 1, release the insertion rod 642. This allows the insertion rod 642 to reset under the action of the reset damping rod 643, allowing it to be inserted into the first slot 616. When measuring deep holes, first insert one end of the conical bucket 2 into the hole groove. Then, make the bottom surface of the orifice block 611 contact the top surface of the workpiece. After contact, the value coinciding with the bottom surface of the orifice block 611 and the first scale 4 can be read, thus achieving measurement. The hole depth of the workpiece is measured. When the hole diameter needs to be measured during the hole depth measurement, simply pull the pull rod 624, causing the pull rod 624 to move the stop rod 625, so that the stop rod 625 comes into contact with the inner wall of the hole. After contact, the second scale 623 and the third scale 626 cooperate to detect the hole diameter of the workpiece. When it is necessary to detect the height of the annular groove in the hole later, first, make the bottom surface of the orifice block 611 fit with the top surface of the workpiece. At this time, the thin plate 3 of the measuring ruler 1 is inserted into the hole and makes the thin plate 3 contact the bottom of the annular groove. Then, the reading is taken. After the reading, the measuring ruler 1 is moved again so that the thin plate 3 comes into contact with the top surface of the annular groove and the reading is taken again. Then, the height of the annular groove can be measured by the difference between the two readings.

[0041] It should be noted that, in this document, relational terms such as "first" and "second" are used only to distinguish one entity or operation from another, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Furthermore, the terms "comprising," "including," or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements includes not only those elements but also other elements not expressly listed, or elements inherent to such a process, method, article, or apparatus. Without further limitations, an element defined by the phrase "comprising one..." does not exclude the presence of other identical elements in the process, method, article, or apparatus that includes said element.

[0042] The above embodiments are only used to illustrate the technical solutions of this utility model, and are not intended to limit it. Although this utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art should understand that modifications can still be made to the technical solutions described in the foregoing embodiments, or equivalent substitutions can be made to some of the technical features. Such modifications or substitutions do not cause the essence of the corresponding technical solutions to deviate from the spirit and scope of the technical solutions of the embodiments of this utility model.

Claims

1. An apparatus for detecting the size of a hole or slot of an aircraft part, characterized in that: The utility model provides a kind of hole diameter measuring device, including measuring scale (1);The one end of the measuring scale (1) is fixedly connected with conical hopper (2), the other end of the measuring scale (1) is fixedly connected with sheet (3) respectively on both sides, the one side of the measuring scale (1) is provided with first scale (4), the other side of the measuring scale (1) is provided with sliding slot (5), the outer surface of the measuring scale (1) is slidably connected with aperture measuring assembly (6); The aperture measuring assembly (6) includes sliding component (61), the outer surface of the measuring scale (1) is slidably connected with sliding component (61), the both sides of the sliding component (61) are connected with first measuring component (62) and second measuring component (63) respectively, the one side of the first measuring component (62) is installed with first locking component (64), the one side of the second measuring component (63) is installed with second locking component (65).

2. The apparatus for detecting the size of a hole or slot of an aircraft part according to claim 1, characterized in that: The sliding component (61) includes mouth type block (611), the outer surface of the measuring scale (1) is slidably connected with mouth type block (611), the inner surface of the mouth type block (611) is fixedly connected with sliding block (612), the sliding block (612) is slid in sliding slot (5), the sliding block (612) is screw-threadedly connected with locking bolt (613), the one end of the locking bolt (613) and the one side of measuring scale (1) are in contact with each other.

3. The apparatus for detecting the size of a hole or slot of an aircraft part according to claim 2, characterized in that: The sliding component (61) further includes connecting groove (614) and disc (615), the both sides of the mouth type block (611) are provided with connecting groove (614) respectively, the both sides of the mouth type block (611) are connected with first measuring component (62) and second measuring component (63) respectively by connecting groove (614), the both ends of the one side of the mouth type block (611) are fixedly connected with disc (615) respectively, the one side of the disc (615) is provided with first slot (616) and second slot (617) respectively.

4. The apparatus for detecting the size of a hole or slot of an aircraft part according to claim 3, characterized in that: The first measuring component (62) includes measuring rod (621), connecting groove (614) is rotatably connected with measuring rod (621), the top surface of the measuring rod (621) is provided with moving groove (622), the one side of the measuring rod (621) is provided with second scale (623), the measuring rod (621) is slidably connected with pull rod (624) in, the one end of the pull rod (624) is fixedly connected with stop rod (625), the one side of the pull rod (624) is provided with third scale (626), the measuring rod (621) is screw-threadedly connected with positioning bolt (627), the one end of the positioning bolt (627) and the one side of pull rod (624) are in contact with each other.

5. The apparatus for detecting the size of a hole or slot of an aircraft part according to claim 4, characterized in that: The second measuring component (63) adopts the same structure with first measuring component (62), and is symmetrically installed.

6. The apparatus for detecting the size of a hole or slot of an aircraft part according to claim 5, characterized in that: Said first locking part (64) includes a rectangular plate (641), one side of the measuring rod (621) is fixedly connected with the rectangular plate (641), a plug rod (642) is slidably connected in the rectangular plate (641), one end of the plug rod (642) is respectively matched with the first insertion groove (616) or the second insertion groove (617), one side of the rectangular plate (641) is fixedly connected with a reset damping rod (643), one end of the reset damping rod (643) is fixedly connected with the plug rod (642).

7. The apparatus of claim 6, wherein: Said second locking part (65) adopts the same structure as the first locking part (64) and is symmetrically installed.

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