Airplane stringer drilling device

Abstract

The utility model relates to the technical field of space flight and aviation, and discloses an aircraft stringer drilling device, an aircraft stringer comprises a connecting plate and a web plate, the web plate is perpendicular to the connecting plate, the aircraft stringer drilling device comprises a clamping assembly, a drilling assembly and a drilling assembly, the clamping assembly is used for clamping the web plate and enabling the web plate to extend along a first direction and two sides of the web plate to face a second direction; the Y-axis moving sliding rail extends in the first direction, one end of the Y-axis moving sliding rail is connected with the clamping assembly, and a Y-axis moving part capable of moving in the first direction is installed on the Y-axis moving sliding rail; the X-axis moving sliding rail extends in the second direction, one end of the X-axis moving sliding rail is connected with the Y-axis moving part, an X-axis moving part capable of moving in the second direction is installed on the X-axis moving sliding rail, a drilling part is installed on the X-axis moving part, a drill bit of the drilling part extends in the second direction, and the drill bit is used for drilling a web; wherein the first direction is perpendicular to the second direction.

Description

Technical Field

[0001] This utility model relates to the field of aerospace technology, and in particular to a drilling device for aircraft stringers. Background Technology

[0002] As the number of aircraft in airlines increases, so does the amount of aircraft structural repair and modification. This includes cutting off a corroded section of the aircraft stringer, replacing it with a new section, and then installing a splicing strip at the cut location.

[0003] Aircraft stringers consist of connecting plates and webs, with the webs perpendicular to the connecting plates. When installing the overlap strips, holes need to be drilled in the webs of the aircraft stringers. Currently, the traditional manual drilling method involves using a handheld drill bit to drill holes in the webs of the aircraft stringers; however, the shape and position of the drilled holes are easily deviated, thus affecting the assembly accuracy of the overlap strips. Utility Model Content

[0004] The purpose of this invention is to provide a drilling device for aircraft stringers, which can improve the dimensional and positional accuracy of drilling holes in the web of aircraft stringers.

[0005] To achieve the above objectives, this utility model provides a drilling device for an aircraft stringer, wherein the aircraft stringer includes a connecting plate and a web plate, the web plate being perpendicular to the connecting plate, and includes:

[0006] A clamping assembly for clamping the web plate, such that the web plate extends along a first direction and has its sides facing a second direction;

[0007] Y-axis moving slide rail, the Y-axis moving slide rail extends along a first direction, one end of the Y-axis moving slide rail is connected to the clamping assembly, and a Y-axis moving component capable of moving along the first direction is mounted on the Y-axis moving slide rail;

[0008] An X-axis moving slide rail extends along a second direction, one end of which is connected to the Y-axis moving component. An X-axis moving component capable of moving along the second direction is mounted on the X-axis moving slide rail, and a drilling component is mounted on the X-axis moving component. The drill bit of the drilling component extends along the second direction and is used to drill holes in the web.

[0009] Wherein, the first direction and the second direction are perpendicular to each other.

[0010] Preferably, the X-axis moving component is equipped with a Z-axis moving slide rail extending along a third direction, and the aircraft stringer drilling device further includes:

[0011] Z-axis moving component, the Z-axis moving component is mounted on the Z-axis moving slide rail and can move along a third direction, and the drilling component is mounted on the Z-axis moving component;

[0012] The first direction, the second direction, and the third direction are perpendicular to each other.

[0013] Preferably, it further includes:

[0014] Z-axis drive unit, the Z-axis drive unit is used to drive the Z-axis moving member to move along the third direction, the Z-axis drive unit includes a Z-axis lead screw and a Z-axis gripping part, the Z-axis lead screw extends along the third direction and passes through the X-axis moving member and the Z-axis moving member, and the Z-axis gripping part is installed at one end of the Z-axis lead screw.

[0015] Preferably, the Z-axis moving part includes an adjusting part and a mounting part. The adjusting part is disposed on one side of the X-axis moving part in a third direction. The Z-axis lead screw passes through the X-axis moving part and the adjusting part. The mounting part is connected to one side of the adjusting part in a first direction. The Z-axis moving part is mounted on the side near the mounting part. The mounting part is mounted on the Z-axis moving slide rail. The drilling part is mounted on the mounting part.

[0016] The mounting part has a mounting hole that extends through a third direction. The drilling component is a right-angle drill. The handle of the right-angle drill is inserted into the mounting hole, and the drill bit of the right-angle drill extends along a second direction.

[0017] Preferably, there are two mounting parts, which are respectively connected to the two sides of the adjustment part in the first direction. The X-axis moving member is equipped with the Z-axis moving slide rail on both sides near the two mounting parts, and the mounting part is mounted on the corresponding Z-axis moving slide rail.

[0018] Preferably, it further includes:

[0019] Y-axis drive component, the Y-axis drive component is used to drive the Y-axis moving component to move along a first direction, the Y-axis drive component includes a Y-axis lead screw and a Y-axis gripping part, the Y-axis lead screw extends along the first direction and passes through the Y-axis moving component and the clamping assembly, and the Y-axis gripping part is installed at one end of the Y-axis lead screw.

[0020] Preferably, it further includes:

[0021] An X-axis drive unit is used to drive the X-axis moving member to move along a second direction. The X-axis drive unit includes an X-axis lead screw and an X-axis gripping part. The X-axis lead screw extends along the second direction and passes through the X-axis moving member and the Y-axis moving member. The X-axis gripping part is installed at one end of the X-axis lead screw.

[0022] Preferably, the clamping assembly includes a frame, two fixing blocks, and two positioning bolts:

[0023] Two fixing blocks are sequentially installed at the bottom of the frame along the second direction, and the positioning bolts extend along the second direction. The two positioning bolts pass through the two fixing blocks respectively, and a clamping opening for clamping the web is defined between the two positioning bolts.

[0024] One end of the Y-axis moving slide rail is connected to the frame.

[0025] Preferably, there are two clamping components, which are arranged sequentially and parallel to each other along the first direction, and the two ends of the Y-axis moving slide rail are respectively connected to the two clamping components.

[0026] Preferably, there are two Y-axis moving slide rails, which are arranged sequentially along the second direction and parallel to each other, and the two ends of the X-axis moving slide rail are respectively connected to the two Y-axis moving parts.

[0027] Compared with the prior art, the beneficial effects of this utility model embodiment of an aircraft stringer drilling device are as follows:

[0028] The aircraft's spandrel web is held in place by a clamping assembly. The web extends along a first direction and has its sides facing a second direction. When the X-axis moving component moves along the second direction on the X-axis sliding rail, it drives the drilling component to move synchronously. The drill bit of the drilling component extends along the second direction, passing through the web from one side to the other, thus drilling a hole in the web. Afterward, the X-axis moving component retracts, disengaging the drill bit from the web. When the Y-axis moving component moves along the first direction on the Y-axis sliding rail, it drives both the X-axis moving component and the drilling component to move along the first direction. This allows the drill bit of the drilling component to move to the next drilling position on the web along the first direction, creating multiple holes distributed along the first direction on the web.

[0029] Compared to manually drilling holes in the web of an aircraft strand using a handheld drill, this application uses a clamping assembly to hold and fix the web of the aircraft strand. By adjusting the position of the X-axis moving part in the second direction, the drill bit of the drilling component can drill holes in the web. By adjusting the position of the Y-axis moving part in the first direction, the drill bit of the drilling component can make multiple holes distributed along the first direction in the web. This results in higher dimensional and positional accuracy of the drilling in the web, which is more conducive to meeting the assembly accuracy requirements of the overlap strip. Attached Figure Description

[0030] Figure 1 This is a schematic diagram of the structure of the aircraft stringer drilling device described in this embodiment of the utility model;

[0031] Figure 2 This is a top view of the aircraft stringer drilling device described in this embodiment of the utility model;

[0032] Figure 3 This is a front view of the aircraft stringer drilling device described in this embodiment of the utility model;

[0033] Figure 4 This is a rear view of the aircraft stringer drilling device described in this embodiment of the utility model;

[0034] Figure 5 This is a side view of the aircraft stringer drilling device described in this embodiment of the present invention;

[0035] In the diagram, 1 is the aircraft stringer; 101 is the connecting plate; 102 is the web plate; 2 is the clamping assembly; 201 is the frame; 202 is the fixing block; 203 is the positioning bolt; 204 is the clamping port; 3 is the Y-axis moving slide rail; 4 is the Y-axis moving component; 5 is the X-axis moving slide rail; 6 is the X-axis moving component; 7 is the drilling component; 701 is the drill bit; 702 is the handle; 8 is the Z-axis moving slide rail; 9 is the Z-axis moving component; 901 is the adjusting part; 902 is the mounting part; 9021 is the mounting hole; 10 is the Z-axis drive component; 1001 is the Z-axis lead screw; 1002 is the Z-axis grip; 11 is the Y-axis drive component; 1101 is the Y-axis lead screw; 1102 is the Y-axis grip; 12 is the X-axis drive component; 1201 is the X-axis lead screw; 1202 is the X-axis grip. Detailed Implementation

[0036] The specific embodiments of this utility model will be described in further detail below with reference to the accompanying drawings and examples. The following examples are used to illustrate this utility model, but are not intended to limit its scope.

[0037] In the description of this utility model, it should be understood that, unless otherwise explicitly specified and limited, the terms "installation," "connection," and "joining" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium; and they can refer to the internal connection of two components. Those skilled in the art can understand the specific meaning of the above terms in the embodiments of this utility model based on the specific circumstances.

[0038] In the description of this utility model, it should be understood that the terms "first," "second," and "third" are used for descriptive purposes only and should not be construed as indicating or implying relative importance. Furthermore, the terms "upper," "lower," "left," "right," "front," "rear," "top," "bottom," "inner," "outer," "middle," "vertical," "horizontal," "lateral," "longitudinal," "X-axis direction," "Y-axis direction," and "Z-axis direction," etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings, and are only for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation, and therefore should not be construed as a limitation of this utility model. Moreover, some of the above terms, in addition to indicating orientation or positional relationship, may also be used to indicate other meanings; for example, the term "upper" may in some cases be used to indicate a certain dependency or connection relationship. Those skilled in the art can understand the specific meaning of these terms in this application according to the specific circumstances.

[0039] like Figure 1 As shown in the figure, an aircraft stringer drilling device according to an embodiment of the present invention includes an aircraft stringer 1 comprising a connecting plate 101 and a web plate 102, wherein the web plate 102 is perpendicular to the connecting plate 101 and includes: a clamping assembly 2, a Y-axis moving slide rail 3, and an X-axis moving slide rail 5.

[0040] The clamping assembly 2 is used to clamp the web plate 102, so that the web plate 102 extends along the first direction Y and is positioned on both sides toward the second direction X.

[0041] Y-axis moving slide rail 3 extends along the first direction Y. One end of Y-axis moving slide rail 3 is connected to clamping assembly 2. Y-axis moving component 4, which can move along the first direction Y, is installed on Y-axis moving slide rail 3.

[0042] X-axis moving slide rail 5 extends along the second direction X. One end of X-axis moving slide rail 5 is connected to Y-axis moving component 4. X-axis moving component 6, which can move along the second direction X, is installed on X-axis moving slide rail 5. Drilling component 7 is installed on X-axis moving component 6. Drill bit 701 of drilling component 7 extends along the second direction X. Drill bit 701 is used to drill holes in web plate 102.

[0043] Among them, the first direction Y and the second direction X are perpendicular to each other.

[0044] It should be noted that the clamping assembly 2 clamps the web 102 of the aircraft spanner 1. The web 102 extends along the first direction Y and is positioned with both sides facing the second direction X. When the X-axis moving member 6 moves along the second direction X on the X-axis moving slide rail 5, it can drive the drilling member 7 to move synchronously. The drill bit 701 of the drilling member 7 extends along the second direction X, passing from one side of the web 102 to the other side along the second direction X, thus drilling a hole in the web 102. Afterwards, the X-axis moving member 6 retracts, causing the drill bit 701 to disengage from the web 102. When the Y-axis moving member 4 moves along the first direction Y on the Y-axis moving slide rail 3, it can drive the X-axis moving member 6 and the drilling member 7 to move along the first direction Y, thereby moving the drill bit 701 of the drilling member 7 to the next position in the web 102 that needs to be drilled along the first direction Y, thus drilling multiple holes distributed along the first direction Y in the web 102.

[0045] Compared to manually drilling holes in the web 102 of the aircraft stringer 1 with a handheld drill, this application uses a clamping assembly 2 to clamp and fix the web 102 of the aircraft stringer 1. By adjusting the position of the X-axis moving part 6 in the second direction X, the drill bit 701 of the drilling part 7 can drill holes in the web 102. By adjusting the position of the Y-axis moving part 4 in the first direction Y, the drill bit 701 of the drilling part 7 can drill multiple holes distributed along the first direction Y in the web 102. The form and position accuracy of drilling the web 102 is higher, which is more conducive to meeting the assembly accuracy requirements of the overlapping strip.

[0046] like Figure 1 As shown, in a more specific embodiment, the X-axis moving member 6 is equipped with a Z-axis moving slide rail 8 extending along the third direction Z, and the aircraft stringer drilling device also includes: a Z-axis moving member 9.

[0047] Z-axis moving part 9 is mounted on Z-axis moving slide rail 8 and can move along the third direction Z. Drilling part 7 is mounted on Z-axis moving part 9.

[0048] Among them, the first direction Y, the second direction X, and the third direction Z are perpendicular to each other.

[0049] It should be noted that the Z-axis moving part 9 is mounted on the Z-axis moving slide rail 8 and can move along the third direction Z. The drilling part 7 is mounted on the Z-axis moving part 9. Therefore, when the Z-axis moving part 9 moves along the third direction Z, it can drive the drill bit 701 of the drilling part 7 to move along the third direction Z. Thus, when the drill bit 701 drills a hole in the web 102, it can adjust the height of the hole on the web 102 in the third direction Z, so as to adapt to the assembly of more types of overlapping strips.

[0050] like Figure 1-3 As shown, in a more specific embodiment, it also includes: a Z-axis drive 10;

[0051] Z-axis drive 10 is used to drive Z-axis moving member 9 to move along a third direction Z. Z-axis drive 10 includes Z-axis lead screw 1001 and Z-axis grip 1002. Z-axis lead screw 1001 extends along a third direction Z and passes through X-axis moving member 6 and Z-axis moving member 9. Z-axis grip 1002 is installed at one end of Z-axis lead screw 1001.

[0052] It should be noted that the Z-axis drive component 10 is mounted on the Z-axis sliding rail 8, the Z-axis lead screw 1001 extends along the third direction Z and passes through the X-axis moving component 6 and the Z-axis moving component 9, the Z-axis grip 1002 rotates, causing the Z-axis lead screw 1001 to rotate, the X-axis moving component 6 is fixed in the third direction Z, and the Z-axis moving component 9 can move along the Z-axis lead screw 1001 and the Z-axis sliding rail 8 in the third direction Z without rotating.

[0053] like Figure 1-3 As shown, in a more specific embodiment, the Z-axis moving member 9 includes an adjusting part 901 and a mounting part 902. The adjusting part 901 is disposed on the side of the X-axis moving member 6 in the third direction Z. The Z-axis lead screw 1001 passes through the X-axis moving member 6 and the adjusting part 901. The mounting part 902 is connected to the adjusting part 901 on the side in the first direction Y. The X-axis moving member 6 is mounted with a Z-axis moving slide rail 8 on the side near the mounting part 902. The mounting part 902 is mounted on the Z-axis moving slide rail 8. A drilling part 7 is mounted on the mounting part 902.

[0054] The mounting part 902 has a mounting hole 9021 that extends through the third direction Z. The drilling part 7 is a right-angle drill. The handle 702 of the right-angle drill is inserted into the mounting hole 9021, and the drill bit 701 of the right-angle drill extends along the second direction X.

[0055] It should be noted that the Z-axis moving part 9 includes an adjusting part 901 and a mounting part 902. The adjusting part 901 is located on the side of the X-axis moving part 6 in the third direction Z. The Z-axis lead screw 1001 passes through the X-axis moving part 6 and the adjusting part 901. The mounting part 902 is mounted on the Z-axis moving slide rail 8. The rotating Z-axis gripping part 1002 drives the Z-axis lead screw 1001 to rotate. The position of the X-axis moving part 6 in the third direction Z is fixed. The adjusting part 901 moves along the Z-axis lead screw 1001 in the third direction Z, driving the mounting part 902 to move along the Z-axis moving slide rail 8 in the third direction Z.

[0056] Since the mounting part 902 is located on the same side of the adjusting part 901 and the X-axis moving part 6 in the first direction Y, the handle 702 of the right angle drill can be inserted into the mounting hole 9021 on the mounting part 902, and there is no obstruction in the third direction Z. The drill bit 701 at one end of the right angle drill is outside the mounting hole 9021 and can drill a hole in the web plate 102. The other end of the right angle drill is connected to an electric wire to provide power to the drill bit 701.

[0057] like Figure 1 , 4 As shown, in a more specific embodiment, there are two mounting parts 902, which are respectively connected to the two sides of the adjusting part 901 in the first direction Y. The X-axis moving member 6 is equipped with Z-axis moving slide rails 8 on both sides near the two mounting parts 902, and the mounting parts 902 are mounted on the corresponding Z-axis moving slide rails 8.

[0058] It should be noted that there are two mounting parts 902, which are respectively connected to the two sides of the adjusting part 901 in the first direction Y. The X-axis moving part 6 is equipped with Z-axis moving slide rails 8 on both sides near the two mounting parts 902. The mounting parts 902 are mounted on the corresponding Z-axis moving slide rails 8. Therefore, the rotating Z-axis gripping part 1002 drives the Z-axis lead screw 1001 to rotate. The adjusting part 901 moves along the Z-axis lead screw 1001 in the third direction Z, and the two mounting parts 902 move along the two Z-axis moving slide rails 8 in the third direction Z.

[0059] Both mounting parts 902 are equipped with drilling components 7, that is, the two drilling components 7 are arranged sequentially in the first direction Y. Therefore, when the Z-axis moving component 9 moves along the second direction X, the drill bits 701 of the two drilling components 7 can drill holes in the web plate 102 at the same time, thereby improving the efficiency of drilling multiple holes in the web plate 102 in the first direction Y.

[0060] like Figure 3 As shown, in a more specific embodiment, it also includes: a Y-axis drive 11;

[0061] Y-axis drive 11 is used to drive Y-axis moving member 4 to move along the first direction Y. Y-axis drive 11 includes Y-axis lead screw 1101 and Y-axis gripping part 1102. Y-axis lead screw 1101 extends along the first direction Y and passes through Y-axis moving member 4 and clamping assembly 2. Y-axis gripping part 1102 is installed at one end of Y-axis lead screw 1101.

[0062] It should be noted that the Y-axis moving part 4 is mounted on the Y-axis moving slide rail 3, the Y-axis lead screw 1101 extends along the first direction Y and passes through the Y-axis moving part 4 and the clamping assembly 2, the Y-axis gripping part 1102 rotates, causing the Y-axis lead screw 1101 to rotate, the clamping assembly 2 is fixed in the first direction Y, and the Y-axis moving part 4 can move along the Y-axis lead screw 1101 and the Y-axis moving slide rail 3 in the third direction Z without rotating.

[0063] The Y-axis moving component 4 is mounted on the Y-axis moving slide rail 3, specifically: the Y-axis moving slide rail 3 passes through the Y-axis moving component 4.

[0064] like Figure 4-5 As shown, in a more specific embodiment, it also includes: an X-axis drive 12;

[0065] The X-axis drive 12 is used to drive the X-axis moving member 6 to move along the second direction X. The X-axis drive 12 includes an X-axis lead screw 1201 and an X-axis gripping part 1202. The X-axis lead screw 1201 extends along the second direction X and passes through the X-axis moving member 6 and the Y-axis moving member 4. The X-axis gripping part 1202 is installed at one end of the X-axis lead screw 1201.

[0066] It should be noted that the X-axis moving part 6 is mounted on the X-axis moving slide rail 5, the X-axis lead screw 1201 extends along the second direction X and passes through the X-axis moving part 6 and the Y-axis moving part 4, the X-axis grip 1202 rotates, causing the X-axis lead screw 1201 to rotate, the position of the Y-axis moving part 4 in the second direction X is fixed, and the X-axis moving part 6 can move along the X-axis lead screw 1201 and the X-axis moving slide rail 5 in the third direction Z without rotating.

[0067] The X-axis moving component 6 is mounted on the X-axis moving slide rail 5, specifically: the X-axis moving slide rail 5 passes through the X-axis moving component 6.

[0068] like Figure 5 As shown, in a more specific embodiment, the clamping assembly 2 includes a frame 201, two fixing blocks 202, and two positioning bolts 203:

[0069] Two fixing blocks 202 are installed sequentially at the bottom of the frame 201 along the second direction X. The positioning bolts 203 extend along the second direction X. The two positioning bolts 203 pass through the two fixing blocks 202 respectively, and the two positioning bolts 203 define a clamping opening 204 for clamping the web plate 102.

[0070] One end of the Y-axis moving slide rail 3 is connected to the frame 201.

[0071] It should be noted that the two fixing blocks 202 are installed sequentially at the bottom of the frame 201 along the second direction X, and the positioning bolts 203 extend along the second direction X. The two positioning bolts 203 pass through the two fixing blocks 202 respectively, and the two positioning bolts 203 define a clamping opening 204 for clamping the web plate 102. Thus, adjusting the distance between the two positioning bolts 203 can adjust the size of the clamping opening 204 to accommodate clamping and fixing web plates 102 of different thicknesses.

[0072] The bottom of rack 201 is also equipped with feet.

[0073] like Figure 1 As shown, in a more specific embodiment, there are two clamping components 2, which are arranged sequentially and parallel to each other along the first direction Y, and the two ends of the Y-axis moving slide rail 3 are respectively connected to the two clamping components 2.

[0074] It should be noted that there are two clamping components 2. The two clamping components 2 are arranged sequentially along the first direction Y and are parallel to each other, so that the two clamping components 2 clamp the two parts of the web plate 102 in the first direction Y, which can clamp the web plate 102 more stably.

[0075] Furthermore, two clamping components 2 are connected to both ends of the Y-axis moving slide rail 3 to ensure the stability of the Y-axis moving slide rail 3 as it extends along the first direction Y, and to ensure the stability of the movement of the Y-axis moving component 4.

[0076] When the Y-axis drive unit 11 includes the Y-axis lead screw 1101, the Y-axis lead screw 1101 also passes through the two clamping assemblies 2, improving the stability of the Y-axis lead screw 1101.

[0077] like Figure 1 As shown, in a more specific embodiment, there are two Y-axis moving slide rails 3. The two Y-axis moving slide rails 3 are arranged sequentially along the second direction X and are parallel to each other. The two ends of the X-axis moving slide rail 5 are respectively connected to two Y-axis moving parts 4.

[0078] It should be noted that there are two Y-axis moving slide rails 3. The two Y-axis moving slide rails 3 are arranged sequentially along the second direction X and are parallel to each other. The two ends of the X-axis moving slide rail 5 are respectively connected to two Y-axis moving parts 4 to ensure the stability of the X-axis moving slide rail 5 extending along the second direction X and to ensure the stability of the movement of the X-axis moving parts 6.

[0079] The working process of this utility model is as follows: The clamping assembly 2 clamps the web plate 102 of the aircraft spanner 1. The web plate 102 extends along the first direction Y and is arranged on both sides facing the second direction X. When the X-axis moving member 6 moves along the second direction X on the X-axis moving slide rail 5, it can drive the drilling member 7 to move synchronously. The drill bit 701 of the drilling member 7 extends along the second direction X and passes from one side of the web plate 102 to the other side along the second direction X to drill a hole in the web plate 102. Afterwards, the X-axis moving member 6 retracts, causing the drill bit 701 to disengage from the web plate 102. When the Y-axis moving member 4 moves along the first direction Y on the Y-axis moving slide rail 3, it can drive the X-axis moving member 6 and the drilling member 7 to move along the first direction Y. Thus, the drill bit 701 of the drilling member 7 moves to the next position in the web plate 102 that needs to be drilled along the first direction Y to drill a hole, thereby drilling multiple holes distributed along the first direction Y in the web plate 102.

[0080] In summary, this utility model provides a drilling device for aircraft stringers, which can improve the dimensional and positional accuracy of drilling holes in the web of aircraft stringers.

[0081] The above are merely preferred embodiments of this utility model. It should be noted that, for those skilled in the art, several improvements and substitutions can be made without departing from the technical principles of this utility model, and these improvements and substitutions should also be considered within the protection scope of this utility model.

Claims

1. An aircraft stringer drilling apparatus, the aircraft stringer comprising a web and a flange, the web being perpendicular to the flange, characterised by, Comprise: Clamping assembly for clamping the web, the web extends along the first direction and both sides are arranged towards the second direction; Y-axis moving slide rail extending along the first direction, one end of the Y-axis moving slide rail is connected with the clamping assembly, and a Y-axis moving piece capable of moving along the first direction is installed on the Y-axis moving slide rail; X-axis moving slide rail extending along the second direction, one end of the X-axis moving slide rail is connected with the Y-axis moving piece, an X-axis moving piece capable of moving along the second direction is installed on the X-axis moving slide rail, a drilling piece is installed on the X-axis moving piece, a drill bit of the drilling piece extends along the second direction, and the drill bit is used for drilling the web; Wherein, the first direction and the second direction are perpendicular to each other.

2. The aircraft stringer drilling apparatus of claim 1, wherein, A Z-axis moving slide rail extending along a third direction is installed on the X-axis moving piece, and the aircraft longeron drilling device further comprises: A Z-axis moving piece installed on the Z-axis moving slide rail and capable of moving along the third direction, and the drilling piece is installed on the Z-axis moving piece; Wherein, the first direction, the second direction and the third direction are perpendicular to each other.

3. The aircraft stringer drilling apparatus of claim 2, wherein, Further comprising: A Z-axis driving piece for driving the Z-axis moving piece to move along the third direction, the Z-axis driving piece comprises a Z-axis lead screw and a Z-axis holding part, the Z-axis lead screw extends along the third direction and passes through the X-axis moving piece and the Z-axis moving piece, and the Z-axis holding part is installed at one end of the Z-axis lead screw.

4. The aircraft stringer drilling apparatus of claim 3, wherein, The Z-axis moving piece comprises an adjusting part and a mounting part, the adjusting part is arranged at one side of the X-axis moving piece in the third direction, the Z-axis lead screw passes through the X-axis moving piece and the adjusting part, the mounting part is connected at one side of the adjusting part in the first direction, the X-axis moving piece is installed with the Z-axis moving slide rail at the side close to the mounting part, the mounting part is installed on the Z-axis moving slide rail, and the drilling piece is installed on the mounting part; The mounting part is provided with a mounting hole penetrating along the third direction, the drilling piece is a right-angle drill, a handle of the right-angle drill is inserted into the mounting hole, and a drill bit of the right-angle drill extends along the second direction.

5. The aircraft stringer drilling apparatus of claim 4, wherein, The mounting part is provided with two, the two mounting parts are respectively connected at both sides of the adjusting part in the first direction, the X-axis moving piece is installed with the Z-axis moving slide rail at both sides close to the two mounting parts, and the mounting part is installed on the corresponding Z-axis moving slide rail.

6. The aircraft stringer drilling apparatus of claim 1, wherein, Further comprising: A Y-axis driving piece for driving the Y-axis moving piece to move along the first direction, the Y-axis driving piece comprises a Y-axis lead screw and a Y-axis holding part, the Y-axis lead screw extends along the first direction and passes through the Y-axis moving piece and the clamping assembly, and the Y-axis holding part is installed at one end of the Y-axis lead screw.

7. The aircraft stringer drilling apparatus of claim 1, wherein, Further comprising: An X-axis driving member for driving the X-axis moving member to move along a second direction, the X-axis driving member comprising an X-axis screw rod extending along the second direction and passing through the X-axis moving member and the Y-axis moving member, and an X-axis holding portion mounted at one end of the X-axis screw rod.

8. The aircraft stringer drilling apparatus of claim 1, wherein, The clamping assembly comprises a rack, two fixing blocks and two positioning bolts. The two fixing blocks are sequentially mounted on the bottom of the rack along the second direction, the positioning bolts extend along the second direction, and the two positioning bolts pass through the two fixing blocks respectively, and a clamping opening for clamping the web plate is defined between the two positioning bolts. One end of the Y-axis moving slide rail is connected to the rack.

9. The aircraft stringer drilling apparatus of claim 1, wherein, The clamping assembly is provided with two clamping assemblies, the two clamping assemblies are sequentially arranged along the first direction and parallel to each other, and the two ends of the Y-axis moving slide rail are respectively connected to the two clamping assemblies.

10. The aircraft stringer drilling apparatus of claim 9, wherein, The Y-axis moving slide rail is provided with two Y-axis moving members, the two Y-axis moving members are sequentially arranged along the second direction and parallel to each other, and the two ends of the X-axis moving slide rail are respectively connected to the two Y-axis moving members.

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