Orthotic device for aeroengine blade wax pattern

Abstract

The utility model discloses a kind of orthopaedic devices for aero-engine blade wax mould, belong to aero-engine turbine blade production equipment technical field.It includes: pedestal;Blade body correction seat one, install on pedestal, blade body correction seat one includes installation body one, lower orthopaedic block one and upper orthopaedic block one, installation body one is installed on pedestal, lower orthopaedic block one swing installation is in installation body one, upper orthopaedic block one is rotationally installed on lower orthopaedic block one, the upside of lower orthopaedic block one is equipped with upside open arc groove one, the downside of upper orthopaedic block one is equipped with arc convex one, arc groove one and arc convex one are limited to form blade body contour section orthopaedic through slot one between;Swing drive mechanism, drive lower orthopaedic block one swing in height direction so that upper orthopaedic block one has extrusion correction position one to blade body contour section after rotating.The orthopaedic device of the utility model is favorable to improve the precision and stability of aero-engine blade wax mould orthopaedics.

Description

Technical Field

[0001] This utility model relates to the technical field of aero-engine turbine blade production equipment, and in particular to a straightening device for aero-engine blade wax molds. Background Technology

[0002] Aero-engine blade wax models are a key intermediate product in the precision casting process of aero-engine blades. Due to the complex shape of aero-engine blades and the high requirements for dimensional accuracy, the blade profile, torsion angle, thickness distribution, etc. are all determined by aerodynamic design optimization. Dimensional deviations will change the flow state of airflow on the blade surface. For example, excessive blade thickness will change the blade's lift-to-drag ratio, directly affecting the compressor's compression efficiency or the turbine's work capacity. Therefore, the dimensional accuracy requirements for the manufactured aero-engine blade wax models are very high.

[0003] Furthermore, in the current process of forming aero-engine blade wax molds, molten wax is injected into a molding die and held at a certain pressure and temperature for a period of time to allow the wax to cool and solidify, forming the aero-engine blade wax mold. Due to factors such as wax characteristics and mold performance, the dimensions of the formed aero-engine blade wax mold are prone to deviation. To inspect the quality of the formed aero-engine blade wax mold, existing technologies use high-precision measuring equipment such as coordinate measuring machines to measure the shape and size of the aero-engine blade wax mold. If the error of the solidified aero-engine blade wax mold exceeds the allowable error range, it is necessary to correct the formed aero-engine blade wax mold using a wax mold straightening mold. However, when using the existing wax mold straightening method to straighten the formed aero-engine blade wax mold, due to the deficiencies in the structural design of the wax mold straightening mold, the adjustment precision of the extrusion block used to extrude the aero-engine blade wax mold by the straightening operator is unstable, resulting in unstable straightening precision of the aero-engine blade wax mold and affecting the quality of the aero-engine blade wax mold obtained after straightening. Therefore, there is an urgent need for a straightening device that can improve the accuracy and stability of straightening wax models of aero-engine blades. Summary of the Invention

[0004] The purpose of this invention is to overcome at least one deficiency of the prior art and to provide a correction device for aero-engine blade wax models that is beneficial to improving the accuracy and stability of the correction of aero-engine blade wax models.

[0005] The technical solution of this utility model to solve the above-mentioned technical problems is as follows: A straightening device for aero-engine blade wax molds according to this application includes: Base; A blade straightening seat is mounted on the base. The blade straightening seat includes a mounting body, a lower straightening block, and an upper straightening block. The mounting body is mounted on the base. The lower straightening block is oscillatingly mounted on the mounting body and can oscillate relative to the mounting body in the height direction. The upper side of the lower straightening block has an arc-shaped groove with an open upper side. The upper straightening block is rotatably mounted on the lower straightening block and can rotate in the height direction. The lower side of the upper straightening block has an arc-shaped protrusion. The upper straightening block's ability to rotate relative to the lower straightening block in the height direction allows it to compress the wax model blade. The correction includes a compression correction position one and a deviation position one relative to the blade profile of the wax model; the aircraft engine blade wax model is placed between the arc-shaped groove one and the arc-shaped protrusion one; when the upper correction block one is placed at the compression correction position one, the blade profile segment correction channel one is defined between the arc-shaped groove one and the arc-shaped protrusion one, and the inner wall of the blade profile segment correction channel one compresses and corrects the profile of the blade profile segment one directly opposite it; when the upper correction block one is located at the deviation position one, the inner wall of the blade profile segment correction channel one releases the compression on the profile of the blade profile segment one directly opposite it. A swing drive mechanism is installed between the lower orthotic block and the mounting body. The lower orthotic block can swing relative to the mounting body in the height direction under the drive of the swing drive mechanism. The upper orthotic block can swing in the height direction as the lower orthotic block swings. The upper orthotic block can rotate in the height direction relative to the swinging lower orthotic block to have the compression correction position and the deviation position.

[0006] The beneficial effects of this utility model are as follows: In this embodiment, the aero-engine blade wax model to be corrected is placed between the arc-shaped groove on the lower corrector block and the arc-shaped protrusion on the upper corrector block using the lower corrector block and the upper corrector block respectively. Furthermore, the lower corrector block is oscillatingly mounted on the mounting body and can oscillate relative to the mounting body in the height direction, while the upper corrector block is rotatably mounted on the lower corrector block and can rotate in the height direction. During the correction of the aero-engine blade wax model, it is beneficial to adjust the oscillation position of the lower corrector block relative to the mounting body and the rotation position of the upper corrector block relative to the lower corrector block according to the structural contour of the aero-engine blade wax model to be corrected, so that the space defined between the arc-shaped groove and the arc-shaped protrusion can be more... A good match is made to the wax model of the aero-engine blade to be corrected, avoiding the adverse deformation of the wax model when it is placed in the space defined between the arc groove and the arc protrusion. Furthermore, the lower straightening block is driven to rotate by the swing drive mechanism, so that the upper straightening block is placed in the compression straightening position. This helps to match the contour of the blade profile segment straightening groove formed between the arc groove and the arc protrusion with the contour that the blade profile segment needs to be formed. This allows the inner wall of the blade profile segment straightening groove to compress and straighten the contour of the blade profile segment that is directly opposite it, improving the accuracy and stability of the aero-engine blade wax model straightening, and thus improving the quality of the aero-engine blade wax model obtained after straightening.

[0007] In addition, based on the above technical solution, the present invention can be further improved as follows, and can also have the following additional technical features.

[0008] According to one embodiment of this application, the first end of the mounting body in the left-right direction is provided with a support block, and the first end of the lower orthopedic block is provided with a push protrusion in the height direction directly opposite the support block, and the push protrusion is located above the support block. The support block and the push protrusion have a spacing to form an adjustable pad embedding groove. The swing drive mechanism includes: An adjusting pad is detachably embedded in the pad embedding groove. During the process of embedding the adjusting pad into the pad embedding groove, the lower side of the adjusting pad abuts against the upper side of the support block, and the upper side of the adjusting pad pushes against the lower side of the pushing protrusion, causing the lower orthopedic block to swing relative to the mounting body in the height direction, and the upper orthopedic block to rotate relative to the swinging lower orthopedic block in the height direction. When the adjusting pad is fully embedded in the pad embedding groove, the upper orthopedic block is positioned at the compression correction position one. When the adjusting pad is removed from the pad embedding groove, the upper orthopedic block can rotate relative to the lower orthopedic block in the height direction to the deviation position one.

[0009] In this embodiment, by embedding the adjusting pad in the pad embedding groove, the lower straightening block 1 swings relative to the mounting body 1 in the height direction under the action of the adjusting pad. When the adjusting pad is fully embedded in the pad embedding groove, the upper straightening block 1 is placed in the compression and correction position 1. At this time, the inner sidewall of the blade profile section straightening through groove 1 compresses and corrects the profile of the blade profile section 1 that is directly opposite it, which helps to make the blade profile section 1 obtain a profile that meets the requirements of the design drawings.

[0010] According to one embodiment of this application, the adjusting pads are provided in multiple groups, and each group of adjusting pads includes multiple adjusting pads. The multiple adjusting pads in the same group of adjusting pads have the same thickness, while the multiple adjusting pads in different groups of adjusting pads have different thicknesses.

[0011] In this embodiment, multiple sets of adjusting pads are provided. The thickness of the multiple adjusting pads in different sets of adjusting pads is not equal. The angle at which the straightening block 1 swings relative to the mounting body 1 in the height direction is different when the adjusting pads of different thicknesses are adjusted. This is beneficial to the fact that the straightening device for the aero-engine blade wax model can select adjusting pads of different thicknesses for straightening according to the contour deformation characteristics of the blade profile segment 1, thereby improving the accuracy and stability of straightening the aero-engine blade wax model.

[0012] According to one embodiment of this application, the straightening device for aero-engine blade wax molds further includes: A shelf is mounted on the base, and the shelf is provided with a resting part for holding a plurality of the adjusting pads.

[0013] In this embodiment, a shelf is provided on the base, and the adjustment pad is placed on the shelf, which makes it easy to organize and store the adjustment pad.

[0014] According to one embodiment of this application, the lower side of the adjusting pad forms a lower stop support surface, and the upper side of the adjusting pad is provided with a stepped structure to form an upper stop support surface one and an upper stop support surface two. The thickness between the upper stop support surface one and the lower stop support surface is a first thickness, and the thickness between the upper stop support surface two and the lower stop support surface is a second thickness. The first thickness is greater than the second thickness.

[0015] In this embodiment, by adjusting the first and second thicknesses of the pad, it is beneficial to allow the lower straightening block to swing at different angles relative to the mounting body in the height direction using the same adjusting pad, thereby improving the accuracy of straightening the wax model of the aero-engine blade.

[0016] According to one embodiment of this application, the upper stop support surface one is provided with an angle mark one, and the upper stop support surface two is provided with an angle mark two; wherein, the angle mark one marks the angle at which the adjusting pad can push the lower orthopedic block one to swing relative to the mounting body one in the height direction when the first thickness is fully embedded in the pad insertion groove, and the angle mark two marks the angle at which the adjusting pad can push the lower orthopedic block one to swing relative to the mounting body one in the height direction when the second thickness is fully embedded in the pad insertion groove.

[0017] In this embodiment, by providing angle mark one on the upper stop support surface one and angle mark two on the upper stop support surface two, angle mark one and angle mark two indicate the angle at which the lower orthopedic block one can swing relative to the mounting body one in the height direction, which is more conducive to selecting the corresponding angle mark one or angle mark two according to the angle at which the lower orthopedic block one swings relative to the mounting body one in the height direction.

[0018] According to one embodiment of this application, the mounting body 1 is provided with an arc-shaped mounting groove 1 with an upper open side in the front-rear direction, and the lower straightening block 1 is provided with an arc-shaped mounting protrusion 1 on its lower side. The arc-shaped mounting protrusion 1 is housed in the arc-shaped mounting groove 1 and can swing within the arc-shaped mounting groove 1. The mounting body one is also provided with an arc-shaped limiting protrusion one in the front-rear direction. The arc-shaped limiting protrusion one extends into the arc-shaped mounting groove one. The arc-shaped mounting protrusion one is provided with an arc-shaped limiting groove one directly opposite the arc-shaped limiting protrusion one. The arc-shaped limiting protrusion one extends into the arc-shaped limiting groove one. The arc-shaped limiting protrusion one can limit the angle of swing of the lower orthopedic block one relative to the mounting body one in the height direction.

[0019] In this embodiment, by housing the arc-shaped mounting protrusion 1 in the arc-shaped mounting groove 1, it is easier for the lower straightening block 1 to swing on the mounting body 1; by extending the arc-shaped limiting protrusion 1 into the arc-shaped mounting groove 1, it is beneficial to limit the swing angle of the lower straightening block 1 on the mounting body 1, thereby helping to avoid damage to the aero-engine blade wax model located in the straightening through groove 1 of the blade profile section by excessive swing angle during the swing process.

[0020] According to one embodiment of this application, the straightening device for aero-engine blade wax molds further includes: An auxiliary drive mechanism is installed between the mounting body and the lower orthopedic block, and the lower orthopedic block can swing in the height direction under the drive of the auxiliary drive mechanism, and the upper orthopedic block can swing in the height direction as the lower orthopedic block swings. The upper orthopedic block can rotate in the height direction relative to the swinging lower orthopedic block to have a suitable compression correction position and a deviation position.

[0021] In this embodiment, the lower orthopedic block is driven to swing in the height direction by an auxiliary drive mechanism. This facilitates the adjustment of the spacing between the support block and the push protrusion by adjusting the thickness of the adjustable pad in the pad embedding groove as needed. This makes it easier to embed the adjustable pad with a suitable thickness into the pad embedding groove, and also makes it easier for the lower side of the adjustable pad to abut against the upper side of the support block, and for the upper side of the adjustable pad to push against the lower side of the push protrusion, thereby improving the accuracy of placing the upper orthopedic block in the compression correction position.

[0022] According to one embodiment of this application, the mounting body is provided with a movable clearance groove, which extends horizontally in the left-right direction. A threaded through hole communicating with the movable clearance groove is provided at the second end of the mounting body. The mounting body is also provided with a vertical clearance opening, which is located above and communicates with the movable clearance groove. The auxiliary drive mechanism includes: A drive slider is slidably installed in the movable clearance groove, and a limiting slot is provided on the upper side of the drive slider facing the vertical clearance opening; The drive rod is connected to the lower side of the arc-shaped mounting protrusion, facing the limiting slot, and the lower end of the drive rod extends into the limiting slot. A drive screw is threadedly connected to the threaded through hole. One end of the drive screw is connected to the drive slider, and the other end of the drive screw is provided with an adjusting grip. The adjusting grip is located on the outside of the mounting body. The drive slider can slide in the movable clearance groove under the pushing action of the drive screw, so that the drive rod extending into the limiting slot drives the lower orthopedic block to swing in the height direction. When the drive slider slides in the movable clearance groove, the drive rod can move left and right in the vertical clearance through hole.

[0023] In this embodiment, the mounting body is provided with a movable clearance groove and a threaded through hole and a vertical clearance opening that communicate with the movable clearance groove. The driving slider in the movable clearance groove slides in the movable clearance groove under the action of the driving screw that is threadedly connected to the threaded through hole, which is beneficial to drive the driving rod located on the limiting slot to move left and right in the vertical clearance opening. The driving rod located below the arc-shaped mounting protrusion extends into the limiting slot on the driving slider, which is beneficial to drive the arc-shaped mounting protrusion to swing in the arc-shaped mounting groove when the driving slider slides in the movable clearance groove, which is beneficial to limit the angle of swing of the lower orthopedic block on the mounting body.

[0024] According to one embodiment of this application, the straightening device for aero-engine blade wax molds further includes: A height adjustment mechanism is installed between the base and the mounting body, and the mounting body can adjust its height in the vertical direction under the adjustment of the height adjustment mechanism.

[0025] In this embodiment, by setting a height adjustment mechanism between the base and the mounting body, it is beneficial to adjust the height position of the mounting body in the vertical direction, which in turn is beneficial to adjust the height position of the lower orthopedic block in the vertical direction.

[0026] According to one embodiment of this application, the lower side of the mounting body is provided with a stop slope, the stop slope being inclined from left to right from low to high, and the upper side of the base facing the mounting body is provided with a body mounting part, the body mounting part extending in the left-right direction, and the height adjustment mechanism including: A height adjustment slider is slidably mounted on the main body mounting part and can slide in the left and right directions. The upper side of the height adjustment slider is provided with a second stop slope that stops against the first stop slope. The second stop slope is inclined from left to right from low to high. A push rod is provided, one end of which is mounted on one end of the height adjustment slider. The height adjustment slider can slide between the base and the mounting body in the left-right direction under the pushing action of the push rod, thereby adjusting the height position of the mounting body in the vertical direction.

[0027] In this embodiment, by setting a stop slope one on the lower side of the mounting body one, and the stop slope one being stopped by the stop slope two set on the upper side of the height adjustment slider, it is beneficial to adjust the height position of the mounting body one in the vertical direction when the height adjustment slider slides in the left and right direction under the pushing action of the push rod, thereby adjusting the height position of the blade profile section straightening groove one in the vertical direction. This is beneficial to improving the accuracy and stability of the straightening of the aero-engine blade wax model, and thus improving the quality of the aero-engine blade wax model obtained after straightening.

[0028] According to one embodiment of this application, the straightening device for aero-engine blade wax molds further includes: A height adjustment reference scale is provided on the upper side of the base. The height adjustment reference scale is used to reference the distance that the height adjustment slider slides between the base and the mounting body in the left and right direction. The reference baseline is set on the height adjustment slider, directly opposite the height adjustment reference scale.

[0029] In this embodiment, by setting a height adjustment reference scale and a reference baseline, it is beneficial to accurately adjust the distance the height adjustment slider slides in the left and right directions, which in turn is beneficial to accurately adjust the height position of the mounting body and the lower straightening block on it in the vertical direction, thereby improving the accuracy and stability of straightening the wax model of the aero-engine blade. Attached Figure Description

[0030] To more clearly illustrate the technical solutions in this utility model, the drawings used in the description of the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this application. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0031] Figure 1 This is a schematic diagram of the structure of the straightening device for aero-engine blade wax mold according to an embodiment of the present invention; Figure 2 This is a schematic diagram of the structure of the leaf correction seat in this embodiment of the present utility model; Figure 3 for Figure 2 Disassembly and assembly diagrams of some components; Figure 4 This is a schematic diagram of the base structure in an embodiment of the present utility model; Figure 5 for Figure 2 Straighten the top view; Figure 6 This is a schematic diagram of the tenon straightening seat structure in an embodiment of this utility model; Figure 7 This is a schematic diagram of the structure of one of the adjusting pads in an embodiment of the present utility model. Detailed Implementation

[0032] To make the objectives, technical solutions, and advantages of this application clearer, the embodiments of this application will be described in further detail below with reference to the accompanying drawings.

[0033] To better understand the above-mentioned objectives, features, and advantages of this utility model, the present utility model will be further described in detail below with reference to the accompanying drawings and specific embodiments. It should be noted that, unless otherwise specified, the embodiments and features described in these embodiments can be combined with each other.

[0034] Many specific details are set forth in the following description in order to provide a full understanding of the present invention. However, the present invention may also be implemented in other ways different from those described herein. Therefore, the scope of protection of the present invention is not limited to the specific embodiments disclosed below.

[0035] This application provides a shaping device for wax models of aero-engine blades, such as... Figures 1 to 3 As shown, it includes: Base 1; A blade straightening seat 3 is mounted on a base 1. The blade straightening seat 3 includes a mounting body 31, a lower straightening block 32, and an upper straightening block 33. The mounting body 31 is mounted on the base 1. The lower straightening block 32 is oscillatingly mounted on the mounting body 31 and can oscillate relative to the mounting body 31 in the height direction. The upper side of the lower straightening block 32 has an arc-shaped groove 321 with an open upper side. The upper straightening block 33 is rotatably mounted on the lower straightening block 32 and can rotate in the height direction. The lower side of the upper straightening block 33 has an arc-shaped protrusion 331. The upper straightening block 33 can rotate relative to the lower straightening block 32 in the height direction and has a function of supporting the wax model. The blade is subjected to compression correction at position one and deviation position one relative to the wax model blade. The aero-engine blade wax model 8 is placed between the arc-shaped groove 321 and the arc-shaped protrusion 331. When the upper correction block 33 is placed at position one, the blade profile section correction channel 34 is defined between the arc-shaped groove 321 and the arc-shaped protrusion 331. The inner wall of the blade profile section correction channel 34 compresses and corrects the profile of the blade profile section one that is directly opposite it. When the upper correction block 33 is located at position one, the inner wall of the blade profile section correction channel 34 releases the compression of the profile of the blade profile section one that is directly opposite it. A swing drive mechanism is installed between the lower orthotic block 32 and the mounting body 31. The lower orthotic block 32 can swing relative to the mounting body 31 in the height direction under the drive of the swing drive mechanism. The upper orthotic block 33 can swing in the height direction along with the swing of the lower orthotic block 32. The upper orthotic block 33 can rotate in the height direction relative to the swinging lower orthotic block 32 and has a compression correction position and a deviation position.

[0036] In this embodiment, as Figures 1 to 3 As shown, in this embodiment, the aero-engine blade wax model 8 to be corrected is placed between the arc-shaped groove 321 on the lower correcting block 32 and the arc-shaped protrusion 331 on the upper correcting block 33, provided on the blade correction seat 3. Furthermore, the lower correcting block 32 is oscillatingly mounted on the mounting body 31 and can oscillate relative to the mounting body 31 in the height direction, while the upper correcting block 33 is rotatably mounted on the lower correcting block 32 and can rotate in the height direction. During the correction of the aero-engine blade wax model 8, it is beneficial to adjust the oscillation position of the lower correcting block 32 relative to the mounting body 31 and the rotation position of the upper correcting block 33 relative to the lower correcting block 32 according to the structural contour of the aero-engine blade wax model 8 to be corrected, so that the space defined between the arc-shaped groove 321 and the arc-shaped protrusion 331 is... The space can better match the wax model 8 of the aero-engine blade to be corrected, avoiding the adverse deformation of the wax model 8 when it is placed in the space defined between the arc groove 321 and the arc protrusion 331. Furthermore, by driving the lower straightening block 32 to rotate through the swing drive mechanism, the upper straightening block 33 is driven to the compression straightening position. This helps to match the contour of the blade profile section straightening channel 34 defined between the arc groove 321 and the arc protrusion 331 with the contour that the blade profile section needs to be formed. This allows the inner wall of the blade profile section straightening channel 34 to compress and straighten the contour of the blade profile section that is directly opposite it, improving the accuracy and stability of the straightening of the aero-engine blade wax model 8 and improving the quality of the aero-engine blade wax model 8 obtained after straightening.

[0037] Furthermore, such as Figure 1 , Figure 2 and Figure 5As shown, in this embodiment, a coordinate measuring reference column 19 is installed on one side of the blade profile section straightening groove 34, and the coordinate measuring reference column 19 is located in the middle of the upper side of the base 1. The lower side of the base 1 is provided with multiple vertical support beams 11 to support the base 1. One end of the upper straightening block 33 is rotatably installed on one end of the lower straightening block 32, and the other end of the upper straightening block 33 is connected to the lower straightening block 32 through a latch 35. It should be noted that the structure of the latch 35 and other latches in this embodiment can refer to the existing latches in the art, and the selection of latches can also be selected according to the requirements, which will not be elaborated here.

[0038] Furthermore, such as Figure 1 and Figure 6 As shown, a tenon straightening seat 2 is also provided on the base 1, installed on the base 1 and located on the horizontal side of the blade straightening seat 3. The tenon straightening seat 2 includes a tenon mounting body 21, a lower tenon straightening block 22, and an upper tenon straightening block 23. The tenon mounting body 21 is installed on the base 1. The lower tenon straightening block 22 is oscillatingly installed on the tenon mounting body 21 and can oscillate relative to the tenon mounting body 21 in the height direction. The upper side of the lower tenon straightening block 22 is provided with an upper open tenon arc-shaped groove. One end of the tenon upper straightening block 23 is rotatably mounted on the lower tenon straightening block 22 and can rotate in the height direction. The other end of the tenon upper straightening block 23 is connected to the lower tenon straightening block 22 through the tenon straightening lock 25. The lower side of the tenon upper straightening block 23 is provided with a tenon arc-shaped groove. The tenon upper straightening block 23 can rotate relative to the lower tenon straightening block 22 in the height direction and has a tenon straightening position for positioning and straightening the wax model tenon and a tenon deviation position relative to the wax model tenon; to launch the aircraft engine The tenon of the blade wax mold 8 is placed between the first and second arc-shaped grooves of the tenon. When the straightening block 23 on the tenon is in the tenon positioning and correction position, the tenon contour section straightening groove 24 formed between the first and second arc-shaped grooves of the tenon defines the tenon contour section straightening groove 24. The inner wall of the tenon contour section straightening groove 24 positions and corrects the tenon directly opposite it. When the straightening block 23 on the tenon is in a deviated position, the inner wall of the tenon contour section straightening groove 24 releases its position on the tenon directly opposite it. The compression is fixed; furthermore, the swing drive mechanism is installed between the tenon lower straightening block 22 and the tenon mounting body 21, and the tenon lower straightening block 22 can swing relative to the tenon mounting body 21 in the height direction under the drive of the swing drive mechanism, and the tenon upper straightening block 23 can swing in the height direction with the swing of the tenon lower straightening block 22, and the tenon upper straightening block 23 can rotate in the height direction relative to the swinging tenon lower straightening block 22 to have a tenon correction position and a tenon deviation position.

[0039] In this embodiment, as Figure 1 and Figure 6As shown, in this embodiment, the blade tenon is placed between the tenon arc-shaped groove one and the tenon arc-shaped groove two on the tenon straightening seat 2. The swing drive mechanism drives the tenon lower straightening block 22 to swing relative to the tenon mounting body 21 in the height direction, so that the tenon upper straightening block 23 can swing in the height direction with the swing of the tenon lower straightening block 22. The tenon upper straightening block 23 can rotate in the height direction relative to the swinging tenon lower straightening block 22 to have a tenon straightening position and a tenon deviation position; thus, it is beneficial to form a torsion angle and a blade profile that meet the design requirements between the tenon and the blade body.

[0040] It should be noted that, as Figures 1 to 7 As shown, the connection method between the tenon mounting body 21 and the tenon lower straightening block 22 in this embodiment is the same as or similar to the connection method between the mounting body 31 and the lower straightening block 32. The connection method between the tenon mounting body 21 and the base 1 in this embodiment is the same as or similar to the connection method between the mounting body 31 and the base 1, and will not be described again here.

[0041] Furthermore, such as Figure 1 , Figure 4 and Figure 5 As shown, the base 1 is also provided with a crown correction mounting groove 183, which is located on the horizontal side of the blade correction seat 3 away from the tenon correction seat 2. The base 1 is also provided with a crown correction seat 4, which is installed in the crown correction mounting groove 183. The crown correction seat 4 includes an upper crown mounting block and a lower crown mounting block. The lower crown mounting block is fixedly installed on the base 1, and a crown mounting groove adapted to the shape and size of the crown is formed on the upper side of the lower crown mounting block. One end of the upper crown mounting block is rotatably installed on the lower crown mounting block and can rotate in the height direction. The other end of the upper crown mounting block is connected to the lower crown mounting block through a crown lock. A crown positioning block is also provided on the lower side of the upper crown mounting block. A crown screw is provided on the upper crown mounting block opposite the crown positioning block. The crown positioning block has a crown screw that mates with the crown threaded hole. The crown screw can be used to adjust the vertical height of the crown positioning block. After the crown is placed into the crown mounting groove, the upper mounting block of the crown is fixed to the lower mounting block of the crown by the crown locking buckle. By adjusting the vertical height of the crown positioning block, the crown is fixed in the crown mounting groove. This helps to pre-fix the crown, thus preventing the crown from rotating when the blade profile is rotated to a suitable angle by the blade straightening seat 3, which would cause errors. It should be noted that the specific structure of the crown straightening seat 4 is not illustrated and described in detail in this embodiment. The specific structure and installation method of the crown straightening seat 4 can also refer to the existing technology in this field, and will not be repeated here.

[0042] Furthermore, such as Figures 1 to 7As shown, the straightening device for the wax model of the aero-engine blade in this embodiment also includes one or more of the following: blade straightening seat 2 5, blade straightening seat 3 6, and blade straightening seat 4 7. The structures of blade straightening seat 2 5, blade straightening seat 3 6, and blade straightening seat 4 7 are similar to those of blade straightening seat 1 3, and will not be described in detail here. It should be noted that blade straightening seat 1 3, blade straightening seat 2 5, blade straightening seat 3 6, and blade straightening seat 4 7 are located at different positions along the blade length and are used to straighten blade profile segments corresponding to different positions. Blade profile segment 1 is one of multiple blade profile segments. The cross-section of the aero-engine turbine blade is as follows: The irregular "banana shape" of the aero-engine blade wax model results in different shapes for the blade profile segments at different positions along the blade length. Therefore, the profiles of the blade profile segment straightening grooves formed on the blade straightening seats 1-3, 2-5, 3-6, and 4-7 for straightening different blade profile segments are all different. This facilitates the straightening of blade profile segments located at different positions along the blade length and improves the accuracy of the straightening process. Furthermore, after the straightening of the blade profile segments is completed, the blade profile of the aero-engine blade wax model conforms to the design requirements of the drawings.

[0043] It should be noted that for the correction of a wax model for an aero-engine blade, one or more correction devices can be used to correct the blade profile segments that need correction at different positions along the blade length. Moreover, when using multiple correction devices, the different correction devices can complement each other so that multiple correction devices can cover all blade profile segments at different positions along the blade length. In addition, when a wax model for an aero-engine blade only needs to correct one blade profile segment, for example, only blade profile segment one needs to be corrected, a blade correction seat 3 provided on the correction device for the aero-engine blade wax model can also be used to correct the wax model for the aero-engine blade.

[0044] One embodiment of this application, such as Figure 3 and Figure 7 As shown, the first end of the mounting body 31 in the left-right direction is provided with a support block 310, and the first end of the lower straightening block 32 is provided with a push protrusion 320 in the height direction directly opposite the support block 310. The push protrusion 320 is located above the support block 310, and there is a gap between the support block 310 and the push protrusion 320 to form a spacer insertion groove with adjustable spacing. The swing drive mechanism includes: Adjusting pad 9 is detachably embedded in the pad embedding groove. During the process of inserting adjusting pad 9 into the pad embedding groove, the lower side of adjusting pad 9 abuts against the upper side of support block 310, and the upper side of adjusting pad 9 pushes against the lower side of push protrusion 320, causing lower straightening block 32 to swing relative to mounting body 31 in the height direction, and upper straightening block 33 to rotate relative to the swinging lower straightening block 32 in the height direction. When adjusting pad 9 is fully embedded in the pad embedding groove, upper straightening block 33 is placed in compression correction position 1. When adjusting pad 9 is removed from the pad embedding groove, upper straightening block 33 can rotate relative to lower straightening block 32 in the height direction to deviation position 1.

[0045] In this embodiment, as Figure 3 and Figure 7 As shown, in this embodiment, by embedding the adjusting pad 9 into the pad slot between the support block 310 and the push protrusion 320, the lower straightening block 32 swings relative to the mounting body 31 in the height direction under the action of the adjusting pad 9. When the adjusting pad 9 is fully embedded in the pad slot, it is beneficial to place the upper straightening block 33 in the compression and correction position 1, which in turn is beneficial to the inner sidewall of the blade profile section straightening through groove 34 to compress and correct the profile of the blade profile section 1 that is directly opposite it, so as to achieve the correction of the profile of the blade profile section 1 so that the profile of the blade profile section 1 meets the shape required by the design drawings.

[0046] Furthermore, such as Figure 3 , Figure 6 and Figure 7As shown, the installation method of the swing drive mechanism between the tenon lower straightening block 22 and the tenon mounting body 21 in this embodiment is the same as or similar to the installation method of the swing drive mechanism between the lower straightening block 32 and the mounting body 31. The first end of the tenon mounting body 21 in the left-right direction is provided with a tenon support block 210. The first end of the tenon lower straightening block 22 is provided with a tenon pushing protrusion 220 in the height direction, which is directly opposite to the tenon support block 210. The tenon pushing protrusion 220 is located above the tenon support block 210. There is a gap between the tenon support block 210 and the tenon pushing protrusion 220 to form an adjustable pad embedding groove. The adjustable pad 9 is detachably embedded in the pad embedding groove. During the process of inserting the adjusting pad 9 into the groove, the lower side of the adjusting pad 9 abuts against the upper side of the tenon support block 210, and the upper side of the adjusting pad 9 pushes against the lower side of the tenon push-up protrusion 220, causing the tenon lower straightening block 22 to swing relative to the tenon mounting body 21 in the height direction, and the tenon upper straightening block 23 to rotate relative to the swinging tenon lower straightening block 22 in the height direction. When the adjusting pad 9 is fully inserted into the groove, the tenon upper straightening block 23 is placed in the tenon correction position. When the adjusting pad 9 is removed from the groove, the tenon upper straightening block 23 can rotate relative to the tenon lower straightening block 22 in the height direction to the tenon deviation position.

[0047] One embodiment of this application, such as Figure 4 , Figure 5 and Figure 7 As shown, there are multiple sets of adjusting pads 9, and each set of adjusting pads includes multiple adjusting pads 9. The thickness of the multiple adjusting pads 9 in the same set is equal, while the thickness of the multiple adjusting pads 9 in different sets is not equal.

[0048] In this embodiment, as Figure 2 , Figure 4 , Figure 5 and Figure 7 As shown, in this embodiment, multiple sets of adjusting pads 9 are provided. The thickness of the multiple adjusting pads 9 in different sets of adjusting pads 9 is not equal. The adjusting pads 9 with different thicknesses adjust the straightening block 32 to swing at different angles relative to the mounting body 31 in the height direction. This is beneficial to enable the straightening device for the aero-engine blade wax model to select adjusting pads 9 of different thicknesses for straightening according to the contour deformation characteristics of the blade profile segment 1, thereby improving the accuracy and stability of straightening the aero-engine blade wax model 8.

[0049] Furthermore, such as Figures 1 to 7 As shown, before the wax model blade is corrected, the contour of the wax model blade body of the aero-engine blade wax model 8 to be corrected is detected by the contour detection device to obtain the contour feature parameters of multiple blade body contour segments of the wax model blade body. The contour feature parameters of the multiple blade profile segments are compared one-to-one with multiple standard contour feature parameters to obtain the contour deviation of the multiple blade profile segments. The standard contour feature parameters are the contour feature parameters of multiple blade profile segments of the wax model blade of the standard aero-engine blade wax model 8. The multiple standard contour feature parameters are obtained by pre-detection. Based on the multiple contour deviations, the contour correction amounts of the multiple blade profile segments are obtained, thereby determining the size of the first preset angle that the swing drive mechanism needs to drive the lower correction block 32 to rotate. An adjustment pad 9 of appropriate thickness is selected based on the first preset angle, which helps to ensure that the lower correction block 32 swings at a suitable angle relative to the mounting body 31 in the height direction. This, in turn, helps to define a suitable blade profile segment correction through groove 34 between the arc-shaped groove 321 and the arc-shaped protrusion 331. After correction according to the contour correction amounts, the multiple... The contour feature parameters of the blade profile segment are within the allowable error range of the standard contour feature parameters that correspond to them one-to-one. For the contour correction amount of the blade profile segment one, when the swing drive mechanism drives the lower correction block one 32 to rotate the first preset angle, the inner sidewall of the blade profile segment correction through groove one 34 squeezes the contour of the blade profile segment one that is directly opposite it, so that the deformation of the contour of the blade profile segment one is equal to the contour correction amount. The blade profile segment one is one of a plurality of blade profile segments.

[0050] In this embodiment, as Figure 1 and Figure 7 As shown, in this embodiment, a contour detection device is used to detect the contour of the wax model blade of the aero-engine blade wax model 8 to be corrected. The contour feature parameters of multiple detected blade contour segments are compared one-to-one with multiple standard contour feature parameters to obtain the contour deviation of multiple blade contour segments. This is beneficial for identifying the blade contour segments that need to be corrected based on the multiple contour deviations, and for obtaining the contour correction amount of the blade contour segments that currently need to be corrected. This is further beneficial for obtaining the first preset angle size of the swing drive mechanism to drive the lower correction block 32 to swing based on the contour correction amount of the blade contour segments that currently need to be corrected. When the swing drive mechanism drives the lower correction block 32 to swing the first preset angle, the inner wall of the blade contour segment correction groove 34 squeezes the contour of the blade contour segment 1 that is directly opposite it. This is beneficial for making the deformation of the blade contour segment 1 after being squeezed by the inner wall of the blade contour segment correction groove 34 equal to the contour correction amount.

[0051] One embodiment of this application, such as Figure 4 and Figure 5 As shown, the straightening device for aero-engine blade wax models also includes: The shelf 14 is mounted on the base 1 and has a shelf portion for holding multiple adjusting pads 9.

[0052] In this embodiment, as Figure 4 and Figure 5 As shown, in this embodiment, a shelf 14 is provided on the base 1, and the adjustment pad 9 is placed on the shelf 14, which makes it easy to organize and store the adjustment pad 9.

[0053] Furthermore, such as Figure 1 , Figure 4 and Figure 5 As shown, the shelf 14 is provided with a shelf cover plate 13, which is fixed to the base 1 by cover plate fixing screws 15.

[0054] One embodiment of this application, such as Figure 7 As shown, the lower side of the adjusting pad 9 forms a lower stop support surface, and the upper side of the adjusting pad 9 is provided with a stepped structure to form an upper stop support surface 91 and an upper stop support surface 92. The thickness between the upper stop support surface 91 and the lower stop support surface is the first thickness, and the thickness between the upper stop support surface 92 and the lower stop support surface is the second thickness. The first thickness is greater than the second thickness.

[0055] In this embodiment, as Figure 3 and Figure 7 As shown, in this embodiment, by adjusting the first thickness and the second thickness of the pad 9 to be different, it is beneficial that the same adjusting pad 9 can make the lower straightening block 32 swing at different angles relative to the mounting body 31 in the height direction, thereby improving the accuracy of straightening the aero-engine blade wax model 8.

[0056] One embodiment of this application, such as Figure 3 and Figure 7 As shown, the upper stop support surface 91 is provided with an angle mark 911, and the upper stop support surface 92 is provided with an angle mark 921; wherein, the angle mark 911 marks the angle at which the adjusting pad 9 can push the lower orthopedic block 32 to swing relative to the mounting body 31 in the height direction when the first thickness is fully embedded in the groove, and the angle mark 921 marks the angle at which the adjusting pad 9 can push the lower orthopedic block 32 to swing relative to the mounting body 31 in the height direction when the second thickness is fully embedded in the groove.

[0057] In this embodiment, as Figure 3 and Figure 7As shown, in this embodiment, by providing an angle mark 911 on the upper stop support surface 91 and an angle mark 921 on the upper stop support surface 92, the angle mark 911 and the angle mark 921 indicate the angle at which the lower orthopedic block 32 can swing relative to the mounting body 31 in the height direction. This makes it easier to select the corresponding angle mark 911 or angle mark 921 according to the angle at which the lower orthopedic block 32 swings relative to the mounting body 31 in the height direction.

[0058] One embodiment of this application, such as Figure 3 As shown, the mounting body 31 has an arc-shaped mounting groove 312 with an upper opening in the front-rear direction, and the lower straightening block 32 has an arc-shaped mounting protrusion 322 on the lower side. The arc-shaped mounting protrusion 322 is housed in the arc-shaped mounting groove 312 and can swing within the arc-shaped mounting groove 312. The mounting body 31 is also provided with an arc-shaped limiting protrusion 313 in the front-rear direction. The arc-shaped limiting protrusion 313 extends into the arc-shaped mounting groove 312. The arc-shaped mounting protrusion 322 is provided with an arc-shaped limiting groove 313 opposite to the arc-shaped limiting protrusion 313. The arc-shaped limiting protrusion 313 extends into the arc-shaped limiting groove 313. The arc-shaped limiting protrusion 313 can limit the angle of swing of the lower orthopedic block 32 relative to the mounting body 31 in the height direction.

[0059] In this embodiment, as Figure 3 As shown, in this embodiment, by housing the arc-shaped mounting protrusion 322 in the arc-shaped mounting groove 312, it is easier for the lower straightening block 32 to swing on the mounting body 31; by extending the arc-shaped limiting protrusion 313 into the arc-shaped mounting groove 312, it is beneficial to limit the swing angle of the lower straightening block 32 on the mounting body 31, thereby helping to avoid damage to the aero-engine blade wax model 8 located in the straightening through groove 34 of the blade profile section by excessive swing angle of the lower straightening block 32 during the swing process.

[0060] One embodiment of this application, such as Figure 2 and Figure 3 As shown, the straightening device for aero-engine blade wax models also includes: An auxiliary drive mechanism is installed between the mounting body 31 and the lower orthotic block 32. The lower orthotic block 32 can swing in the height direction under the drive of the auxiliary drive mechanism, and the upper orthotic block 33 can swing in the height direction along with the swing of the lower orthotic block 32. The upper orthotic block 33 can rotate in the height direction relative to the swinging lower orthotic block 32 to have a suitable compression correction position and a deviation position.

[0061] In this embodiment, as Figure 2 and Figure 3As shown, in this embodiment, the lower orthopedic block 32 is driven to swing in the height direction by an auxiliary drive mechanism. This facilitates the adjustment of the thickness of the adjusting pad 9 embedded in the pad embedding groove as needed, thereby adjusting the spacing between the pad embedding groove formed between the support block 310 and the push protrusion 320. This is beneficial for embedding the adjusting pad 9 with a suitable thickness into the pad embedding groove, and also for making the lower side of the adjusting pad 9 abut against the upper side of the support block 310, so that the upper side of the adjusting pad 9 pushes against the lower side of the push protrusion 320, improving the accuracy of placing the upper orthopedic block 32 in the compression correction position.

[0062] One embodiment of this application, such as Figure 3 As shown, the mounting body 31 is provided with a movable clearance groove 315, which extends horizontally in the left-right direction. The second end of the mounting body 31 is provided with a threaded through hole 316 communicating with the movable clearance groove 315. The mounting body 31 is also provided with a vertical clearance opening 314, which is located above the movable clearance groove 315 and communicates with it. The auxiliary drive mechanism includes: The drive slider 38 is slidably installed in the movable clearance groove 315, and the upper side of the drive slider 38 is provided with a limit slot 382 facing the vertical clearance opening 314. The drive rod 383 is connected to the lower side of the arc-shaped mounting protrusion 322, facing the limiting slot 382, ​​and the lower end of the drive rod 383 extends into the limiting slot 382; The drive screw 384 is threadedly connected to the threaded through hole 316. One end of the drive screw 384 is connected to the drive slider 38, and the other end of the drive screw 384 is provided with an adjustable grip. The adjustable grip is located on the outside of the mounting body 31. The drive slider 38 can slide in the movable clearance groove 315 under the pushing action of the drive screw 384, so that the drive rod 383 extending into the limiting slot 382 drives the lower orthopedic block 32 to swing in the height direction. When the drive slider 38 slides in the movable clearance groove 315, the drive rod 383 can move left and right in the vertical clearance through opening 314.

[0063] In this embodiment, as Figure 3As shown, in this embodiment, the mounting body 31 is provided with a movable clearance groove 315 and a threaded through hole 316 and a vertical clearance opening 314 communicating with the movable clearance groove 315. The driving slider 38 in the movable clearance groove 315 slides in the movable clearance groove 315 under the action of the driving screw 384 threadedly connected to the threaded through hole 316, which is conducive to driving the driving rod 383 located on the limiting slot 382 to move left and right in the vertical clearance opening 314. The driving rod 383 located on the lower side of the arc-shaped mounting protrusion 322 extends into the limiting slot 382 on the driving slider 38, which is conducive to driving the arc-shaped mounting protrusion 322 to swing in the arc-shaped mounting groove 312 when the driving slider 38 slides in the movable clearance groove 315, which is conducive to limiting the angle of swing of the lower orthopedic block 32 on the mounting body 31.

[0064] Furthermore, such as Figure 1 As shown, a baffle 317 is provided on the side of the mounting body 31 facing away from the arc-shaped limiting groove 31 in the front-rear direction. The baffle 317 is installed on the mounting body 31 by screws to prevent impurities from falling into the movable clearance groove 315 and the arc-shaped mounting groove 312 when the straightening device used for the wax model of the aero-engine blade is working. This helps to avoid the swing of the straightening block 32 under the influence of impurities and to prevent impurities from affecting the operation of the auxiliary drive mechanism.

[0065] Furthermore, such as Figure 3 As shown, a screw mounting protrusion 3841 is provided on one end of the drive screw 384, and a screw mounting through groove 381 is provided at the drive slider 38 and the drive screw 384. The screw mounting protrusion 3841 is installed in the screw mounting through groove 381.

[0066] One embodiment of this application, such as Figures 1 to 5 As shown, the straightening device for aero-engine blade wax models also includes: A height adjustment mechanism is installed between the base 1 and the mounting body 31. The mounting body 31 can adjust its height position in the vertical direction under the adjustment of the height adjustment mechanism.

[0067] In this embodiment, as Figures 1 to 5 As shown, in this embodiment, by setting a height adjustment mechanism between the base 1 and the mounting body 31, it is beneficial to adjust the height position of the mounting body 31 in the vertical direction, which in turn is beneficial to adjust the height position of the lower orthopedic block 32 in the vertical direction.

[0068] One embodiment of this application, such as Figures 1 to 5 As shown, the lower side of the mounting body 31 is provided with a stop slope, which is inclined from left to right from low to high. The base 1 is provided with a mounting part on the upper side of the mounting body 31, which extends in the left-right direction. The height adjustment mechanism includes: The height adjustment slider 30 is slidably mounted on the main body mounting part and can slide in the left and right directions. The upper side of the height adjustment slider 30 is provided with a second stop slope that stops against the first stop slope. The second stop slope is inclined from left to right from low to high. A push rod 304 is installed at one end on one end of a height adjustment slider 30. Under the push of the push rod 304, the height adjustment slider 30 can slide between the base 1 and the mounting body 31 in the left and right directions, thereby adjusting the height of the mounting body 31 in the vertical direction.

[0069] In this embodiment, as Figures 1 to 5 As shown, in this embodiment, by setting a stop slope one on the lower side of the mounting body 31, and the stop slope one being stopped by a stop slope two set on the upper side of the height adjustment slider 30, it is beneficial to adjust the height position of the mounting body 31 in the vertical direction when the height adjustment slider 30 slides in the left and right direction under the pushing action of the push rod 304, thereby adjusting the height position of the blade profile section straightening groove 34 in the vertical direction. This is beneficial to improving the accuracy and stability of the straightening of the aero-engine blade wax model 8, and thus improving the quality of the aero-engine blade wax model 8 obtained after straightening. Furthermore, such as Figure 3 As shown, the lower side of the mounting body 31 is provided with a guide limiting groove 311, which extends out of the mounting body 31 in the left-right direction. The height adjustment mechanism also includes: Guide limit block 37 is installed on the upper side of the height adjustment slider. The upper side of guide limit block 37 is provided with guide limit groove 1, which extends through guide limit block 37 along the length direction of push rod 304. Guide rail 371 is slidably installed in guide limiting groove 1. The upper side of guide rail 371 is higher than the upper side of height adjustment slider in the height direction.

[0070] In this embodiment, as Figure 3As shown, in this embodiment, the height adjustment slider is pushed by the push rod 304 to slide along the length of the push rod 304. This facilitates the sliding of the guide limiting block 37 inside the height adjustment slider relative to the guide rail 371 along the length of the push rod 304, and further facilitates the sliding of the guide limiting groove 1 of the guide limiting block 37 relative to the guide rail 371 along the length of the push rod 304. With the guide rail 371 slidably installed in the guide limiting groove 1, when the height adjustment slider slides along the length of the push rod 304, it helps to reduce the sliding friction between the height adjustment slider and the device or mechanism installed on the upper part of the guide rail 371. The stop slope 2 is inclined from left to right from low to high, which helps to change the vertical height position of the guide rail 371 on the upper side of the stop slope 2 during the sliding process, and further facilitates the change in the vertical height position of the device or mechanism installed on the upper side of the guide rail 371.

[0071] Furthermore, such as Figure 3 As shown, the upper side of the height adjustment slider faces the guide limiting groove 1 and guide limiting groove 2 302. The guide limiting groove 2 302 extends out of the height adjustment slider along the extension direction of the guide limiting groove 1. The upper side of the height adjustment slider is also provided with the installation and storage groove 1 301. The guide limiting block 1 37 is installed in the installation and storage groove 1 301. When the guide limiting block 1 37 is installed in the installation and storage groove 1 301, the guide limiting groove 1 and the guide limiting groove 2 302 are connected. The guide rail 1 371 is provided with the guide rail mounting hole 1 3711. The upper part of the guide rail 1 371 is fixedly installed in the guide limiting groove 5 311 by connecting it with the guide rail mounting hole 1 3711 through screws. The lower part of the guide rail 1 371 is slidably installed in the guide limiting groove 1 and the guide limiting groove 2 302.

[0072] Furthermore, such as Figure 3 As shown, when the guide limit block 37 is installed in the installation and storage groove 301, limit stop blocks 372 are provided on both sides of the guide limit block 37.

[0073] In this embodiment, as Figure 3 As shown, in this embodiment, the upper side of the height adjustment slider is provided with a mounting and storage groove 301, which is beneficial for installing the guide limiting block 37 in the mounting and storage groove 301. The guide limiting groove 302 is connected to the guide limiting groove 1 and extends out of the height adjustment slider along the extension direction of the guide limiting groove 1. This is beneficial for sliding the guide rail 371 along the length direction of the push rod 304 on the guide limiting groove 1 and the guide limiting groove 302. When the height adjustment slider slides along the length direction of the push rod 304, it is beneficial to reduce the sliding friction between the height adjustment slider and the device or mechanism installed on the upper part of the guide rail 371.

[0074] Furthermore, such as Figure 3As shown, the height adjustment mechanism also includes: Guide rail 2 361 is installed on the lower side of the height adjustment slider. The extension direction of guide rail 2 361 is the same as the extension direction of guide rail 1 371; and the lower side of guide rail 2 361 is lower than the lower side of the height adjustment slider in the height direction. Guide limiting block 2 36 is used for fixed installation. Guide limiting groove 3 is provided on the upper side of guide limiting block 2 36. Guide limiting groove 3 extends out of guide limiting block 2 36 along the length direction of push rod 304. Guide rail 2 361 extends into guide limiting groove 3 and can slide along the extension direction of guide limiting groove 3 under the limitation of guide limiting groove 3.

[0075] In this embodiment, as Figure 3 As shown, in this embodiment, by providing a guide limiting groove on the upper side of the guide limiting block 36, it is beneficial to slide the guide rail 361 on the guide limiting block 36, thereby facilitating the sliding of the height adjustment slider located on the upper part of the guide rail 361 relative to the guide limiting block 36.

[0076] Furthermore, such as Figure 3 As shown, the lower side of the height adjustment slider is provided with a guide limiting groove four. The guide limiting groove four extends out of the height adjustment slider along the extension direction of the guide limiting groove three. The guide rail two is installed in the guide limiting groove four. Furthermore, the guide rail two 361 is provided with a guide rail mounting hole two 3611. The guide rail two 361 is fixedly installed in the guide limiting groove four by connecting it with the guide rail mounting hole two 3611 with screws.

[0077] In this embodiment, as Figure 3 As shown, in this embodiment, the lower side of the height adjustment slider is provided with a guide mounting groove 2, and the guide mounting groove 2 extends out of the height adjustment slider along the extension direction of the guide limiting groove 3. This facilitates the installation of the guide rail 2 361 in the guide mounting groove 2, thereby making it easier for the height adjustment slider located on the upper part of the guide rail 2 361 to slide relative to the guide limiting block 2 36.

[0078] Furthermore, such as Figures 3 to 5As shown, the main body mounting section is provided with a second mounting and storage groove 171 and a sixth guide and limiting groove 181. The second guide and limiting block 36 is fixedly installed in the second mounting and storage groove 171, and the sixth guide and limiting groove 181 extends out of the main body mounting section along the extension direction of the third guide and limiting groove. The base 1 is also provided with a main body stop block 12, which is located on the left and right sides of the mounting main body 31. The main body stop block 12 is provided with a main body mounting groove 121. Both ends of the mounting main body 31 are movably installed in the main body mounting groove 121. One end of the mounting main body 31 is also provided with a mounting hole 122. The push rod 304 passes through the mounting hole 122 and is threadedly connected to the mounting hole 122. One end of the push rod 304 is provided with a push mounting protrusion 3041, and one end of the height adjustment slider 30 is provided with a push mounting groove 303. The push mounting protrusion 3041 is fixedly installed in the push mounting groove 303.

[0079] Furthermore, such as Figures 3 to 5 As shown, when the guide limit block 2 36 is installed in the installation and storage groove 2 171, limit stop blocks 2 362 are provided on both sides of the guide limit block 2 36.

[0080] One embodiment of this application, such as Figures 3 to 5 As shown, the straightening device for aero-engine blade wax models also includes: The height adjustment reference scale 161 is set on the upper side of the base 1. The height adjustment reference scale 161 is used to reference the distance that the height adjustment slider 30 slides in the left and right direction between the base 1 and the mounting body 31. Reference baseline 305 is set on the height adjustment slider 30, directly opposite the height adjustment reference scale 161.

[0081] In this embodiment, as Figures 3 to 5 As shown, in this embodiment, by setting the height adjustment reference scale 161 and the reference baseline 305, it is beneficial to accurately adjust the distance of the height adjustment slider 30 sliding in the left and right directions, which in turn is beneficial to accurately adjust the height position of the mounting body 31 and the lower straightening block 32 on it in the vertical direction, thereby improving the accuracy and stability of straightening the aero-engine blade wax model 8.

[0082] In addition to the technical solutions disclosed in this embodiment, the structure and working principle of the aero-engine blade wax model 8, the latch 35 and other latches in this utility model can be referred to conventional technical solutions in this technical field. However, these conventional technical solutions are not the focus of this utility model, and will not be described in detail here.

[0083] In this utility model, the term "multiple" refers to two or more unless otherwise explicitly defined. The terms "installation," "connection," "linking," and "fixing," etc., should be interpreted broadly. For example, "connection" can be a fixed connection, a detachable connection, or an integral connection; "linking" can be a direct connection or an indirect connection through an intermediate medium. Those skilled in the art can understand the specific meaning of the above terms in this utility model according to the specific circumstances.

[0084] In the description of this utility model, it should be understood that the terms "upper", "lower", "front", "rear", etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are only for the convenience of describing this application and simplifying the description, and do not indicate or imply that the device or unit referred to must have a specific orientation or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this application.

[0085] In the description of this specification, the terms "one embodiment," "some embodiments," "specific embodiment," etc., refer to a specific feature, structure, material, or characteristic described in connection with that embodiment or example, which is included in at least one embodiment or example of this application. In this specification, the illustrative expressions of the above terms do not necessarily refer to the same embodiment or example. Furthermore, the specific features, structures, materials, or characteristics described may be combined in any suitable manner in one or more embodiments or examples.

[0086] The above are merely preferred embodiments of this application and are not intended to limit this application. Various modifications and variations can be made to this application by those skilled in the art. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of this application should be included within the protection scope of this application.

Claims

1. A shaping device for wax models of aero-engine blades, characterized in that, include: Base; A blade straightening seat is mounted on the base. The blade straightening seat includes a mounting body, a lower straightening block, and an upper straightening block. The mounting body is mounted on the base. The lower straightening block is oscillatingly mounted on the mounting body and can oscillate relative to the mounting body in the height direction. The upper side of the lower straightening block has an arc-shaped groove with an open upper side. The upper straightening block is rotatably mounted on the lower straightening block and can rotate in the height direction. The lower side of the upper straightening block has an arc-shaped protrusion. The upper straightening block's ability to rotate relative to the lower straightening block in the height direction allows it to compress the wax model blade. The correction includes a compression correction position one and a deviation position one relative to the blade profile of the wax model; the aircraft engine blade wax model is placed between the arc-shaped groove one and the arc-shaped protrusion one; when the upper correction block one is placed at the compression correction position one, the blade profile segment correction channel one is defined between the arc-shaped groove one and the arc-shaped protrusion one, and the inner wall of the blade profile segment correction channel one compresses and corrects the profile of the blade profile segment one directly opposite it; when the upper correction block one is located at the deviation position one, the inner wall of the blade profile segment correction channel one releases the compression on the profile of the blade profile segment one directly opposite it. A swing drive mechanism is installed between the lower orthotic block and the mounting body. The lower orthotic block can swing relative to the mounting body in the height direction under the drive of the swing drive mechanism. The upper orthotic block can swing in the height direction as the lower orthotic block swings. The upper orthotic block can rotate in the height direction relative to the swinging lower orthotic block to have the compression correction position and the deviation position.

2. The straightening device for aero-engine blade wax molds according to claim 1, characterized in that, The first end of the mounting body in the left-right direction is provided with a support block, and the first end of the lower orthopedic block is provided with a push protrusion in the height direction directly opposite the support block, and the push protrusion is located above the support block. There is a gap between the support block and the push protrusion to form an adjustable pad embedding groove. The swing drive mechanism includes: An adjusting pad is detachably embedded in the pad embedding groove. During the process of embedding the adjusting pad into the pad embedding groove, the lower side of the adjusting pad abuts against the upper side of the support block, and the upper side of the adjusting pad pushes against the lower side of the pushing protrusion, causing the lower orthopedic block to swing relative to the mounting body in the height direction, and the upper orthopedic block to rotate relative to the swinging lower orthopedic block in the height direction. When the adjusting pad is fully embedded in the pad embedding groove, the upper orthopedic block is positioned at the compression correction position one. When the adjusting pad is removed from the pad embedding groove, the upper orthopedic block can rotate relative to the lower orthopedic block in the height direction to the deviation position one.

3. The straightening device for aero-engine blade wax molds according to claim 2, characterized in that, The adjusting pads are provided in multiple groups, and each group of adjusting pads includes multiple adjusting pads. The multiple adjusting pads in the same group of adjusting pads have the same thickness, while the multiple adjusting pads in different groups of adjusting pads have different thicknesses.

4. The straightening device for aero-engine blade wax molds according to claim 3, characterized in that, Also includes: A shelf is mounted on the base, and the shelf is provided with a resting part for holding a plurality of the adjusting pads.

5. The straightening device for aero-engine blade wax molds according to claim 2, characterized in that, The lower side of the adjusting pad forms a lower stop support surface, and the upper side of the adjusting pad has a stepped structure forming an upper stop support surface one and an upper stop support surface two. The thickness between the upper stop support surface one and the lower stop support surface is a first thickness, and the thickness between the upper stop support surface two and the lower stop support surface is a second thickness. The first thickness is greater than the second thickness.

6. The straightening device for aero-engine blade wax molds according to claim 5, characterized in that, An angle mark 1 is provided on the upper stop support surface 1, and an angle mark 2 is provided on the upper stop support surface 2; wherein, the angle mark 1 marks the angle at which the adjusting pad can push the lower orthopedic block 1 to swing relative to the mounting body 1 in the height direction when the first thickness is fully embedded in the pad insertion groove, and the angle mark 2 marks the angle at which the adjusting pad can push the lower orthopedic block 1 to swing relative to the mounting body 1 in the height direction when the second thickness is fully embedded in the pad insertion groove.

7. The straightening device for aero-engine blade wax molds according to claim 1, characterized in that, The mounting body 1 has an arc-shaped mounting groove 1 with an upper opening in the front-rear direction, and the lower straightening block 1 has an arc-shaped mounting protrusion 1 on its lower side. The arc-shaped mounting protrusion 1 is housed in the arc-shaped mounting groove 1 and can swing within the arc-shaped mounting groove 1. The mounting body one is also provided with an arc-shaped limiting protrusion one in the front-rear direction. The arc-shaped limiting protrusion one extends into the arc-shaped mounting groove one. The arc-shaped mounting protrusion one is provided with an arc-shaped limiting groove one directly opposite the arc-shaped limiting protrusion one. The arc-shaped limiting protrusion one extends into the arc-shaped limiting groove one. The arc-shaped limiting protrusion one can limit the angle of swing of the lower orthopedic block one relative to the mounting body one in the height direction.

8. The straightening device for aero-engine blade wax molds according to claim 7, characterized in that, Also includes: An auxiliary drive mechanism is installed between the mounting body and the lower orthopedic block, and the lower orthopedic block can swing in the height direction under the drive of the auxiliary drive mechanism, and the upper orthopedic block can swing in the height direction as the lower orthopedic block swings. The upper orthopedic block can rotate in the height direction relative to the swinging lower orthopedic block to have a suitable compression correction position and a deviation position.

9. The straightening device for aero-engine blade wax molds according to claim 8, characterized in that, The mounting body is provided with a movable clearance groove, which extends horizontally in the left-right direction. The second end of the mounting body is provided with a threaded through hole communicating with the movable clearance groove. The mounting body is also provided with a vertical clearance opening, which is located above and communicates with the movable clearance groove. The auxiliary drive mechanism includes: A drive slider is slidably installed in the movable clearance groove, and a limiting slot is provided on the upper side of the drive slider facing the vertical clearance opening; The drive rod is connected to the lower side of the arc-shaped mounting protrusion, facing the limiting slot, and the lower end of the drive rod extends into the limiting slot. A drive screw is threadedly connected to the threaded through hole. One end of the drive screw is connected to the drive slider, and the other end of the drive screw is provided with an adjusting grip. The adjusting grip is located on the outside of the mounting body. The drive slider can slide in the movable clearance groove under the pushing action of the drive screw, so that the drive rod extending into the limiting slot drives the lower orthopedic block to swing in the height direction. When the drive slider slides in the movable clearance groove, the drive rod can move left and right in the vertical clearance through hole.

10. The straightening device for aero-engine blade wax molds according to claim 1, characterized in that, Also includes: A height adjustment mechanism is installed between the base and the mounting body, and the mounting body can adjust its height in the vertical direction under the adjustment of the height adjustment mechanism.

11. The straightening device for aero-engine blade wax molds according to claim 10, characterized in that, The lower side of the mounting body is provided with a stop slope, which is inclined from left to right. The base is provided with a mounting part on its upper side facing the mounting body, which extends in the left-right direction. The height adjustment mechanism includes: A height adjustment slider is slidably mounted on the main body mounting part and can slide in the left and right directions. The upper side of the height adjustment slider is provided with a second stop slope that stops against the first stop slope. The second stop slope is inclined from left to right from low to high. A push rod is provided, one end of which is mounted on one end of the height adjustment slider. The height adjustment slider can slide between the base and the mounting body in the left-right direction under the pushing action of the push rod, thereby adjusting the height position of the mounting body in the vertical direction.

12. The straightening device for aero-engine blade wax molds according to claim 11, characterized in that, Also includes: A height adjustment reference scale is provided on the upper side of the base. The height adjustment reference scale is used to reference the distance that the height adjustment slider slides between the base and the mounting body in the left and right direction. The reference baseline is set on the height adjustment slider, directly opposite the height adjustment reference scale.

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