CN109332652A - A kind of blade positioning base manufacturing device - Google Patents
A kind of blade positioning base manufacturing device Download PDFInfo
- Publication number
- CN109332652A CN109332652A CN201811495918.2A CN201811495918A CN109332652A CN 109332652 A CN109332652 A CN 109332652A CN 201811495918 A CN201811495918 A CN 201811495918A CN 109332652 A CN109332652 A CN 109332652A
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- China
- Prior art keywords
- blade
- axis
- casting
- pedestal
- rectangular block
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D19/00—Casting in, on, or around objects which form part of the product
- B22D19/009—Casting in, on, or around objects which form part of the product for casting objects the members of which can be separated afterwards
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B21/00—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B21/00—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant
- G01B21/20—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant for measuring contours or curvatures, e.g. determining profile
Abstract
A kind of blade positioning base manufacturing device comprising the casting equipment of a blank for the rectangular block of casting and a dissolution shaping device for the blank progress shaping to the rectangular block.The casting equipment includes casting pedestal, positioning templet and mold cavity, the mold cavity is formed by the casting pedestal and with the movable side wall of the casting movable connection of pedestal, the T-type face of the side wall of the casting pedestal where first boom is provided with the first preformed groove, the movable side wall corresponds to first preformed groove and is provided with the second preformed groove, by first preformed groove and second preformed groove, it is provided with " mouth " type posting.A kind of blade positioning base manufacturing device provided by the present invention is substantially shorter the measurement duration of blade, while can reduce production cost and maintenance cost by preparing standardized base.
Description
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 device of the pedestal positioned when being measured for manufacturing 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) establish datum plane, that is, according to the axis of 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
The technical problem to be solved in the present invention is to provide a kind of blade positioning base manufacturing devices, front is reduced or avoided
The problem of being previously mentioned.
In order to solve the above technical problems, the invention proposes a kind of blade positioning base manufacturing device, supplemented by the pedestal
The locking plate slot size at the top of blade profile size, the size of listrium and tenon tooth to the blade of turbo blade is helped to measure, by eutectic
The rectangular block around the tenon tooth that point alloy casting is formed, the locking plate slot are not covered by low-melting alloy, the turbine
Blade has a theoretical reference coordinate system, the axis of the false boss of the z-axis and blade of the theoretical reference coordinate system
Be overlapped, the x-y plane of the theoretical reference coordinate system can by be capable of first pair of recessed portion of apical tooth two sides to the tenon tooth into
Two standard rollers of row clamping are established in two axis of clamp position, and the intersection point of z-axis and x-y plane is origin, and x-axis is logical
Origin and parallel with the axis of the roller is crossed, y-axis is vertical with x-axis.The rectangular block include be linked in sequence the first side elevation,
Second side elevation, third side elevation and the 4th side elevation, first side elevation and/or the third side elevation and the theory
The x-axis of reference frame is parallel, the y of second side elevation and/or the 4th side elevation and the theoretical reference coordinate system
Axis is parallel, and the rectangular block further includes first water close to the locking plate slot vertical with the z-axis of the theoretical reference coordinate system
Plane, the top surface of the rectangular block and the minimum range of the listrium in the z-axis direction are not less than 2mm.It includes one and is used for
Cast the rectangular block blank casting equipment and one for carrying out the dissolution shaping of shaping to the blank of the rectangular block
Equipment,
The casting equipment includes that casting pedestal, positioning templet and mold cavity, the casting pedestal are connected with liftable
The first boom, bearing is installed on first boom, the fixed device of the first false boss has been rotatably connected by bearing,
The mold cavity be a T-type cavity, the mold cavity by the casting pedestal and with the movable connection of the casting pedestal
Movable side wall formed, the T-type face of the side wall of the casting pedestal where first boom is provided with the first preformed groove, institute
State movable side wall and correspond to first preformed groove and be provided with the second preformed groove, the movable side wall be provided with it is described second reserved
The corresponding briquetting being detachably connected of slot is provided with " mouth " type by first preformed groove and second preformed groove
Posting.
The dissolution shaping device includes shaping pedestal, and the shaping pedestal is connected with liftable second boom, described
Second boom is provided with the second false boss clamp device, and the shaping pedestal is provided with hot oil chamber, and the hot oil chamber setting exists
Below second boom, the intracavitary hot oil for being injected with temperature and being not less than 180 DEG C of the hot oil, the top surface of the hot oil chamber is extremely
Size on a few direction is less than the size of the x-axis direction of the rectangular block.
Preferably, at least one side of the mold cavity is formed by dismountable flapper.
Preferably, at least one side of the mold cavity is the inclined-plane being inclined outwardly.
Preferably, the T-type face of the mold cavity is the horizontal type face for forming the first level face.
Preferably, the posting is made of the metal plate of 3mm thickness.
Preferably, the posting is made of the resin plate of 3-4mm thickness.
Blade positioning base manufacturing device provided by the present invention is substantially shorter blade by preparing standardized base
The measurement duration, while can reduce 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 will be manufactured by a kind of blade positioning base manufacturing device of a specific embodiment according to the present invention
Schematic illustration of the pedestal for the blade profile dimensional measurement of turbo blade；
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. 4 c is the part isometric decomposition texture schematic illustration of the casting equipment of Fig. 4 a；
Fig. 4 d is the stereochemical structure schematic illustration of rectangular block manufactured by the casting equipment of Fig. 4 c；
Fig. 5 is the broken section principle schematic diagram of the dissolution shaping device for shaping Fig. 4 a rectangular block prepared.
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 position a kind of blade of a specific embodiment according to the present invention
Schematic illustration of the pedestal manufactured by pedestal manufacturing device for the blade profile dimensional measurement of turbo blade；Fig. 3 b is to Fig. 3 a's
The schematic illustration of turbo blade progress listrium dimensional measurement；Fig. 3 c is to carry out tenon tooth locking tab slot to the turbo blade of Fig. 3 a
The schematic illustration of dimensional measurement；Fig. 4 a is a kind of broken section structural principle of the casting equipment of pedestal for being used to prepare Fig. 3 a
Schematic diagram；Fig. 4 b is the overlooking state partial cross principle schematic diagram of the casting equipment of Fig. 4 a；Fig. 4 c is the casting of Fig. 4 a
The part isometric decomposition texture schematic illustration of equipment；Fig. 4 d is the stereochemical structure of rectangular block manufactured by the casting equipment of Fig. 4 c
Schematic illustration；Fig. 5 is the broken section structural principle signal of the dissolution shaping device for shaping Fig. 4 a rectangular block prepared
Figure.Referring to shown in Fig. 1 a, 2a, 3a-5, the present invention provides a kind of blade positioning base manufacturing device, the pedestal is auxiliary pair
131 size of locking plate slot at 13 top of the blade profile size of the blade 11 of turbo blade 1, the size of listrium 12 and tenon tooth measures,
It is cast by low-melting alloy the rectangular block 3 around the tenon tooth 13 formed, the locking plate slot 131 do not hide by low-melting alloy
Lid exposes the rectangular block 3, and the turbo blade 1 has a theoretical reference coordinate system, the theoretical reference coordinate system
Z-axis is overlapped with the axis of the false boss 14 of the blade 1, and the x-y plane of the theoretical reference coordinate system can be by can be to institute
Two standard rollers 2 that first pair of recessed portion of the apical tooth two sides of tenon tooth 13 is clamped are stated to come in two axis of clamp position
It establishes, the intersection point of z-axis and x-y plane is origin, and x-axis by origin and parallel with the axis of the roller 2, hang down by y-axis and x-axis
Directly.The rectangular block 3 includes the first side elevation, the second side elevation, third side elevation and the 4th side elevation being linked in sequence, described
First side elevation and/or the third side elevation are parallel with the x-axis of the theoretical reference coordinate system, second side elevation and/
Or the 4th side elevation is parallel with the y-axis of the theoretical reference coordinate system, the rectangular block 3 further includes and the theoretical reference
The vertical first level face 31 close to the locking plate slot 131 of the z-axis of coordinate system, the top surface of the rectangular block and the listrium 12
Minimum range in the z-axis direction is not less than 2mm.It includes the casting equipment 4 of a blank for the rectangular block of casting
With a dissolution shaping device 5 for the blank progress shaping to the rectangular block, application method may include following steps,
Step A, provides a casting equipment 4, and the casting equipment 4 includes casting pedestal 41, positioning templet 42 and pours
Mold cavity 43, the casting pedestal 41 are connected with liftable first boom 411, are equipped with bearing on first boom 411, lead to
It crosses bearing and has been rotatably connected the fixed device 44 of the first false boss, the false boss 14 of the blade 1 to be measured is inserted
Enter to be mounted in the fixed device 44 of first false boss, then lock the blade 1 in first technique by screw
In the fixed device 44 of boss, it is lifted on the blade 1 on first boom 411, by adjusting first boom is locked
411 in the position of vertical direction, thus can be by the direction of the x, y, z axis of the theoretical reference coordinate system of the blade 1
It is fixed up, but the blade 1 (that is to say the theoretical reference coordinate system) can rotate on first boom 411.Then,
The tested corresponding positioning templet 42 of the blade 1 is mounted on the casting pedestal 41, in this manner it is possible to pass through institute
The fitting of the listrium 12 of positioning templet 42 and the blade 1 is stated, the angular of the blade 1 is fixed, so that the leaf
All freedom degrees of piece 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.
Referring to fig. 4 shown in a, 4b, 4c, the mold cavity 43 can be by the casting pedestal 41 and with the casting bottom
The formation of movable side wall 45 of 41 movable connections of seat, referring to fig. 4 shown in c, the first guiding has been can be set in the casting pedestal 41
Slot 46, first guide post 451 corresponding with first guide groove 46 has can be set in the movable side wall 45, in this way, described
Movable side wall 45 easily can be attached and separate with the casting pedestal 41, described so as to very easily be formed
Mold cavity 43, and the rectangular block 3 is taken out after cast molding.
The positioning templet 42 can be set with first boom 411 in the side of the mold cavity 43 of the same side
Wall, the movable side wall 45 can be the side wall relative to first boom 411, and the mold cavity 43 can be as shown in Figure 4 a
One T-type cavity, in this way, the T-type face 431 of the mold cavity 43 is the type chamber table for forming the first level face 31
Face, since casting process fully wrapped around can cover the locking plate slot 131 at 13 top of tenon tooth, the mold cavity 43
Using T-type cavity, then it can avoid the 431 molding first level face 31 of institute of T-type face in subsequent extra low-melting alloy
It in structure removal process, will not be destroyed, and can be used as positioning reference.
The side wall of c and Fig. 4 d referring to fig. 4, the movable side wall 45 and the casting pedestal 41 may be provided with the T
Type face 431, since the side wall of the casting pedestal where first boom 411 is fixed structure, and the movable side wall
45 need to carry out linear movement, and therefore, the T-type face 431 can be with the casting pedestal 41 where first boom 411
Side wall the T-type face 431 based on.When subsequent measurement clamping, the positioning surface for measuring tooling can the casting pedestal 41
The T-type face 431 of side wall be formed by the first level face 31 as positioning surface and carry out clamping.
The T-type face 431 of the side wall of the casting pedestal 41 where first boom 411 is provided with one first
Preformed groove 4111, corresponding first preformed groove 4111 of the movable side wall 45 are provided with the second preformed groove 4511, the activity
Side wall 45 is provided with the briquetting 4512 being detachably connected corresponding with second preformed groove 4511, passes through first preformed groove
4111 and second preformed groove 4511, " mouth " type can be set and positioned before installation blade, the rectangular block 3 of casting
Frame 47, the posting 47 can be the resin plate of the 3-4mm thickness by the metal plate or high temperature resistant (200 degree or more) of 3mm thickness
Material is made.
The posting 47 is arranged in the mold cavity 43 and then puts down the blade 1, then pouring by d referring to fig. 4
During casting, the posting 47 can cast with the rectangular block 3 and be integrated, since the posting 47 is to pass through before casting
Lead to the mold cavity 43 to place, therefore be capable of providing intuitive visual reference, consequently facilitating adjusting the blade 1 in vertical direction
Position, enable the operator to locking plate slot 131 described in intuitive judgment whether can be located at the first level face 31 under.This
Outside, the case where posting 47 is " mouth " type structure around one, also can avoid heat deformation warpage in casting process.
Step B is poured low-melting alloy in the mold cavity 43, is stained with cold water brush using hairbrush after casting and closes in low melting point
Jin Shang is waited 5 seconds or so, to low-melting alloy cooled and solidified, unclamps the screw of the fixed device 44 of first false boss, and
Remove the movable side wall 45 (if desired, first boom 411 can also be risen) of the mold cavity 43, so that it may take out
The blade 1 provided with the rectangular block 3.
Step C, provides a dissolution shaping device 5, and the dissolution shaping device 5 includes shaping pedestal 51, the shaping
Pedestal 51 is connected with liftable second boom 511, and second boom 511 is provided with the second false boss clamp device 54,
The insertion of the false boss 14 of the blade 1 to be measured is mounted in the fixed device 54 of second false boss, then is led to
It crosses screw to lock the blade 1 in the fixed device 54 of second false boss, the blade 1 is made to be lifted on described second
On boom 511, the shaping pedestal 51 is provided with hot oil chamber 52, and the hot oil chamber 52 is arranged below second boom 511,
It is injected with temperature in the hot oil chamber 52 and is not less than 180 DEG C of hot oil, by adjusting the height and position of second boom 511,
The package under the first level face 31 may make to cover the alloy component of the locking plate slot 131 at 13 top of tenon tooth
It immerses in the hot oil of the hot oil chamber 52, package thus may make to cover the locking plate slot 131 at 13 top of tenon tooth
Alloy dissolution, so that the locking plate slot 131 be made to be exposed from the rectangular block 3.Second boom 511 is promoted, is made described
Tenon tooth 13 and the hot oil of the hot oil chamber 52 disengage, and remove the blade 1, complete the preparation to the rectangular block 3.
As shown in figure 5,52 bottom of hot oil chamber may be provided with an oil outlet, top may be provided with pouring orifice, in this way,
The hot oil chamber 52 can be connect with hot-oil circulation processing equipment 6 by pipeline, so as to ensure in the hot oil chamber 52
Hot oil temperature, and the low-melting alloy for being dissolved into hot oil can be recycled in time.
The hot-oil circulation processing equipment 6 may include the cooling tank (not regarding out in figure) being linked in sequence and heater (figure
In do not regard out), specific structure can refer to team's one kind provided by Chinese patent 201611189008.2 where inventor
The structure of cooling tank and heater employed in the low-melting alloy removal device of blade inner cavity, details are not described herein.
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, that is, can control the blade
1 rectangular block 3 immerses the position in the hot oil of the hot oil chamber 52.It certainly, can also be as shown in figure 5, by the hot oil chamber
The size of the x-axis direction less than the rectangular block 3 is sized at least one direction of 52 top surface, in this way, can lead to
The posting 47 is crossed with the contact of 52 top surface of hot oil chamber to limit the position for the rectangular block 3 for immersing hot oil, had
The limit of the posting 47 is isolated, so that it may ensure that the first level face 31 will not contact with hot oil and melt deformation.
If the rectangular block 3 only rests in hot oil, then usually need just to can ensure that within 10-15 minutes the cladding locking plate slot
131 alloy all dissolves.
The fixed device 54 of second false boss can also be rotatably connected by bearing and second boom 511,
In this way, can be rotated the blade 1 after the blade 1 lifts and immerses hot oil, thus accelerate the speed of alloy dissolution, 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 and is fixedly connected with, 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, so as to more accurately control the revolving speed of the blade 1.
When the revolving speed of the blade 1 is controlled at 10-20 revs/min, the rectangular block 3 need to only impregnate 5-8 points in hot oil
Clock is that the alloy for coating the locking plate slot 131 may make all to dissolve.
Since on the rectangular block 3 after cast molding, the posting 47 can protrude from first plane 31, and
After step C processing, the posting 47 can be also retained among the rectangular block 3, therefore, when subsequent measurement clamping, be measured
The positioning surface of tooling can be with the T-type of the two side walls of not set first preformed groove 4111 of the casting pedestal 41
Face 431 is formed by the first level face 31 as positioning surface and carries out clamping.Evacuation opens the posting 47.
The casting equipment 4 can share a pedestal with the dissolution shaping device 5, that is to say, that the casting bottom
Seat 41 and the shaping pedestal 51 can complete all operationss in a station in this way on same bottom plate.
The casting equipment 4 can share a pedestal with the dissolution shaping device 5, that is to say, that the casting bottom
Seat 41 and the shaping pedestal 51 can complete all operationss in a station in this way on same bottom plate.
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.
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, it need to only keep the listrium
12 have certain distance with the side wall of the mold cavity 43.
The top surface and the minimum range of the listrium 12 in the z-axis direction that can control the rectangular block 3 are greater than 2mm, in this way
It can ensure the space needs that the size to the listrium 12 measures.
The first level face 31 can be made to be greater than 1.5mm with the minimum range of the locking plate slot 131 in the z-axis direction.This
Sample can reserve enough measurement spaces for the locking plate slot 131.
In practice, to 3 kinds of turbo blades of Mr. Yu's h type engine h, when due to using the device of the invention, casting equipment
Combinable is a set of, it is only necessary to the cast molding of different type blade base can be realized with changing positioning templet.And measurement process
Measurement tooling and the structure of measuring tool also greatly simplified, so that the time of replacement measuring tool is greatly decreased, compared with background
Original process method described in 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.
A kind of blade positioning base manufacturing device provided by the present invention is substantially shorter by preparing standardized base
The measurement duration of blade, while can reduce 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 (6)
1. a kind of blade positioning base manufacturing device, which is characterized in that the pedestal is leaf of the auxiliary to the blade of turbo blade
Molded dimension, the size of listrium and the locking plate slot size at the top of tenon tooth measure, and cast the circular institute formed by low-melting alloy
The rectangular block of tenon tooth is stated, the locking plate slot is not covered by low-melting alloy, and there is the turbo blade theoretical reference to sit
Mark system, the z-axis of the theoretical reference coordinate system are overlapped with the axis of the false boss of the blade, the theoretical reference coordinate system
X-y plane can pressed from both sides by two standard rollers that first pair of recessed portion for capableing of apical tooth two sides to the tenon tooth is clamped
Two axis of state are held to establish, the intersection point of z-axis and x-y plane is origin, and x-axis passes through origin and the axis with the roller
In parallel, y-axis is vertical with x-axis.The rectangular block include be linked in sequence the first side elevation, the second side elevation, third side elevation and
4th side elevation, first side elevation and/or the third side elevation are parallel with the x-axis of the theoretical reference coordinate system, institute
It states the second side elevation and/or the 4th side elevation is parallel with the y-axis of the theoretical reference coordinate system, the rectangular block further includes
Vertical with the z-axis of the theoretical reference coordinate system first level face close to the locking plate slot, the top surface of the rectangular block with
The minimum range of the listrium in the z-axis direction is not less than 2mm.It includes pouring for a blank for the rectangular block of casting
Casting machine and a dissolution shaping device for the blank progress shaping to the rectangular block,
The casting equipment includes casting pedestal, positioning templet and mold cavity, and the casting pedestal is connected with liftable the
One boom is equipped with bearing on first boom, has been rotatably connected the fixed device of the first false boss by bearing, described
Mold cavity is a T-type cavity, work of the mold cavity by the casting pedestal and with the casting movable connection of pedestal
Dynamic side wall is formed, and the T-type face of the side wall of the casting pedestal where first boom is provided with the first preformed groove, the work
Dynamic side wall corresponds to first preformed groove and is provided with the second preformed groove, and the movable side wall is provided with and second preformed groove pair
The briquetting being detachably connected answered is provided with " mouth " type positioning by first preformed groove and second preformed groove
Frame.
The dissolution shaping device includes shaping pedestal, and the shaping pedestal is connected with liftable second boom, and described second
Boom is provided with the second false boss clamp device, and the shaping pedestal is provided with hot oil chamber, and the hot oil chamber is arranged described
Below second boom, the intracavitary hot oil for being injected with temperature and being not less than 180 DEG C of the hot oil, at least the one of the top surface of the hot oil chamber
Size on a direction is less than the size of the x-axis direction of the rectangular block.
2. the apparatus according to claim 1, which is characterized in that at least one side of the mold cavity is by removably living
Dynamic baffle is formed.
3. the apparatus according to claim 1, at least one side of the mold cavity is the inclined-plane being inclined outwardly.
4. the apparatus according to claim 1, the T-type face of the mold cavity is the level for forming the first level face
Type face.
5. the apparatus according to claim 1, the posting is made of the metal plate of 3mm thickness.
6. the apparatus according to claim 1, the posting is made of the resin plate of 3-4mm thickness.
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| CN201811495918.2A CN109332652B (en) | 2018-12-07 | 2018-12-07 | Blade positioning base manufacturing device |
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| CN201811495918.2A CN109332652B (en) | 2018-12-07 | 2018-12-07 | Blade positioning base manufacturing device |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112729069A (en) * | 2020-12-24 | 2021-04-30 | 中国航发北京航空材料研究院 | Turbocharger impeller blade outer edge defect detection tool and detection method thereof |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3822080A1 (en) * | 1987-07-22 | 1989-02-02 | Rolls Royce Plc | METHOD FOR PRODUCING AN AXIAL FLOW COMPRESSOR ASSEMBLY |
| CN101513708A (en) * | 2009-03-19 | 2009-08-26 | 无锡透平叶片有限公司 | Method for locating datum surface to process leaf blade and blade root |
| CN102145460A (en) * | 2010-11-20 | 2011-08-10 | 无锡透平叶片有限公司 | Novel integral turning method of blades |
| 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 |
| CN103350213A (en) * | 2013-07-04 | 2013-10-16 | 常州市三维技术成套设备有限公司 | Low-melting-point alloy casting positioning technology in turbine blade machining |
| CN105382202A (en) * | 2015-12-04 | 2016-03-09 | 南车玉柴四川发动机股份有限公司 | Method for meeting positioning requirement of complex-shaped workpiece through alloy casting |
| 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 |
| CN108917548A (en) * | 2018-04-19 | 2018-11-30 | 中国航发南方工业有限公司 | Turbo blade Surface inspection method and measuring device |
-
2018
- 2018-12-07 CN CN201811495918.2A patent/CN109332652B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3822080A1 (en) * | 1987-07-22 | 1989-02-02 | Rolls Royce Plc | METHOD FOR PRODUCING AN AXIAL FLOW COMPRESSOR ASSEMBLY |
| CN101513708A (en) * | 2009-03-19 | 2009-08-26 | 无锡透平叶片有限公司 | Method for locating datum surface to process leaf blade and blade root |
| CN102145460A (en) * | 2010-11-20 | 2011-08-10 | 无锡透平叶片有限公司 | Novel integral turning method of blades |
| 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 |
| CN103350213A (en) * | 2013-07-04 | 2013-10-16 | 常州市三维技术成套设备有限公司 | Low-melting-point alloy casting positioning technology in turbine blade machining |
| 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 |
| CN105382202A (en) * | 2015-12-04 | 2016-03-09 | 南车玉柴四川发动机股份有限公司 | Method for meeting positioning requirement of complex-shaped workpiece through alloy casting |
| CN108917548A (en) * | 2018-04-19 | 2018-11-30 | 中国航发南方工业有限公司 | Turbo blade Surface inspection method and measuring device |
Non-Patent Citations (2)
| Title |
|---|
| 樊秋玲等: "叶片加工中的方箱工艺及设备", 《发电设备》 * |
| 申秀丽等: "《航空燃气涡轮发动机典型制造工艺》", 30 June 2016, 北京航空航天大学出版社 * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112729069A (en) * | 2020-12-24 | 2021-04-30 | 中国航发北京航空材料研究院 | Turbocharger impeller blade outer edge defect detection tool and detection method thereof |
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| CN109332652B (en) | 2020-10-16 |
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