CN109530626B - Preparation method of turbine blade base - Google Patents

Abstract

A preparation method of a turbine blade base comprises the following steps of A, providing a casting device, wherein the casting device comprises a casting base, a fixed positioning block and a movable positioning block, so that a movable clamping part and the fixed clamping part form clamping and fixing of a tenon tooth, and B, casting a low-melting-point alloy. And step C, providing a dissolving and shaping device, wherein the dissolving and shaping device comprises a shaping base, the shaping base is provided with a hot oil cavity, and an alloy part which is arranged below the first horizontal plane and covers the locking piece groove in a wrapping mode is immersed in hot oil in the hot oil cavity, so that the locking piece groove is exposed from the rectangular block. The preparation of the rectangular block is completed. According to the preparation method of the turbine blade base, provided by the invention, the measurement period of the blade can be greatly shortened by preparing the standard base, and meanwhile, the production cost and the maintenance cost can be reduced.

Description

Preparation method of turbine blade base

Technical Field

The invention relates to the technical field of aero-engine production, in particular to a method for preparing a base for measuring blade parts in the production process of turbine blades of small and medium-sized aero-engines.

Background

In the manufacturing process of the aircraft engine, the turbine blade can be formed by casting a single blade part in a precision casting mode, and then the single blade part is assembled on the flange plate to form a turbine whole.

FIG. 1a is a schematic perspective view of a first stage turbine blade; FIG. 1b is a schematic perspective view of a two-stage turbine blade; FIG. 1c is a schematic perspective view of a free-turbine blade; FIG. 2a is a schematic illustration of a blade profile sizing of the first stage turbine blade of FIG. 1 a; FIG. 2b is a schematic illustration of platform sizing of the first stage turbine blade of FIG. 1 a; FIG. 2c is a schematic illustration of a measurement of the tip tab slot dimensions of the dovetail for the stage one turbine blade of FIG. 1 a; in fig. 2c, a schematic front view and a schematic left view of the measuring fixture during the measuring process are shown.

Referring to fig. 1a-2c, in the manufacturing process of a gas turbine, for each individual turbine blade casting produced through a precision casting process, it is generally required to measure the blade profile size of the blade body 11, the size of the platform 12 and the size of the locking plate slot 131 at the top of the tenon tooth 13 after the turbine blade 1 is cast, so as to judge whether the cast single blade is a qualified product.

In the existing measurement process, for the measurement of the blade profile size, as shown in fig. 2a, a pair of rolling rods 2 (corresponding special rolling rods 2, that is, rolling rods 2 with different diameters are designed for different types of blades 1) are required to clamp the tenon tooth 13 on a special vice, during the measurement, the rolling rods 2 are firstly aligned for establishing a coordinate system used during the blade measurement, and then a special measuring tool (not shown in the figure) is used for measuring the blade profile size of the blade body 11.

For the measurement of the dimension of the flange 12, as shown in fig. 2b, a special measuring tool is used to clamp all the tenon teeth 13, expose the flange 12, and measure the dimension of the flange 12 with a special measuring tool (not shown).

For the dimension measurement of the locking piece slot 131 at the top of the tenon tooth 13, as shown in fig. 2c, a special measurement tool needs to be used to clamp the tenon tooth 13 and expose the top tooth portion, so that the locking piece slot 131 can not be blocked, and then a special measurement tool (not shown in the figure) is used to measure the relevant dimension of the locking piece slot 131.

Although each individual turbine blade 1 produced by the precision casting process has a cylindrical process boss 14 with dimensional accuracy guaranteed, the process boss 14 is mainly used for clamping and positioning of subsequent machining processes in the existing production process, and the process boss 14 is not physically used (for example, clamping, positioning and the like) in the existing measurement process.

As shown in fig. 2a, in the conventional blade measurement process, the theoretical reference coordinate system of the blade 1 is generally established by using the rolling rods 2 tightly clamping the tenon teeth 13 of the blade 1 (generally, the first pair of concave parts clamped at two sides of the top teeth of the tenon teeth 13 as shown in fig. 2 a) to establish a datum plane, that is, an x-y plane is established according to the axes of two theoretically parallel rolling rods 2, the axis of the cylindrical process boss 14 of the blade 1 is taken as a z-axis, the intersection point of the z-axis and the x-y plane is taken as an origin, the x-axis passes through the origin and is parallel to the axis of the rolling rods 2, and the y-axis is perpendicular to the x-axis. In the theoretical reference coordinate system of the blade 1, the z-axis is used to indicate the position relationship among the blade body 11, the platform 12 and the tenon tooth 13, and it is usually directed in the direction from the tenon tooth 13 to the blade body 11, and the x-axis and the y-axis are mainly used to indicate the tooth shape of the tenon tooth 13, so the directions of the x-axis and the y-axis can be adjusted according to the need (e.g. the matching convenience with the reference coordinate system of the measuring tool during the measurement), that is, the direction of the x-axis may be the direction from the air inlet side of the blade to the air outlet side, or vice versa, and the direction of the y-axis may be the direction from the basin side to the back side of the blade, or vice versa.

During measurements with different measuring tools or for different types of blades, the theoretical reference coordinate system can be translated according to the actual conditions of the measuring tools, i.e. for the measuring instruments to facilitate reading, the origin of the theoretical reference coordinate system of the blade 1 can be moved in the direction of the three coordinate axes by Δ x, Δ y, Δ z, respectively, so as to be able to coincide with the reference coordinate system of the measuring instrument. Of course, it will be appreciated by those skilled in the art that the theoretical reference frame of the blade may also be rotated as shown in figures 2b, 2c in order to facilitate operation of the surveying instrument.

As described above, for different turbine blades as shown in fig. 1a to 1c, the existing measurement process methods are all that, when measuring the blade profile of the blade body 11, a dedicated measurement tool is used to clamp the tenon tooth 13 (for example, a first pair of concave parts on both sides of the top tooth of the tenon tooth 13 are clamped by a pair of rolling bars 2 on a dedicated vice) to expose the blade profile, and the size of the blade profile is measured by positioning the tenon tooth 13; when the relevant dimension of the locking piece slot 131 at the top of the tenon tooth 13 is measured, replacing a special measuring tool, clamping most of the tenon teeth 13 and exposing the tops of the tenon teeth, thereby measuring the relevant dimension of the locking piece slot 131; when the size of the flange plate 12 is measured, a plurality of sets of special measuring tools need to be replaced according to the change of the measuring position, the tenon tooth 13 is clamped to expose the measured position of the flange plate 12, and the relevant size is measured.

The existing measuring method has a complex and complicated process, for example, when the blade profile is measured, in the process of clamping the roller bars 2 by using a vice, the horizontal degree of the two roller bars 2 can finally influence the precision of the blade profile data obtained by measurement, so that an operator has to have rich experience to ensure the efficiency of the process of clamping the roller bars 2; and for the special measuring tool for measuring the flange plate 12 and the locking plate groove 131, as shown in fig. 2b and 2c, if the gap of the installation groove is too large, the blade state after clamping is difficult to ensure to be consistent, and if the gap is too small, the blade is difficult to be installed, so that the manufacturing difficulty of the installation groove is large, and the precision is difficult to ensure. Moreover, in order to avoid damage to the blade, the hardness of the material used for manufacturing the special measuring tool (especially the mounting groove position) is generally lower than that of the blade 1, so that the mounting groove is easily worn during use, and the size is changed.

In the measuring process, each measuring part needs a special tool, so that each blade needs multiple sets of special tools, and the production cost is high. In addition, the large number of the tools also causes great management difficulty and increases the maintenance difficulty of the tools. And because the whole process is manually operated, the clamping and measuring process of each size requires a skilled operation skill of an operator.

The existing measuring process has low operation efficiency. For at least hundreds of finished products of various blade precision castings in each batch in actual production, each blade needs to be measured, so that the measuring process needs to consume a long time, and the measuring process can become one of important factors for prolonging the whole production period.

Disclosure of Invention

The technical problem to be solved by the present invention is to provide a method for manufacturing a turbine blade base, which reduces or avoids the aforementioned problems.

In order to solve the technical problem, the invention provides a method for preparing a turbine blade base, the base is used for measuring the blade profile size of a blade body of a turbine blade, the size of an edge plate and the size of a locking plate groove at the top of a tenon tooth, a rectangular block which is formed by casting a low-melting-point alloy and surrounds the tenon tooth, the blade slots are not covered by the low melting point alloy, the turbine blade has a theoretical reference coordinate system, the z-axis of the theoretical reference coordinate system is coincident with the axis of the technological boss of the blade, the x-y plane of the theoretical reference coordinate system can be established by two axes of two standard rolling rods in a clamping state, the two axes can clamp the first pair of concave parts on two sides of the top tooth of the tenon tooth, the intersection point of the z-axis and the x-y plane is an original point, the x-axis passes through the original point and is parallel to the axes of the rolling rods, and the y-axis is perpendicular to the x-axis. The rectangular block comprises a first side vertical face, a second side vertical face, a third side vertical face and a fourth side vertical face which are sequentially connected, the first side vertical face and/or the third side vertical face are parallel to an x axis of a theoretical reference coordinate system, the second side vertical face and/or the fourth side vertical face are parallel to a y axis of the theoretical reference coordinate system, the rectangular block further comprises a first horizontal plane which is perpendicular to a z axis of the theoretical reference coordinate system and close to the locking piece groove, one face, opposite to the first horizontal plane, of the rectangular block is a top face, and the minimum distance between the top face of the rectangular block and the edge plate in the z axis direction is not less than 2 mm. Which comprises the following steps of,

step A, a casting device is provided, the casting device comprises a casting base, a fixed positioning block and a movable positioning block, the fixed positioning block is fixedly connected with the casting base, the movable positioning block is slidably connected with the casting base, the fixed positioning block is provided with a fixed clamping part with a molded surface consistent with a semi-circular arc surface of a standard rolling rod, the movable positioning block is provided with a movable clamping part with a molded surface consistent with a semi-circular arc surface of a standard rolling rod, a first pair of concave parts on two sides of a top tooth of a tenon tooth is attached to the fixed clamping part of the fixed positioning block, then the movable positioning block is moved, the movable clamping part and the fixed clamping part form a pair, the tenon tooth is clamped and fixed, and then the movable positioning block is fixed.

And B, pouring the low-melting-point alloy into a closed cavity formed by the casting base and the movable positioning block and used for pouring the low-melting-point alloy, brushing the low-melting-point alloy on the low-melting-point alloy by using a brush dipped in cold water after pouring, waiting for about 5 seconds, loosening the movable positioning block after the low-melting-point alloy is cooled and solidified, and taking out the blade.

And step C, providing a dissolving and shaping device, wherein the dissolving and shaping device comprises a shaping base, the shaping base is connected with a lifting arm capable of lifting, the lifting arm is provided with a process boss fastening device, a process boss of the blade to be measured is inserted and installed in the process boss fastening device, so that the blade is hoisted on the lifting arm, the shaping base is provided with a hot oil cavity, the hot oil cavity is arranged below the lifting arm, hot oil with the temperature not lower than 180 ℃ is injected into the hot oil cavity, the height position of the lifting arm is adjusted, the alloy part of the locking piece groove covering the top of the tenon tooth, which is wrapped below the first horizontal plane, is immersed into the hot oil of the hot oil cavity, and the locking piece groove is exposed from the rectangular block 3. The preparation of the rectangular block is completed.

Preferably, in step a, the casting base is provided with three side walls connected in sequence, the fixed positioning block is fixedly connected with the casting base by the middle side wall, the casting base is provided with a guide groove on the side opposite to the middle side wall, and the movable positioning block is slidably connected with the casting base through a guide block matched with the guide groove.

Preferably, in the step a, a lifting rod is arranged on a side wall of the casting base in the middle, a horizontal telescopic rod is arranged at the top of the lifting rod, the horizontal telescopic rod comprises a T-shaped rod, after a first blade is clamped and fixed, the position of the T-shaped rod is adjusted, so that a cross rod of a T-shaped head of the T-shaped rod is supported against the process boss, the position of the T-shaped rod is fixed, and in a subsequent clamping process of the blade, the initial position of the blade is positioned by using the T-shaped rod.

Preferably, in step a, the fixed positioning top surface of the fixed positioning block is used for molding the first horizontal surface.

Preferably, in step a, a scale is marked on the fixed clamping part.

Preferably, in step C, the process boss fastening device is rotatably connected to the suspension arm through a bearing, and when the blade is hoisted and immersed in hot oil, the blade is rotated to accelerate the dissolution of the alloy.

According to the preparation method of the turbine blade base, provided by the invention, the measurement period of the blade can be greatly shortened by preparing the standard base, and meanwhile, the production cost and the maintenance cost can be reduced.

Drawings

The drawings are only for purposes of illustrating and explaining the present invention and are not to be construed as limiting the scope of the present invention. Wherein the content of the first and second substances,

FIG. 1a is a schematic perspective view of a first stage turbine blade;

FIG. 1b is a schematic perspective view of a two-stage turbine blade;

FIG. 1c is a schematic perspective view of a free-turbine blade;

FIG. 2a is a schematic illustration of a blade profile sizing of the first stage turbine blade of FIG. 1 a;

FIG. 2b is a schematic illustration of platform sizing of the first stage turbine blade of FIG. 1 a;

FIG. 2c is a schematic illustration of a measurement of the tip tab slot dimensions of the dovetail for the stage one turbine blade of FIG. 1 a;

FIG. 3a is a schematic view of a turbine blade base prepared according to a turbine blade base preparation method of an embodiment of the present invention for blade profile sizing of a turbine blade;

FIG. 3b is a schematic illustration of platform sizing of the turbine blade of FIG. 3 a;

FIG. 3c is a schematic illustration of a tooth top cleat slot size measurement taken on the turbine blade of FIG. 3 a;

FIG. 4a is a schematic partial cross-sectional structural view of an apparatus for preparing the base of FIG. 3 a;

FIG. 4b is a schematic view of the structure of FIG. 4a in a partial section;

FIG. 4c is a schematic perspective view of the backup bar of FIG. 4 a;

FIG. 4d is a schematic perspective view of a rectangular block formed by the casting apparatus of FIG. 4 a;

fig. 5 is a schematic partial sectional structural view of a dissolution reshaping apparatus for reshaping the rectangular block prepared in fig. 4 a.

Detailed Description

In order to more clearly understand the technical features, objects, and effects of the present invention, embodiments of the present invention will now be described with reference to the accompanying drawings. Wherein like parts are given like reference numerals.

FIG. 1a is a schematic perspective view of a first stage turbine blade; FIG. 2a is a schematic illustration of a blade profile sizing of the first stage turbine blade of FIG. 1 a; FIG. 3a is a schematic view of a turbine blade base prepared according to a turbine blade base preparation method of an embodiment of the present invention for blade profile sizing of a turbine blade; FIG. 3b is a schematic illustration of platform sizing of the turbine blade of FIG. 3 a; FIG. 3c is a schematic illustration of a tooth top cleat slot size measurement taken on the turbine blade of FIG. 3 a; FIG. 4a is a schematic partial cross-sectional structural view of an apparatus for preparing the base of FIG. 3 a; FIG. 4b is a schematic view of the structure of FIG. 4a in a partial section; FIG. 4c is a schematic perspective view of the backup bar of FIG. 4 a; FIG. 4d is a schematic perspective view of a rectangular block formed by the casting apparatus of FIG. 4 a; fig. 5 is a schematic partial sectional structural view of a dissolution reshaping apparatus for reshaping the rectangular block prepared in fig. 4 a. Referring to fig. 1a, 2a, 3a-5, the present invention provides a method for manufacturing a turbine blade base, the base is used for measuring the blade profile size of a blade body 11 of a turbine blade 1, the size of a flange 12 and the size of a locking plate groove 131 at the top of a tenon tooth 13, the base is a rectangular block 3 which is formed by casting a low-melting-point alloy and surrounds the tenon tooth 13, the locking plate groove 131 is not covered by the low-melting-point alloy and exposes the rectangular block 3, the turbine blade 1 has a theoretical reference coordinate system, the z-axis of the theoretical reference coordinate system is coincident with the axis of a process boss 14 of the blade 1, the x-y plane of the theoretical reference coordinate system can be established by two axes of two standard rolling rods 2 which can clamp a first pair of recesses at two sides of a top tooth of the tenon tooth 13 in a clamping state, the intersection point of the z-axis and the x-y plane is an origin, the x-axis passes through the origin and is parallel to the axis of the roller 2, and the y-axis is perpendicular to the x-axis. The rectangular block 3 comprises a first side elevation, a second side elevation, a third side elevation and a fourth side elevation which are connected in sequence, the first side elevation and/or the third side elevation is parallel to an x axis of the theoretical reference coordinate system, the second side elevation and/or the fourth side elevation is parallel to a y axis of the theoretical reference coordinate system, the rectangular block 3 further comprises a first horizontal plane 31 which is perpendicular to a z axis of the theoretical reference coordinate system and close to the locking piece groove 131, one surface of the rectangular block 3 opposite to the first horizontal plane 31 is a top surface, and the minimum distance between the top surface of the rectangular block and the flange plate 12 in the z axis direction is not less than 2 mm. Which comprises the following steps of,

step a, providing a casting device 4, where the casting device 4 includes a casting base 41, a fixed positioning block 42 and a movable positioning block 43, the fixed positioning block 42 is fixedly connected to the casting base 41, the movable positioning block 43 is slidably connected to the casting base 41, the fixed positioning block 42 is provided with a fixed clamping portion 422 having a profile consistent with a semi-circular arc surface of the standard rolling rod 2, the movable positioning block 43 is provided with a movable clamping portion 432 having a profile consistent with a semi-circular arc surface of the standard rolling rod 2, a first tooth socket (i.e., a first pair of concave portions on both sides of a top tooth) of the tenon tooth 13 of the blade 1 is attached to the fixed clamping portion 422 of the fixed positioning block 42, and then the movable positioning block 43 is moved so that the movable clamping portion 432 and the fixed clamping portion 422 form clamping fixation to the tenon tooth 13, the movable positioning block 43 is then fixed, so that the blade 1 can be clamped and fixed by a pair of standard rolling bars 2 on a special vice as the tenon tooth 13 is clamped by a pair of standard rolling bars 2 when the blade profile dimension is measured in the prior art as described in the background.

Referring to fig. 4a and 4b, the casting base 41 may be provided with three sidewalls connected in sequence, the fixed positioning block 42 may be fixedly connected to the casting base 41 by a countersunk bolt (not shown) or the like depending on the middle sidewall, the casting base 41 may be provided with a guide slot 411 at a side opposite to the middle sidewall, such that the movable positioning block 43 may be slidably connected to the casting base 41 by providing a guide block matching with the guide slot 411, and when the movable clamping portion 432 and the fixed clamping portion 422 form a clamping fixation to the tenon 13, the three sidewalls of the casting base 41 and the movable positioning block 43 may form a closed cavity for casting a low melting point alloy.

The fixed clamping portion 422 and the movable clamping portion 432 are both provided with a profile which is consistent with the semi-circular arc surface of the standard rolling rod 2, so that the x-y plane of the theoretical reference coordinate system of the blade 1 can be fixed by clamping and fixing the tenon tooth 13 by the fixed clamping portion 422 and the movable clamping portion 432, and because only the fixable line of the movable clamping portion 432 moves linearly during operation, the clamping of the fixed clamping portion 422 and the movable clamping portion 432 is easier to operate than the clamping of the tenon tooth 13 by the pair of standard rolling rods 2 on a special vice during the measurement of the size of the blade profile in the prior art, which is described in the background art, so that the skill requirement of an operator can be greatly reduced.

For different types of blades 1, the casting base 41 can be used for forming a closed cavity for casting the low-melting-point alloy by only providing the corresponding fixed positioning block 42 and the corresponding movable positioning block 43 according to a targeted design. Therefore, the manufacturing cost of the tool can be greatly reduced.

For convenience of operation, the casting base 41 may be further provided with a lifting rod 412 on the middle side wall, the top of the lifting rod is provided with a horizontal telescopic rod 413, the horizontal telescopic rod 413 comprises a T-shaped rod 414, so that, for each type of said blades 1, the clamping of the first piece of said blade 1 can be carried out by a skilled worker by hand, when the first piece of said blade 1 is clamped and fixed, the position of the T-bar 414 can be adjusted so that the cross-bar of the T-head of the T-bar 414 comes into abutment with the technological boss 14 of the blade 1, and fixes the position of the T-bar 414 so that, during subsequent clamping of the blade 1, even if unskilled operators can also utilize the T-shaped rod 414 to complete the positioning of the initial position of the blade 1, so that the clamping difficulty can be reduced, and the clamping efficiency can be greatly improved.

The fixed positioning top surface 421 of the fixed positioning block 42 may be used to form the first horizontal surface 31, and as long as the precision of the movable positioning block 43 can be well controlled, the movable positioning top surface 431 of the movable positioning block 43 may also be used to form the first horizontal surface 31, and of course, in the subsequent measurement process, only the surface formed by the fixed positioning top surface 421 of the fixed positioning block 42 may be used as the first horizontal surface 31, so that the manufacturing requirement on the fixed positioning top surface 421 of the movable positioning block 43 may be reduced, and the manufacturing cost may be reduced.

Since the clamping of the standard roller 2 to the blade 1 can be repeated by the fixed clamping portion 422 and the movable clamping portion 432, the first side elevation, the third side elevation, the second side elevation and the fourth side elevation of the blade 1 can be easily prepared by the side wall of the closed cavity for casting the low melting point alloy, which is formed by the casting base 41 and the movable positioning block 43.

And step B, pouring the low-melting-point alloy into a closed cavity for pouring the low-melting-point alloy, which is formed by the pouring base 41 and the movable positioning block 43, dipping cold water by using a brush after pouring, brushing the low-melting-point alloy on the low-melting-point alloy, waiting for about 5 seconds, cooling and solidifying the low-melting-point alloy, and loosening the movable positioning block 43 to take out the blade 1 provided with the rectangular block 3.

Since the fixed clamping portion 422 and the movable clamping portion 432 can clamp the tenon tooth 13, no low-melting-point alloy part exists at the part of the rectangular block 3 cast and molded in this step, that is, a cavity exists in the part of the rectangular block 3 where the tenon tooth 13 is clamped.

FIG. 4d is a schematic perspective view of a rectangular block formed by the casting apparatus of FIG. 4 a; referring to fig. 4d, a schematic perspective view of the rectangular block 3 is shown, wherein the two symmetrical grooves on the two sides of the rectangular block 3 are the strip-shaped cavities 32 formed by the fixed clamping parts 422 and the movable clamping parts 432, and the top protrusions are the structures formed by the space of the low-melting-point alloy flowing into the guide slots 411.

Step C, providing a dissolving and shaping device 5, wherein the dissolving and shaping device 5 comprises a shaping base 51, the shaping base 51 is connected with a lifting arm 511 capable of ascending and descending, the lifting arm 511 is provided with a process boss fastening device 54, the process boss 14 of the blade 1 to be measured is inserted and installed in the process boss fastening device 54, the blade 1 is locked in the process boss fastening device 54 through a screw, the blade 1 is hung on the lifting arm 511, the shaping base 51 is provided with a hot oil cavity 52, the hot oil cavity 52 is arranged below the lifting arm 511, hot oil with the temperature not lower than 180 ℃ is filled in the hot oil cavity 52, and the alloy part of the locking piece groove 131 covering the top of the tenon tooth 13 below the first horizontal plane 31 can be immersed in the hot oil cavity 52 by adjusting the height position of the lifting arm 511, this causes the alloy covering the tab slot 131 at the top of the tenon tooth 13 to be dissolved, thereby exposing the tab slot 131 from the rectangular block 3. Lifting the suspension arm 511 to remove the tenon tooth 13 from contact with the hot oil in the hot oil chamber 52, and removing the blade 1, thereby completing the preparation of the rectangular block 3.

As shown in fig. 5, an oil outlet may be disposed at the bottom of the hot oil chamber 52, and an oil filling port may be disposed at the top thereof, so that the hot oil chamber 52 may be connected to the hot oil circulation processing apparatus 6 through a pipeline, thereby ensuring the temperature of the hot oil in the hot oil chamber 52 and timely recovering the low melting point alloy dissolved in the hot oil.

The hot oil circulation treatment device 6 may comprise a cooling tank (not shown) and a heater (not shown) connected in sequence, and the specific structure may refer to the structure of the cooling tank and the heater adopted in the blade cavity low melting point alloy removing device provided by the inventor's team in chinese patent 201611189008.2, and will not be described herein again.

After the blade 1 is hung on the process boss fastening device 54, the z-axis position of the blade 1 is fixed on the suspension arm 511, so that the position of the rectangular block 3 of the blade 1 immersed in the hot oil chamber 52 can be controlled by controlling the lifting and lowering of the suspension arm 511. Since the first horizontal surface 31 is located in the bar-shaped cavity 32, the contact of the first horizontal surface 31 with the hot oil in the hot oil chamber 52 can also be controlled by observing the position of the bar-shaped cavity 32, thereby controlling the position of the rectangular block 3 immersed in the hot oil.

If the rectangular block 3 is left to stand in hot oil only, it usually takes 10-15 minutes to ensure that the alloy covering the tab slot 131 is completely dissolved.

The process boss fastening device 54 may also be rotatably connected to the suspension arm 511 through a bearing, so that after the blade 1 is hoisted and immersed in hot oil, the blade 1 may be rotated, thereby increasing the speed of alloy dissolution, and in order to better control the rotation of the blade 1, the process boss fastening device 54 may be fixedly connected to the bearing on the suspension arm 511, and may be provided with a rod portion 541 extending out of the top surface of the suspension arm 511, so that the motor 7 may be connected through a belt, a gear, and the like arranged on the extended rod portion 541, thereby more precisely controlling the rotation speed of the blade 1.

When the rotating speed of the blade 1 is controlled to be 10-20 revolutions per minute, the rectangular block 3 is soaked in hot oil for 5-8 minutes to completely dissolve the alloy coating the locking piece groove 131.

Because the low-melting-point alloy has good hardness and strength, the rectangular block 3 surrounding the tenon tooth 13 is formed by casting the low-melting-point alloy, and the low-melting-point alloy shrinks towards the tenon tooth 13 after being cooled, solidified and shaped, so that the tenon tooth 13 is firmly clamped by the tooth profile of the tenon tooth 13.

Since the first side elevation and/or the third side elevation of the rectangular block 3 are parallel to the x-axis of the theoretical reference coordinate system, the second side elevation and/or the fourth side elevation are parallel to the y-axis of the theoretical reference coordinate system, and the first horizontal plane 31 is perpendicular to the z-axis of the theoretical reference coordinate system, i.e. the first horizontal plane 31 is parallel to the x-y plane, the reference coordinate system of the blade 1 can be defined by limiting the outer surface of the rectangular block 3, and the theoretical reference coordinate system of the blade 1 can be easily made parallel to the reference coordinate system of the measuring instrument, so that the blade 1 can be conveniently positioned and fixed by using similar fixtures capable of limiting at least three surfaces in each measuring stage, and the reference coordinate system of the measuring instrument can be conveniently adjusted to coincide with the theoretical reference coordinate system of the blade 1, the measuring tool and the measuring tool structure in each measuring process can be simplified. And improve the measurement efficiency.

The first side elevation and/or the third side elevation and the second side elevation and/or the fourth side elevation of the rectangular block 3 are mainly used for clamping and positioning, and in the subsequent measurement process, the reference coordinate system of the blade 1 can be controlled by positioning the process boss 14, so that the first side elevation and/or the third side elevation and/or the second side elevation and/or the fourth side elevation are only required to be not too close to the flange plate 12 and have a certain distance (for example, the minimum distance is not less than 5mm, the maximum distance is not more than 30mm, and if the distance is too large, the rectangular block 3 is easy to have a large volume, and the energy consumption in the manufacturing process is wasted), and therefore, in the step a, when the blade 1 is fixed, only the flange plate 12 is required to be kept at a certain distance from the side wall of the casting cavity.

The minimum distance between the top surface of the rectangular block 3 and the flange 12 in the z-axis direction can be controlled to be larger than 2mm, so that the space requirement for measuring the size of the flange 12 can be ensured.

The minimum distance between the first horizontal surface 31 and the locking piece slot 131 in the z-axis direction can be greater than 1.5 mm. This leaves sufficient measurement space for the locking piece slot 131.

In practice, for 3 turbine blades of a certain type of engine, casting equipment can be combined into one set when the method is adopted, and the casting forming of different types of blade bases can be realized only by replacing the positioning templates. And the structure of the measuring tool and the measuring tool in the measuring process is greatly simplified, so that the preparation time for replacing the measuring tool is greatly shortened, and compared with the original process method in the background technology, the time for construction period can be shortened by about 50%. Moreover, because the measuring tools are reduced, the production cost is greatly reduced, and the tool cost can be reduced by about 60 percent compared with the original measuring method in the background technology. In the measuring process, because the planes such as the side vertical face and the horizontal plane of the rectangular block 3 are positioned and clamped, the high-precision loose block positioning in the background technology can be avoided, the manufacturing cost of the tool is reduced, and the difficulty in tool maintenance is also reduced.

According to the preparation method of the turbine blade base, provided by the invention, the measurement period of the blade can be greatly shortened by preparing the standard base, and meanwhile, the production cost and the maintenance cost can be reduced.

It should be appreciated by those of skill in the art that while the present invention has been described in terms of several embodiments, not every embodiment includes only a single embodiment. The description is given for clearness of understanding only, and it is to be understood that all matters in the embodiments are to be interpreted as including technical equivalents which are related to the embodiments and which are combined with each other to illustrate the scope of the present invention.

The above description is only an exemplary embodiment of the present invention, and is not intended to limit the scope of the present invention. Any equivalent alterations, modifications and combinations can be made by those skilled in the art without departing from the spirit and principles of the invention.

Claims (6)

1. A turbine blade base manufacturing method is characterized in that the base is a rectangular block which is formed by casting low-melting-point alloy and surrounds a tenon tooth, the size of a blade profile of a blade body of a turbine blade and the size of a locking plate groove at the top of the tenon tooth are measured, the locking plate groove is not covered by the low-melting-point alloy, the turbine blade is provided with a theoretical reference coordinate system, the z axis of the theoretical reference coordinate system is coincident with the axis of a process boss of the blade, the x-y plane of the theoretical reference coordinate system is established by two axes of two standard rolling rods which can clamp a first pair of concave parts at two sides of the top tooth of the tenon tooth in a clamping state, the intersection point of the z axis and the x-y plane is an origin, the x axis passes through the origin and is parallel to the axes of the rolling rods, and the y axis is perpendicular to the x axis; the rectangular block comprises a first side elevation, a second side elevation, a third side elevation and a fourth side elevation which are sequentially connected, the first side elevation and/or the third side elevation is parallel to an x axis of the theoretical reference coordinate system, the second side elevation and/or the fourth side elevation is parallel to a y axis of the theoretical reference coordinate system, the rectangular block further comprises a first horizontal plane which is perpendicular to a z axis of the theoretical reference coordinate system and close to the locking piece groove, one surface of the rectangular block, opposite to the first horizontal plane, is a top surface, and the minimum distance between the top surface of the rectangular block and the edge plate in the z axis direction is not less than 2 mm; which comprises the following steps of,

step A, providing casting equipment, wherein the casting equipment comprises a casting base, a fixed positioning block and a movable positioning block, the fixed positioning block is fixedly connected with the casting base, the movable positioning block is slidably connected with the casting base, the fixed positioning block is provided with a fixed clamping part with a molded surface consistent with a semi-circular arc surface of a standard rolling rod, the movable positioning block is provided with a movable clamping part with a molded surface consistent with a semi-circular arc surface of the standard rolling rod, a first pair of concave parts on two sides of a top tooth of a tenon tooth are attached to the fixed clamping part of the fixed positioning block, then the movable positioning block is moved, the movable clamping part and the fixed clamping part form clamping fixation on the tenon tooth, and then the movable positioning block is fixed;

b, pouring a low-melting-point alloy in a closed cavity formed by the casting base and the movable positioning block and used for pouring the low-melting-point alloy, brushing the low-melting-point alloy with a brush dipped in cold water after pouring, waiting for about 5 seconds, loosening the movable positioning block after the low-melting-point alloy is cooled and solidified, and taking out the blade;

step C, providing a dissolving and shaping device, wherein the dissolving and shaping device comprises a shaping base, the shaping base is connected with a lifting arm capable of lifting, the lifting arm is provided with a process boss fastening device, a process boss of the blade to be measured is inserted and installed in the process boss fastening device, so that the blade is hoisted on the lifting arm, the shaping base is provided with a hot oil cavity, the hot oil cavity is arranged below the lifting arm, hot oil with the temperature not lower than 180 ℃ is injected into the hot oil cavity, the height position of the lifting arm is adjusted, an alloy part of the locking piece groove, which is wrapped and covered on the top of the tenon tooth, below the first horizontal plane is immersed in the hot oil of the hot oil cavity, and the locking piece groove is exposed from the rectangular block; the preparation of the rectangular block is completed.

2. The method as claimed in claim 1, wherein in step a, the casting base is provided with three side walls connected in sequence, the fixed positioning block is fixedly connected with the casting base by the middle side wall, the casting base is provided with a guide groove at the side opposite to the middle side wall, and the movable positioning block is slidably connected with the casting base through a guide block matched with the guide groove.

3. The method according to claim 1, wherein in the step a, the casting base is provided with a lifting rod on the side wall in the middle, the top of the lifting rod is provided with a horizontal telescopic rod, the horizontal telescopic rod comprises a T-shaped rod, after the first blade is clamped and fixed, the position of the T-shaped rod is adjusted, so that a cross rod of the T-shaped head of the T-shaped rod is abutted against the technological boss, the position of the T-shaped rod is fixed, and in the subsequent clamping process of the blade, the initial position of the blade is positioned by using the T-shaped rod.

4. The method of claim 1, wherein in step a, the fixed locating top surface of the fixed locating block is used to shape the first horizontal surface.

5. The method of claim 1, wherein in step a, the fixed clamp is marked with a scale.

6. The method of claim 1, wherein in step C, the process boss fastening device is rotatably connected to the boom arm by a bearing, and the blade is rotated to accelerate the dissolution of the alloy after being lifted and immersed in hot oil.

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