CN109434396A - A method of manufacture is used for the integrated base of Blade measuring - Google Patents

A method of manufacture is used for the integrated base of Blade measuring Download PDF

Info

Publication number
CN109434396A
CN109434396A CN201811497600.8A CN201811497600A CN109434396A CN 109434396 A CN109434396 A CN 109434396A CN 201811497600 A CN201811497600 A CN 201811497600A CN 109434396 A CN109434396 A CN 109434396A
Authority
CN
China
Prior art keywords
blade
axis
rectangular block
casting
locking plate
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN201811497600.8A
Other languages
Chinese (zh)
Other versions
CN109434396B (en
Inventor
张小青
梁涛
王科昌
周彭博
蒋万里
李怡
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
AECC South Industry Co Ltd
Original Assignee
AECC South Industry Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by AECC South Industry Co Ltd filed Critical AECC South Industry Co Ltd
Priority to CN201811497600.8A priority Critical patent/CN109434396B/en
Publication of CN109434396A publication Critical patent/CN109434396A/en
Application granted granted Critical
Publication of CN109434396B publication Critical patent/CN109434396B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/04Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from several pieces

Abstract

A method of manufacture is used for the integrated base of Blade measuring comprising following steps: step A constructs a casting type chamber, by blade vertical lifting above the casting type chamber.Step B forms the blank of rectangular block in the intracavitary casting low-melting alloy of the casting type of step A.Step C carries out local heat treatment for the blank of the rectangular block manufactured by step B, melts the alloy structure for eliminating covering locking plate slot, so that the locking plate slot is completely exposed.Complete the manufacture of the rectangular block.A kind of method of integrated base of the manufacture provided by the present invention for Blade measuring substantially reduces the measurement duration of blade, and effectively reduce production cost and maintenance cost by providing standardized pedestal for blade.

Description

A method of manufacture is used for the integrated base of Blade measuring
Technical field
The present invention relates to aero-engine production technical field, in particular to a kind of turbine in Small Aeroengine In blade manufacturing process, the manufacturing method of the integrated base for being measured to blade part.
Background technique
In the manufacturing process of aero-engine, the mode that hot investment casting can be used in turbo blade carries out single blade part Casting and forming, then single blade part is assembled on listrium, assembling formed turbine entirety.
Fig. 1 a is a kind of stereochemical structure schematic illustration of Turbine Blade;Fig. 1 b is a kind of the vertical of second turbine blade Body principle schematic diagram;Fig. 1 c is a kind of stereochemical structure schematic illustration of free turbine blade;Fig. 2 a is to the one of Fig. 1 a Grade turbo blade carries out the schematic illustration of blade profile dimensional measurement;Fig. 2 b is to carry out listrium size to the Turbine Blade of Fig. 1 a The schematic illustration of measurement;Fig. 2 c is that the principle for carrying out the slot dimensional measurement of tenon tooth locking tab to the Turbine Blade of Fig. 1 a is shown It is intended to;In figure 2 c, it is shown that in measurement process, the facing structure schematic illustration and left view structural principle of measured material are illustrated Figure.
Referring to shown in Fig. 1 a-2c, in gas turbine manufacturing process, for every kind produced by hot investment casting process Individual turbo blade casting requires usually after 1 Foundry Production of turbo blade comes out to the blade profile size of blade 11, edge 131 size of locking plate slot at 13 top of size and tenon tooth of plate 12 measures, so that the single blade for judging that Foundry Production goes out is No is qualified product.
In existing measurement process, the measurement for blade profile size needs on special vice with a pair as shown in Figure 2 a Roller 2 (having corresponding dedicated roller 2, that is, the roller 2 of different-diameter for the different types of design of blade 1) is clamped Tenon tooth 13, elder generation's centering roller 2, for establishing coordinate system when Blade measuring, reuses special measuring tool and (does not regard in figure when measurement The blade profile size of blade 11 is measured out).
Measurement for 12 size of listrium needs to clamp whole tenon tooths 13 using special measurement tooling as shown in Figure 2 b, will Listrium 12 exposes, then the size of listrium 12 is measured with special measuring tool (not regarding out in figure).
Dimensional measurement for 13 locking tab slot 131 of tenon tooth need to use special measurement tooling to clamp tenon as shown in Figure 2 c Tooth 13 simultaneously exposes apical tooth position, and the locking plate slot 131 is not blocked, and reuses special measuring tool (not regarding out in figure) survey Measure 131 relative dimensions of locking plate slot.
Although the every kind of individual turbo blade 1 produced by hot investment casting process all accuracy with size obtain The cylindrical false boss 14 of guarantee, but in existing production technology, the false boss 14 is mainly used for follow-up machine and adds process Clamping and the purposes such as positioning, in existing measurement process, utilization physically is not carried out to the false boss 14 and (such as is pressed from both sides The purposes such as hold, position).
As shown in Figure 2 a, during existing Blade measuring, the foundation of the theoretical reference coordinate system of the blade 1 is usually adopted With following principle, (usually it is clamped in as shown in Figure 2 a described first with the roller 2 of the tenon tooth 13 of blade 1 described in held tight First pair of recessed portion of 13 apical tooth two sides of tenon tooth) Lai Jianli datum plane, that is, the axis according to theoretical two parallel rollers 2 Line establishes x-y plane, and the axis by the cylindrical false boss 14 of the blade 1 is z-axis, the friendship of z-axis and x-y plane Point is origin, and for x-axis by origin and parallel with the axis of roller 2, y-axis is vertical with x-axis.In the theoretical referring to seat of the blade 1 In mark system, z-axis is used to indicate positional relationship between the blade 11, the listrium 12 and the tenon tooth 13, usual situation its It is oriented to the direction that the blade 11 is directed toward by the tenon tooth 13, x-axis and y-axis are mainly for for indicating the tooth of the tenon tooth 13 Shape, therefore the direction of x-axis and y-axis can (such as the matching of the reference coordinate system in measurement process with measuring tool facilitates journey as needed Degree) it adjusts, that is to say, that the pointing direction of x-axis can be the direction that exhaust side is directed toward from blade leading edge, be also possible to On the contrary, the pointing direction of y-axis is also possible to opposite either from the direction of leaf basin side direction blade back side.
It is above-mentioned in measurement process during being measured using different measuring tools or for different types of blade Theoretical reference coordinate system can be translated according to the actual conditions of measuring tool, in other words, in order to which measuring instrument is convenient for reading, blade 1 theoretical reference coordinate system origin can mobile △ x, △ y, △ z on the direction of three reference axis respectively, so as to measurement The reference coordinate system of instrument is overlapped.Certainly, it will be appreciated by those skilled in the art that for the ease of measuring instrument operation, such as scheme Shown in 2b, 2c, the theoretical reference coordinate system of blade can also be rotated.
As previously mentioned, existing measurement process is to survey for the different turbo blades such as Fig. 1 a- Fig. 1 c Tenon tooth 13 is clamped using special measurement tooling when measuring the blade profile of the blade 11 (such as to be pressed from both sides on special vice with a pair of of roller 2 Firmly first pair of recessed portion of the apical tooth two sides of tenon tooth 13) expose blade profile, it is positioned with tenon tooth 13 to measure blade profile size;In measurement tenon When 13 locking tab 131 relative dimensions of slot of tooth, special measurement tooling is replaced, clamp most of tenon tooth 13 and will be revealed at the top of tenon tooth Out, to measure 131 relative dimensions of locking plate slot;When measuring 12 size of listrium, it may be desirable to according to the variation of measuring point Replacement covers special measurement tooling, clamps the exposing listrium 12 of tenon tooth 13 and is tested position, measures relative dimensions.
Above-mentioned existing measurement method, process very complicated, for example, clamping 2 clamping of roller using vice when measuring blade profile During, the horizontality of two rollers 2 can finally influence the precision for the blade profile data that measurement obtains, therefore operator It must the experienced efficiency that could ensure 2 process of clamping roller;And the special measurement for measuring listrium 12 and locking plate slot 131 Tooling clamps rear blade state if mounting groove gap is too big and is difficult to guarantee unanimously as shown in figs. 2 b and 2 c, can if gap is too small Blade is caused to be difficult to pack into, therefore mounting groove manufacture difficulty is big, precision is difficult to guarantee.And in order to avoid causing to damage to blade, Under normal conditions, the blade 1 can be less than for manufacturing the hardness of the material of special measurement tooling (especially installation groove location) The hardness of material therefore in use, also easily cause the abrasion of mounting groove, to cause change in size.
In measurement process, since each measuring point requires special tooling, cause to require each blade More set special toolings, so that production cost is high.In addition, tooling quantity also results in management difficulty more big, tooling Maintenance difficulties increase.And since all processes are all manual operationss, the clamping measurement process of each size is both needed to grasp Author has more skilled operation skill.
Existing measurement process operating efficiency is very low.For at least up to a hundred various blade essence castings of every batch of in actual production Part finished product, since every blade is both needed to measure, measurement process needs to expend the very long time, drags to can become One of an important factor for prolonging the entire production cycle.
Summary of the invention
A kind of method of integrated base the technical problem to be solved in the present invention is to provide manufacture for Blade measuring, with The problem of being formerly mentioned is reduced or avoided.
In order to solve the above technical problems, a kind of side of the integrated base the invention proposes manufacture for Blade measuring Method, manufactured by pedestal be used for the locking plate slot at the top of blade profile size, the size of listrium and tenon tooth to the blade of turbo blade Size measures, and the pedestal is the rectangular block around the tenon tooth formed of being cast by low-melting alloy, the locking plate Slot is not covered by low-melting alloy, and the turbo blade has a theoretical reference coordinate system, the z of the theoretical reference coordinate system Axis is overlapped with the axis of the false boss of the blade, and the x-y plane of the theoretical reference coordinate system can be by can be to the tenon Two standard rollers that first pair of recessed portion of the apical tooth two sides of tooth is clamped are established in two axis of clamp position, z Axis and the intersection point of x-y plane are origin, and for x-axis by origin and parallel with the axis of the roller, y-axis is vertical with x-axis.The square Shape block includes the first side elevation, the second side elevation, third side elevation and the 4th side elevation being linked in sequence, first side elevation And/or the third side elevation is parallel with the x-axis of the theoretical reference coordinate system, second side elevation and/or the described 4th Side elevation is parallel with the y-axis of the theoretical reference coordinate system, and the rectangular block further includes the z-axis with the theoretical reference coordinate system The vertical first level face close to the locking plate slot comprising following steps:
Step A, constructs a casting type chamber, and the casting type chamber includes at least one for forming the first level face Horizontal type face and vertical with the horizontal type face at least two orthogonal contoured sidewalls that are linked in sequence, will be described Blade vertical lifting is above the casting type chamber, so that the listrium is above the casting type chamber, the tenon tooth is described Casting type is intracavitary, and the z-axis of the theoretical reference coordinate system of the blade is vertical with the horizontal type face, and x-axis and y-axis are respectively and mutually The vertical contoured sidewall is parallel.
Step B forms the blank of the rectangular block in the intracavitary casting low-melting alloy of the casting type of step A.
Step C carries out local heat treatment for the blank of the rectangular block manufactured by step B, melts elimination covering The alloy structure of the locking plate slot, so that the locking plate slot is completely exposed.Complete the manufacture of the rectangular block.
Preferably, in step, the casting type chamber is a T-type cavity, the T-type face of the casting type chamber be for Form the horizontal type face in the first level face.
Preferably, in step, the casting type chamber is rectangular cavities, and the bottom surface of the casting type chamber is for forming The horizontal type face in the first level face.
Preferably, in step, at least one side of the casting type chamber is formed by dismountable flapper.
Preferably, in step, at least one side of the casting type chamber is the inclined-plane being inclined outwardly.
Preferably, in step C, the rectangular block is immersed into hot oil, makes the rectangular block for being wrapped in the locking plate slot Partial ablation.
Preferably, in step C, hot oil is sprayed to the alloy for covering the lock runner region, keeps the locking plate slot complete Expose.
The method of integrated base of a kind of manufacture provided by the present invention for Blade measuring, by providing mark for blade The pedestal of standardization, substantially reduces the measurement duration of blade, and effectively reduces production cost and maintenance cost.
Detailed description of the invention
The following drawings are only intended to schematically illustrate and explain the present invention, not delimit the scope of the invention.Wherein,
Fig. 1 a is a kind of stereochemical structure schematic illustration of Turbine Blade;
Fig. 1 b is a kind of stereochemical structure schematic illustration of second turbine blade;
Fig. 1 c is a kind of stereochemical structure schematic illustration of free turbine blade;
Fig. 2 a is the schematic illustration that blade profile dimensional measurement is carried out to the Turbine Blade of Fig. 1 a;
Fig. 2 b is the schematic illustration that listrium dimensional measurement is carried out to the Turbine Blade of Fig. 1 a;
Fig. 2 c is the schematic illustration that the slot dimensional measurement of tenon tooth locking tab is carried out to the Turbine Blade of Fig. 1 a;
Fig. 3 a is the integrated base that Blade measuring is used for using a kind of manufacture of a specific embodiment according to the present invention The turbo blade of pedestal made by the method for seat carries out the schematic illustration of blade profile dimensional measurement;
Fig. 3 b is the schematic illustration that listrium dimensional measurement is carried out to the turbo blade of Fig. 3 a;
Fig. 3 c is the schematic illustration that the slot dimensional measurement of tenon tooth locking tab is carried out to the turbo blade of Fig. 3 a;
Fig. 4 a is a kind of broken section principle schematic diagram of the casting equipment of pedestal for being used to prepare Fig. 3 a;
Fig. 4 b is the overlooking state partial cross principle schematic diagram of the casting equipment of Fig. 4 a;
Fig. 5 is the broken section structure of the dissolution shaping device of rectangular block manufactured by casting equipment for shaping Fig. 4 a Schematic illustration;
The stereochemical structure schematic illustration for dissolution shaping device treated the rectangular block that Fig. 6 is Fig. 5.
Specific embodiment
For a clearer understanding of the technical characteristics, objects and effects of the present invention, this hair of Detailed description of the invention is now compareed Bright specific embodiment.Wherein, identical component uses identical label.
Fig. 1 a is a kind of stereochemical structure schematic illustration of Turbine Blade;Fig. 2 a is the Turbine Blade to Fig. 1 a Carry out the schematic illustration of blade profile dimensional measurement;Fig. 3 a is to be used using a kind of manufacture of a specific embodiment according to the present invention The turbo blade of the pedestal made by the method for the integrated base of Blade measuring carries out the principle signal of blade profile dimensional measurement Figure;Fig. 3 b is the schematic illustration that listrium dimensional measurement is carried out to the turbo blade of Fig. 3 a;Fig. 3 c is the turbo blade to Fig. 3 a Carry out the schematic illustration of tenon tooth locking tab slot dimensional measurement;Fig. 4 a is a kind of casting equipment of pedestal for being used to prepare Fig. 3 a Broken section principle schematic diagram;Fig. 4 b is the overlooking state partial cross structural principle signal of the casting equipment of Fig. 4 a Figure;Fig. 5 is the broken section structural principle of the dissolution shaping device of rectangular block manufactured by casting equipment for shaping Fig. 4 a Schematic diagram;The stereochemical structure schematic illustration for dissolution shaping device treated the rectangular block that Fig. 6 is Fig. 5.Referring to Fig. 1 a, 2a, Shown in 3a-6, the present invention provides it is a kind of manufacture for Blade measuring integrated base method, made by pedestal use 131 size of locking plate slot in 13 top of the blade profile size of the blade 11 to turbo blade 1, the size of listrium 12 and tenon tooth is surveyed Amount, the pedestal are the rectangular block 3 around the tenon tooth 13 formed of being cast by low-melting alloy, and the locking plate slot 131 is not It is covered by low-melting alloy, exposes the rectangular block 3, the turbo blade 1 has a theoretical reference coordinate system, the reason It is overlapped by the z-axis of reference frame with the axis of the false boss 14 of the blade 1, the x-y of the theoretical reference coordinate system is flat Face can be by that can clamp shape to two standard rollers 2 that first pair of recessed portion of the apical tooth two sides of the tenon tooth 13 is clamped Two axis of state are established, and the intersection point of z-axis and x-y plane is origin, and x-axis is by origin and flat with the axis of the roller 2 Row, y-axis are vertical with x-axis.The rectangular block 3 includes the first side elevation being linked in sequence, the second side elevation, third side elevation and the Four side elevations, first side elevation and/or the third side elevation are parallel with the x-axis of the theoretical reference coordinate system, described Second side elevation and/or the 4th side elevation are parallel with the y-axis of the theoretical reference coordinate system, and the rectangular block 3 further includes The first level face 31 close to the locking plate slot 131 vertical with the z-axis of the theoretical reference coordinate system, the top of the rectangular block Face and the minimum range of the listrium 12 in the z-axis direction are not less than 2mm.
Since low-melting alloy has good hardness and strength, the present invention using low-melting alloy by being cast Mode, form the rectangular block 3 around the tenon tooth 13, low-melting alloy, can be to the tenon tooth after cooling and solidifying sizing 13 shrink, to form the firm double team to the tenon tooth 13 using the tooth form of the tenon tooth 13.
The manufacturing method of the rectangular block 3 may include steps of:
Step A, constructs a casting type chamber, and the casting type chamber includes at least one for forming the first level face The orthogonal contoured sidewall of 31 horizontal type face and at least two sequential connections vertical with the horizontal type face, by institute 1 vertical lifting of blade is stated above the casting type chamber, so that the listrium 12 is above the casting type chamber, the tenon tooth 13 Intracavitary in the casting type, the z-axis of the theoretical reference coordinate system of the blade 1 is vertical with the horizontal type face, x-axis and y-axis point It is not parallel with the orthogonal contoured sidewall.
When needing to manufacture the rectangular block 3, casting equipment 4 as shown in figures 4 a and 4b can be used, the casting is set Standby 4 include that casting pedestal 41, positioning templet 42 and mold cavity 43, the casting pedestal 41 are connected with liftable first boom 411, bearing is installed on first boom 411, the fixed device 44 of the first false boss has been rotatably connected by bearing, it will The insertion of the false boss 14 of the blade 1 to be measured is mounted in the fixed device 44 of first false boss, then is passed through Screw locks the blade 1 in the fixed device 44 of first false boss, so that the blade 1 is lifted on described first and hangs It, thus can be by the institute of the blade 1 by adjusting locking first boom 411 in the position of vertical direction on arm 411 The direction for stating the x, y, z axis of theoretical reference coordinate system is fixed up, but the blade 1 (that is to say the theoretical reference coordinate system) It can be rotated on first boom 411.Then, the tested corresponding positioning templet 42 of the blade 1 is mounted on institute It states on casting pedestal 41, in this manner it is possible to by the fitting of the positioning templet 42 and the listrium 12 of the blade 1, Gu The angular of the blade 1 is determined, so that all freedom degrees of the blade 1 are fixed.
The fixed device 44 of first false boss is provided with the jack that (clearance fit) is matched with the false boss 14, And fixing screws are connected in jack, thus can by the false boss 14 is inserted into the jack and tighten screw come Connection relationship between the fixed blade 1 and the fixed device of first false boss.By the false boss 14 of the blade 1 It is mounted on the fixed device 44 of first false boss, also allows for the theoretical reference coordinate system of the blade 1 in this way X, y, z direction is fixed, irremovable, but can rotate along bearing centre.For different types of turbo blade, can correspond to every The kind blade 1 manufactures a dedicated positioning templet 42, and as shown in Fig. 4 a, 4b, the positioning templet 42 can be by tight Gu screw is fixedly connected with the casting pedestal 41, by the auxiliary positioning of the positioning templet 42, can ensure and the work The blade 1 that skill boss clamp device 44 connects, which can be stablized, rests on the mold cavity 43, and can ensure the blade 1 The theoretical reference coordinate system is parallel with the coordinate system where the side wall of the mold cavity 43.Namely make the mold cavity 43 Side wall facing each other it is parallel with the x-axis of the theoretical reference coordinate system and y-axis respectively, when replacing the different types of leaf When piece 1, fastening screw only need to be unclamped, removing and replacing the corresponding positioning templet 42 can be realized to different types of described The positioning of blade 1.
In Fig. 4 a and Fig. 4 b, a global facility is shown in the mold cavity 43, but those skilled in the art should Understand, as a casting mold cavity, removes the rectangular block 3 after casting for convenience, the mold cavity 43 can be made at least One side is formed by dismountable flapper, it is of course also possible to be make at least one side of the mold cavity 43 to The inclined-plane of outer incline.
The mold cavity 43 can a T-type cavity as shown in Figure 4 a, in this way, the T-type face 431 of the mold cavity 43 As the horizontal type face for forming the first level face 31, since casting process can the fully wrapped around covering top of tenon tooth 13 The locking plate slot 131 in portion, therefore, the mold cavity 43 use T-type cavity, then can avoid the 431 molding institute, institute of T-type face First level face 31 is stated in subsequent extra low-melting alloy structure removal process, will not be destroyed, and can be used as reference plane Convenient for successor operation.
Certain mold cavity 43 can also be a common rectangular cavities, that is to say, that can be by the mold cavity 43 bottom surface is as horizontal type face, as long as the locking plate slot 131 can be exposed during subsequent processes.
The side wall and adjacent side wall of the mold cavity 3 where the positioning templet 42 can be used as the molding side Wall, for ensureing x-axis that at least two side walls of the rectangular block 3 can respectively with the theoretical reference coordinate system of the blade 1 It is parallel with y-axis.
Step B forms the blank of the rectangular block 3 in the intracavitary casting low-melting alloy of the casting type of step A.
Such as in casting equipment 4 as shown in figures 4 a and 4b, after the blade 1 is in place, it can be poured described It is poured low-melting alloy in mold cavity 43, is stained with cold water brush on low-melting alloy using hairbrush after casting, waits 5 seconds or so, to low Melting alloy cooled and solidified unclamps the screw of the fixed device 44 of the false boss, when at least one side of the mold cavity 43 When face is formed by dismountable flapper, the flapper of the mold cavity 43 is removed, lifts the boom 411, so that it may Take out the blade 1 for being provided with the rectangular block 3.When at least one side of the mold cavity 43 be inclined outwardly it is oblique Face.It then can directly lift the boom 411, so that it may take out the blade 1 for being provided with the rectangular block 3.
Step C carries out local heat treatment, melts elimination and cover for the blank of the rectangular block 3 manufactured by step B The alloy structure of the locking plate slot 131 is covered, so that the locking plate slot 131 is completely exposed.Complete the system of the rectangular block 3 It makes.
The blade 1 with the rectangular block 3 prepared by the equipment 4, since the rectangular block 3 has wrapped up entirely Tenon tooth 13 described in portion, therefore be not met by the needs of entire measurement process, if the rectangular block 3 cast by T-type cavity and At the first level face 31 is formed by the T-type face 431, then can make to be wrapped in by the way that the rectangular block 3 is immersed hot oil The partial ablation of the rectangular block 3 of the locking plate slot 131, that is, correspond to 431 lower section of the T-type face of the mold cavity 43 T-type extended end portion sub-dip enter hot oil so that the low-melting alloy of the part melts, expose the locking plate slot 131.Immerse heat The process of oil can ensure described only it is required that the molding first level face 31 of the institute of the T-type face 431 is not contacted with hot oil First level face 31 it is complete, as long as that is, can ensure that positioning is played in subsequent measurement process in the first level face 31 Effect.
If the rectangular block 3 is cast by rectangular cavities, that is to say, that the bottom surface of the rectangular block 3 is described the One horizontal plane 31 then can only be removed the alloy structure of 131 position of locking plate slot, keep described the first of other positions Horizontal plane 31 is not ablated to, for example, with reference to shown in Fig. 5 and Fig. 6, it is possible to provide a dissolution shaping device 5, the dissolution are whole Shape equipment 5 includes shaping pedestal 51, and the shaping pedestal 51 is connected with liftable second boom 511, second boom 511 It has been rotatably connected the second false boss clamp device 54, the false boss 14 of the blade 1 to be measured is inserted into installation In the fixed device 54 of second false boss, then the blade 1 is locked by screw and is consolidated in second false boss Determine in device 54, be lifted on the blade 1 on second boom 511, the shaping pedestal 51 is provided with working chamber 52, institute It states working chamber 52 to be arranged below second boom 511, the side wall of the working chamber 52 is provided with described at least one direction The hot oil spray head 521 of 52 middle and upper part of working chamber, 52 bottom of working chamber are provided with an oil outlet, the hot oil spray head 521 Pass through pipeline with the oil outlet to connect with a hot-oil circulation processing equipment 6, when 521 oil spout of hot oil spray head, hot oil The highest point of running track is no more than 52 top surface of working chamber, is lifted on second boom 511 it in the blade 1 Afterwards, second boom 511 is fallen, the position of the blade 1 is adjusted, so that the rectangular block 3 is entered the working chamber 52, and protect Hinder 131 region of locking plate slot in the hot oil running track in 521 oil spout of hot oil spray head, opens at the hot-oil circulation Equipment 6 is managed, so that the hot oil spray head 521 is started the hot oil that injection temperation is not less than 180 DEG C, the blade 1 is then rotated, wait cover The alloy in 131 region of locking plate slot is covered by after hot oil melts, second boom 511 is risen, removes the blade 1, complete Preparation to the rectangular block 3.
When due to being measured to the locking plate slot 131, the equipment such as three-coordinates measuring machine can be used and pass through gauge head and type face It contacts to measure, therefore namely it is meant that being formed by the blank of the rectangular block 3 for step B, it is only necessary to by institute Measurement needs can be met by stating locking plate slot 131 and completely exposing, rather than must the apical tooth (the first tooth) of entire tenon tooth will reveal Therefore alloy block out by pre-setting the Hot Oil Spray track of the hot oil spray head 521, and controls the position of the blade 1 It sets, that is, the hot oil that may make the hot oil spray head 521 to be sprayed only is sprayed in the alloy for covering 131 region of locking plate slot On, to will not cause to melt to the alloy of other parts.Dissolution shaping device treated the rectangular block that Fig. 6 is Fig. 5 is stood Body principle schematic diagram, Fig. 6 is mainly used for the type face variation after illustrating rectangular block to be removed alloy part, therefore does not draw in figure Blade out, it is shown in Figure 6, using dissolution shaping device 5 provided by the present invention, although 3 bottom of the rectangular block is gone The alloy component removed is not regular shape, but as long as the locking plate slot 131 can be made all to be exposed and can meet The needs of measurement.The demand to hot oil can be thus substantially reduced, to reduce energy consumption, reduces cost, and can ensure The first level face 31 it is complete.
As shown in figure 5,52 bottom surface of working chamber may be configured as inclined-plane, be conducive to fall in the working chamber 52 in this way Hot oil collect recycling from the oil outlet, the hot-oil circulation processing equipment 6 may include the cooling tank that is linked in sequence (in figure Not depending on out) and heater (not regarded out in figure), team is in Chinese patent where specific structure can refer to inventor Cooling tank and heater employed in a kind of blade inner cavity low-melting alloy removal device provided by 201611189008.2 Structure, details are not described herein.By the hot-oil circulation processing equipment 6, the heat that the hot oil spray head 521 is sprayed can be ensured Oil temperature, and the low-melting alloy for being dissolved into hot oil can be recycled in time.
After the blade 1, which is lifted on second false boss, fixes device 54, the z-axis position of the blade 1 is just It is fixed on second boom 511, therefore, by controlling the lifting of second boom 511, i.e., more accurately controls institute The position of blade 1 is stated, that is, can control the position of the rectangular block 3.
The fixed device 54 of second false boss can be rotatably connected by bearing and second boom 511, this Sample can rotate the blade 1 manually, enable and cover the alloy in 131 region of locking plate slot by the removal of noresidue, in order to Preferably control the rotation of the blade 1, the fixed device 54 of second false boss with the axis on second boom 511 It holds after being fixedly connected, may be provided with the bar portion 541 for extending 511 top surface of the second boom, it in this way can be by extending Bar portion 541 is arranged the structures such as belt, gear and connect with motor 7, described so as to more accurately control the revolving speed of the blade 1 The revolving speed of blade 1 can be controlled in 10-20 revs/min.
When the hot oil spray head 521 only one when, probably needing to spray can to coat the locking plate for 8-10 minutes The alloy of slot 131 all dissolves.The hot oil spray head 521 can be arranged multiple such as arranged symmetrically in the working chamber 52 Two or four, or two are arranged in adjacent two side walls, the time that need to be sprayed can be reduced in this way, promote shaping effect Rate.But the complexity that also will increase the structure of the shaping pedestal 51 in this way, to cause cost increase.
Due to first side elevation of the rectangular block 3 and/or the third side elevation and the theoretical reference coordinate The x-axis of system is parallel, and second side elevation and/or the 4th side elevation are parallel with the y-axis of the theoretical reference coordinate system, institute It is vertical with the z-axis of the theoretical reference coordinate system to state first level face 31, that is, the first level face 31 and the x-y are put down Face is parallel, therefore, by the limit of the outer surface to the rectangular block 3, can limit the reference frame of the blade 1, and The theoretical reference coordinate system of the blade 1 can be made parallel with the reference coordinate system of measuring instrument, easily so as to very square It will pass through and the blade 1 is determined using the similar fixture that can be limited at least three faces in each measuring phases Position is fixed, and the reference coordinate system that also can very easily adjust measuring instrument is overlapped with the theoretical reference coordinate system of the blade 1, Also it can simplify the measurement tooling of each measurement process and the structure of measuring tool.And promote measurement efficiency.
First side elevation and/or the third side elevation of the rectangular block 3 and second side elevation and/or 4th side elevation is mainly used for clamping position, can be by determining the false boss 14 in subsequent measurement process Therefore position only needs not lean on too close with the listrium 12, has a spacing to control the reference frame of the blade 1 From (such as minimum range is not less than 5mm, maximum distance is not more than 30mm, apart from excessive, be easy to cause 3 volume of rectangular block It is larger, waste the energy consumption of manufacturing process), therefore, in step, when fixing the blade 1 to be measured, it need to only keep institute The side wall for stating listrium 12 and the mold cavity 43 has certain distance, certainly, by the way that the positioning templet 42 is arranged, can make The coordinate system of the rectangular block 3 cast of blade 1 described in same type is stablized, consequently facilitating subsequent mass standardize into Row measurement.
The top surface of the rectangular block 3 and the minimum range of the listrium 12 in the z-axis direction are greater than 2mm, can ensure in this way The space needs that the size of the listrium 12 is measured.
If the rectangular block 3 is cast by T-type cavity, the first level face 31 is formed by the T-type face 431, The first level face 31 can be then set to be greater than 1.5mm with the minimum range of the locking plate slot 131 in the z-axis direction.In this way Enough measurement spaces are reserved for the locking plate slot 131.
If the rectangular block 3 is cast by rectangular cavities, that is to say, that the bottom surface of the rectangular block 3 is described the One horizontal plane 31 then need to only ensure that the locking plate slot 131 is completely exposed the rectangular block 3, that is to say the locking plate slot 131 not by Alloy structure covering.
In practice, 3 kinds of turbo blades of Mr. Yu's h type engine h may make and measured when using method of the invention The measurement tooling of journey and the structure of measuring tool are also greatly simplified, so that the time of replacement measuring tool be greatly decreased, are relatively carried on the back Original process method described in scape technology can shorten for about 50% or so time on the duration.Moreover, because reducing measurement work Dress, greatly reduces production cost, 60% or so frock cost can be usually reduced compared with former measurement method described in background technique. It, can as being that plane as the side elevation and horizontal plane to the rectangular block 3 carries out positioning clamping in measurement process It avoids positioning using high-precision loose piece as stated in the background art, while reducing tooling manufacturing cost, also reduces tooling Maintenance difficulties.
The method of integrated base of a kind of manufacture provided by the present invention for Blade measuring, by providing mark for blade The pedestal of standardization, substantially reduces the measurement duration of blade, and effectively reduces production cost and maintenance cost.
It will be appreciated by those skilled in the art that although the present invention is described in the way of multiple embodiments, It is that not each embodiment only contains an independent technical solution.So narration is used for the purpose of for the sake of understanding in specification, The skilled in the art should refer to the specification as a whole is understood, and by technical solution involved in each embodiment Regard as and can be combined with each other into the modes of different embodiments to understand protection scope of the present invention.
The foregoing is merely the schematical specific embodiment of the present invention, the range being not intended to limit the invention.It is any Those skilled in the art, made equivalent variations, modification and combination under the premise of not departing from design and the principle of the present invention, It should belong to the scope of protection of the invention.

Claims (7)

1. a kind of method of integrated base of manufacture for Blade measuring, manufactured by pedestal be used for the leaf of turbo blade Locking plate slot size at the top of the blade profile size of body, the size of listrium and tenon tooth measures, and the pedestal is by low-melting alloy The rectangular block around the tenon tooth that casting is formed, the locking plate slot are not covered by low-melting alloy, the turbo blade tool There is a theoretical reference coordinate system, the z-axis of the theoretical reference coordinate system is overlapped with the axis of the false boss of the blade, institute State what the x-y plane of theoretical reference coordinate system can be clamped by first pair of recessed portion for capableing of apical tooth two sides to the tenon tooth Two standard rollers are established in two axis of clamp position, and the intersection point of z-axis and x-y plane is origin, x-axis by origin and Parallel with the axis of the roller, y-axis is vertical with x-axis.The rectangular block includes the first side elevation being linked in sequence, second edge-on Face, third side elevation and the 4th side elevation, first side elevation and/or the third side elevation and the theoretical reference coordinate The x-axis of system is parallel, and second side elevation and/or the 4th side elevation are parallel with the y-axis of the theoretical reference coordinate system, institute Stating rectangular block further includes the first level face close to the locking plate slot vertical with the z-axis of the theoretical reference coordinate system, packet Include following steps:
Step A, constructs a casting type chamber, and the casting type chamber includes the water that at least one is used to form the first level face The orthogonal contoured sidewall of flat pattern face and at least two sequential connections vertical with the horizontal type face, by the blade Vertical lifting is above the casting type chamber, so that the listrium is above the casting type chamber, the tenon tooth is in the casting Type is intracavitary, and the z-axis of the theoretical reference coordinate system of the blade is vertical with the horizontal type face, x-axis and y-axis respectively be mutually perpendicular to The contoured sidewall it is parallel.
Step B forms the blank of the rectangular block in the intracavitary casting low-melting alloy of the casting type of step A.
Step C carries out local heat treatment for the blank of the rectangular block manufactured by step B, melts described in elimination covering The alloy structure of locking plate slot, so that the locking plate slot is completely exposed.Complete the manufacture of the rectangular block.
2. the casting type chamber is a T-type cavity the method according to claim 1, wherein in step, The T-type face of the casting type chamber is the horizontal type face for forming the first level face.
3. the method according to claim 1, wherein in step, the casting type chamber is rectangular cavities, institute The bottom surface of casting type chamber is stated as the horizontal type face for forming the first level face.
4. the method according to claim 1, wherein in step, at least one side of the casting type chamber It is formed by dismountable flapper.
5. the method according to claim 1, wherein in step, at least one side of the casting type chamber For the inclined-plane being inclined outwardly.
6. according to the method described in claim 2, it is characterized in that, the rectangular block being immersed hot oil, makes to wrap in step C Wrap up in the partial ablation of the rectangular block of the locking plate slot.
7. according to the method described in claim 3, it is characterized in that, in step C, to the alloy for covering the lock runner region Hot oil is sprayed, exposes the locking plate slot completely.
CN201811497600.8A 2018-12-07 2018-12-07 Method for manufacturing integrated base for blade measurement Active CN109434396B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811497600.8A CN109434396B (en) 2018-12-07 2018-12-07 Method for manufacturing integrated base for blade measurement

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811497600.8A CN109434396B (en) 2018-12-07 2018-12-07 Method for manufacturing integrated base for blade measurement

Publications (2)

Publication Number Publication Date
CN109434396A true CN109434396A (en) 2019-03-08
CN109434396B CN109434396B (en) 2020-09-11

Family

ID=65557062

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201811497600.8A Active CN109434396B (en) 2018-12-07 2018-12-07 Method for manufacturing integrated base for blade measurement

Country Status (1)

Country Link
CN (1) CN109434396B (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011015192A1 (en) * 2009-08-06 2011-02-10 Mtu Aero Engines Gmbh Repair of turbine components and solder alloy therefor
CN202304719U (en) * 2011-10-20 2012-07-04 常州市三维技术成套设备有限公司 Arc fir tree blade root measuring device
CN105436838A (en) * 2015-11-05 2016-03-30 西安航空动力股份有限公司 Machining method for turbine work blade
CN106767237A (en) * 2016-11-23 2017-05-31 沈阳黎明航空发动机(集团)有限责任公司 A kind of processing method for controlling moving turbine blade tenon tooth wall thickness
CN107984340A (en) * 2017-12-01 2018-05-04 中国航发沈阳黎明航空发动机有限责任公司 Reference Transforming fixture and application method before a kind of essence casting blade tenon tooth processing

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011015192A1 (en) * 2009-08-06 2011-02-10 Mtu Aero Engines Gmbh Repair of turbine components and solder alloy therefor
CN202304719U (en) * 2011-10-20 2012-07-04 常州市三维技术成套设备有限公司 Arc fir tree blade root measuring device
CN105436838A (en) * 2015-11-05 2016-03-30 西安航空动力股份有限公司 Machining method for turbine work blade
CN106767237A (en) * 2016-11-23 2017-05-31 沈阳黎明航空发动机(集团)有限责任公司 A kind of processing method for controlling moving turbine blade tenon tooth wall thickness
CN107984340A (en) * 2017-12-01 2018-05-04 中国航发沈阳黎明航空发动机有限责任公司 Reference Transforming fixture and application method before a kind of essence casting blade tenon tooth processing

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
申秀丽等: "《"航空燃气涡轮发动机典型制造工艺》", 30 June 2016 *

Also Published As

Publication number Publication date
CN109434396B (en) 2020-09-11

Similar Documents

Publication Publication Date Title
CN107717364B (en) The cold and hot composite manufacturing method of hollow turbine vane inner cavity hot investment casting shape machining
CN1693014B (en) Method and apparatus for determining the location of core-generated features in an investment casting
US9205522B2 (en) Equipment comprising a rotatable cradle and intended for encasing the airfoil of a turbine blade in order to machine the root
CN109458901A (en) A kind of blade subsidiary pedestal manufacturing device
CN105983658B (en) A kind of Ti3The preparation method of Al alloys guide vane inner ring model for precision casting and formwork
CN109483172A (en) A kind of turbo blade positioning pedestal manufacturing method
CN109317936A (en) A kind of Blade measuring pedestal preparation method
CN109458900A (en) A kind of blade subsidiary pedestal manufacturing method
CN109332652A (en) A kind of blade positioning base manufacturing device
CN109434396A (en) A method of manufacture is used for the integrated base of Blade measuring
CN109443146A (en) A kind of integrated base for Blade measuring
CN109465405A (en) A kind of Blade roughcast measuring block manufacturing method
CN109405699A (en) A kind of Blade roughcast measuring block manufacturing device
CN109332654A (en) A kind of blade of aviation engine pedestal preparation facilities
CN109622923A (en) A kind of blade of aviation engine pedestal preparation method
CN109465606A (en) A kind of preparation method of the pedestal for Blade measuring
CN109332653A (en) A kind of blade positioning base manufacturing method
CN109317981A (en) A kind of preparation facilities of the pedestal for Blade measuring
CN109357599B (en) Integral machining measuring device and method for intermediary case wax mold
CN109530626A (en) A kind of turbo blade pedestal preparation method
CN109397141A (en) A kind of turbo blade pedestal preparation facilities
CN109373949A (en) A kind of turbo blade positioning pedestal manufacturing device
CN114799383B (en) Method and device for trimming casting flange plate of single crystal turbine blade and single crystal turbine blade
CN109317980A (en) A kind of Blade measuring pedestal preparation facilities
CN114425605B (en) Preparation method of titanium and titanium alloy casting containing special-shaped inner cavity

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant