Jet type heat treatment device suitable for cavity structure with large length-diameter ratio and wall thickness
By inserting the jet tube into the large length-to-diameter ratio and wall thickness cavity structure and spraying the coolant with a high-pressure jet pump, the problem of insufficient heat treatment caused by the difficulty of heat treatment liquid and excessive wall thickness is solved, and a higher quality heat treatment is achieved Effect.
Patent Information
- Application Number
- CN202411653456.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-11-18
- Publication Date
- 2025-02-18
AI Technical Summary
The prior art is difficult to effectively carry out heat treatment of cavity structures with large aspect ratios and wall thickness, especially because the heat treatment liquid is difficult to enter the interior of the cavity and the wall thickness is too large, resulting in insufficient heat treatment, which affects the structural strength.
A jet heat treatment device is designed to achieve effective heat treatment by inserting a jet tube into the cavity structure and spraying coolant onto the inner surface of the cavity using a high-pressure jet pump.
This device can overcome the influence of gas film formation in traditional heat exchange, effectively solve the heat treatment problems of the internal materials of large aspect ratio and wall thickness components, and improve the heat treatment quality and structural strength.
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Figure CN119464671A_ABST
Abstract
Description
Technical Field
[0001] The invention relates to the field of casting heat treatment, and in particular to a jet heat treatment device suitable for a cavity structure with a large aspect ratio and a thick wall. Background Art
[0002] At present, the casting process is used to obtain a cavity structure with a large aspect ratio and thick wall, which mainly uses a high-temperature alloy solution to flow and form in a mold and improve the structural strength through a certain heat treatment process. In the heat treatment process of the component, it is usually necessary to place the high-temperature structure in the heat treatment liquid to quickly cool the structure to obtain high-strength material properties. However, when carrying out the material heat treatment process for the cavity structure with a large aspect ratio and thick wall, the main problems are that the heat treatment liquid is difficult to effectively enter the cavity and the wall thickness is too large to effectively heat treat, resulting in low heat treatment quality of the material inside the cavity, which in turn affects the strength and use of the structure. This phenomenon is particularly obvious for structures that are closed at one end. There are two main reasons for this phenomenon:
[0003] On the one hand, for the heat treatment process of high-temperature objects, boiling will occur when the heat treatment liquid contacts the wall of the high-temperature object, which reduces the heat treatment efficiency, which makes the heat treatment thickness of the high-temperature object have an upper limit. Boiling heat transfer is a form of convective heat transfer that generates steam due to the contact between the liquid and the high-temperature wall, which takes away the heat of the object. Figure 1As shown in the figure, during heat exchange, four heat exchange areas will appear on the wall of the high-temperature object, namely, natural convection area, nucleate boiling area, transition boiling area and stable transient boiling. When the temperature difference is small, the heat exchange between the high-temperature object and the coolant belongs to natural convection; when the surface temperature of the object is slightly higher than the saturation temperature point, bubbles are generated at the interface between the wall of the object and the cooling medium, and the nucleate boiling heat exchange stage is entered. In this stage, as the temperature difference further increases, the heat transfer coefficient and heat flux density on the surface of the high-temperature object increase rapidly, and heat conduction is the main heat dissipation; when the temperature difference continues to increase, the heat exchange enters the transition boiling stage, and the heat flux density decreases instead of increasing in this stage. The reason is that there are too many bubbles formed at the interface between the wall of the object and the cooling medium, so that a gas film is formed on the interface, which hinders the heat transfer from the hot surface to the liquid; when the temperature difference increases further, the heat exchange enters the stable transient boiling stage, and in this stage the interface is completely covered with a stable vapor film, the heat transfer coefficient is very small, and heat dissipation is mainly carried out by liquid film conduction. General water cooling will form a layer of steam film at the contact interface between the high-temperature object and the coolant. The object transfers heat to the coolant through the steam film, which is an order of magnitude lower than the heat transfer coefficient of direct contact between the high-temperature object and the coolant. Therefore, the existence of a large area of steam film seriously affects the heat transfer efficiency. This situation is more significant for the heat treatment of large aspect ratio cavity structures. During heat treatment, since the internal cavity of the large aspect ratio component is relatively small, a large number of bubbles will be formed on the surface of the material during heat treatment, resulting in insufficient heat treatment of the material inside the cavity, which in turn affects the strength of the material after heat treatment. Especially for structures with one end closed, it is even more difficult for the heat treatment liquid to effectively enter the closed end of the large aspect ratio structure. The material at this end is not sufficiently heat treated, which can easily cause defects inside the material.
[0004] On the other hand, when the traditional cooling pool cooling heat treatment process is used for thick-walled cavity materials, the effective heat treatment part is mostly the surface material of the cavity structure, and the heat treatment thickness is limited. In particular, the thickness of the effective heat treatment material is extremely limited because the heat treatment liquid is difficult to enter the inner surface of the cavity (only the shallow surface material can meet the heat treatment process's material processing requirements). Therefore, it is difficult for the current heat treatment process to perform high-quality heat treatment on large aspect ratio and thick-walled cavity structures. In addition, if it is a multi-layer cavity structure, such as Figure 2 As shown, the material processing of the intermediate structure part is also difficult to meet the relevant heat treatment process requirements. Therefore, it is urgent to design a jet heat treatment device suitable for large aspect ratio and thick wall cavity structure to solve the above problems. Summary of the invention
[0005] The present invention provides a jet heat treatment device suitable for a cavity structure with a large aspect ratio and a thick wall, which has the effect of spraying a cooling medium onto the inner surface of the cavity for cooling. The specific technical scheme is as follows:
[0006] A jet heat treatment device suitable for a cavity structure with a large aspect ratio and a thick wall, which includes a placement table, on which the cavity structure to be heat treated can be placed and fixed, and a jet device is arranged at one end of the placement table, the jet device includes a plurality of jet tubes, on which injection holes are arranged, the jet tubes can be inserted into the interior of the cavity structure, the jet tubes are connected to a high-pressure jet pump, the high-pressure jet pump provides power for the coolant required for the heat treatment and can be ejected from the injection holes on the jet tubes to perform heat treatment on the interior of the cavity structure.
[0007] Furthermore, a plurality of groups of injection holes are arranged at intervals on the surface of the jet tube, each group of injection holes has four injection holes, and the angle between two adjacent injection holes in the same group is 90 degrees.
[0008] Furthermore, the jet device comprises a moving platform, a first supporting frame is arranged on the moving platform, the jet tube is arranged on the first supporting frame, and the moving platform can drive the jet tube to move horizontally as a whole.
[0009] Furthermore, a second support frame is provided at the end of the placement table, and the second support frame can provide support and guidance for the jet tube.
[0010] Furthermore, one end of the jet tube close to the mobile station is connected to a liquid infusion tube, which is annular and has a liquid inlet on both sides. The liquid infusion tube is connected to a high-pressure jet pump through the two liquid inlets.
[0011] Furthermore, a spray speed regulating device is connected inside the jet tube, and the spray speed regulating device can adjust the flow rate and speed of the coolant sprayed from the spray hole of the jet tube.
[0012] Furthermore, the spray speed adjustment device includes an adjustment rod, which is inserted into the jet tube. An adjustment baffle is provided on the adjustment rod, which is in conflict with the inner wall of the jet tube. There are multiple adjustment baffles and their positions correspond to the spray holes. Rotating the adjustment rod can change the size of the water outlet cross-section of the spray hole.
[0013] Furthermore, the adjusting rod is connected to the adjusting mechanism, and the adjusting mechanism can drive the plurality of adjusting rods to rotate synchronously so as to simultaneously adjust the flow rate and speed of the coolant of all the injection ports.
[0014] Furthermore, the end of the jet tube inserted into the cavity structure is arc-shaped, and a plurality of jet holes are axially inclinedly arranged on the arc-shaped surface.
[0015] Furthermore, a clamping and positioning assembly is provided on the placement table, and the clamping and positioning assembly can position and clamp the cavity structure placed on the placement table.
[0016] The jet heat treatment device suitable for cavity structures with large aspect ratios and thick walls of the present invention has a simple structure and ingenious design. By inserting a jet tube into the cavity structure, the coolant is brought into the cavity structure for heat treatment, thereby overcoming the unfavorable factor in traditional heat exchange theory that the air film generated between the heat treatment liquid and the wall of the high-temperature object affects the heat treatment effect, and effectively solves the heat treatment problem of the internal materials of components with large aspect ratios and thick walls.
[0017] The above description is only an overview of the technical solution of the present invention. In order to more clearly understand the technical means of the present invention, it can be implemented according to the contents of the specification. In order to make the above and other purposes, features and advantages of the present invention more obvious and easy to understand, the specific implementation methods of the present invention are listed below. BRIEF DESCRIPTION OF THE DRAWINGS
[0018] Various other advantages and benefits will become apparent to those of ordinary skill in the art by reading the detailed description of the preferred embodiments below. The accompanying drawings are only for the purpose of illustrating the preferred embodiments and are not to be considered as limiting the present invention. Moreover, the same reference symbols are used throughout the accompanying drawings to represent the same components. In the accompanying drawings:
[0019] Figure 1 It is the relationship diagram between heat flux density and superheat temperature difference;
[0020] Figure 2 It is a cavity structure with large aspect ratio and thick wall;
[0021] Figure 3 A three-dimensional diagram of a jet heat treatment device suitable for a cavity structure with a large aspect ratio and a thick wall according to the present invention;
[0022] Figure 4 A schematic diagram of the jet tube of the jet heat treatment device of the present invention suitable for a cavity structure with a large aspect ratio and a thick wall when it is ready to be inserted;
[0023] Figure 5 It is a schematic diagram of the jet tube of the jet heat treatment device suitable for a cavity structure with a large aspect ratio and a thick wall after being inserted;
[0024] Figure 6 It is a schematic structural diagram of a jet hole of a jet tube of a jet type heat treatment device suitable for a cavity structure with a large aspect ratio and a thick wall according to the present invention;
[0025] Figure 7 The schematic diagram of the structure of the jet tube and the regulating device of the jet type heat treatment device suitable for the cavity structure with large aspect ratio and wall thickness of the present invention. DETAILED DESCRIPTION
[0026] In order to better understand the purpose, function and specific design scheme of the present invention, the jet heat treatment device suitable for large aspect ratio and thick wall cavity structure of the present invention is further described in detail below with reference to the accompanying drawings.
[0027] like Figure 3-7 As shown, the jet heat treatment device suitable for a cavity structure with a large aspect ratio and a thick wall of the present invention includes a placing table 1, and the cavity structure 3 to be heat treated can be placed on the placing table 1 and fixed. A jet device 2 is arranged at one end of the placing table 1, and the jet device 2 includes a plurality of jet tubes 21, and a spray hole 22 is arranged on the jet tube 21. The jet tube 21 can be inserted into the interior of the cavity structure 3. The jet tube 21 is connected to a high-pressure jet pump, and the high-pressure jet pump provides power for the coolant required for the heat treatment and can be sprayed from the spray hole 22 on the jet tube 21 to perform heat treatment on the interior of the cavity structure 3.
[0028] Specifically, multiple groups of injection holes 22 are arranged on the surface of the jet tube 21 at intervals, and the interval between two adjacent groups of injection holes 22 is 5 to 10 cm. There are four injection holes 22 in each group, and the angle between two adjacent injection holes 22 in the same group is 90 degrees. The main purpose of the coolant is to break through the air film and dissipate heat evenly. The material of the jet tube 21 can be ceramic or other high-temperature resistant materials. Preferably, a marking scale is set on the outer surface of the jet tube 21, and the length of the jet tube 21 penetrating into the cavity structure 3 can be obtained according to the scale value.
[0029] The jet device 2 of this embodiment further includes a moving platform 4, on which a first support frame 41 is disposed, and the jet tube 21 is disposed on the first support frame 41. The moving platform 4 can drive the jet tube 21 to move horizontally as a whole, thereby facilitating the insertion of the jet tube 21 into the interior of the cavity structure 3 on the placement platform 1. Preferably, a second support frame 11 is disposed at the end of the placement platform 1, and the second support frame 11 can provide support and guidance for the jet tube 21, so that the jet tube 21 can be stably and reliably inserted into the interior of the cavity structure 3 on the placement platform 1.
[0030] One end of the jet tube 21 close to the moving platform 4 is connected to the infusion tube 24. The infusion tube 24 is ring-shaped. A liquid inlet 25 is respectively provided on both sides of the infusion tube 24. The infusion tube 24 is connected to a high-pressure jet pump through the two liquid inlets 25. While increasing the coolant pressure in the jet tube 21, the pressure in the jet tube 21 at different positions can also be made more uniform.
[0031] like Figure 4 and Figure 7As shown, a jet speed regulating device 5 is connected to the jet tube 21, and the jet speed regulating device 5 can adjust the flow rate and speed of the coolant sprayed from the jet hole 22 of the jet tube 21. The jet speed regulating device 5 includes an adjusting rod 51, which is inserted into the jet tube 21, and an adjusting baffle 52 is arranged on the adjusting rod 51, and the adjusting baffle 52 is in conflict with the inner wall of the jet tube 21. There are multiple adjusting baffles 52 and their positions correspond to the jet hole 22. Rotating the adjusting rod 51 can change the size of the water outlet cross section of the jet hole 22, thereby changing the flow rate and speed of the coolant.
[0032] The adjusting rod 51 is connected to the adjusting mechanism 53, which is fixed on the moving platform 4. The adjusting mechanism 53 can drive multiple adjusting rods 51 to rotate synchronously to achieve the effect of adjusting the flow rate and speed of the coolant of all the injection ports at the same time. The adjusting mechanism 53 of this embodiment is a gear set structure, and the adjusting mechanism 53 includes an adjusting motor 54, which is connected to a reducer, and the adjusting motor 54 and the reducer are fixed on the moving platform 4. The reducer is connected to the driving gear of the gear set, and the driving gear drives each driven gear to rotate, so as to drive the adjusting rods 51 in each jet tube 21 to rotate synchronously, thereby adjusting the flow rate and speed of the coolant of the injection hole 22.
[0033] The maximum injection velocity of the coolant is designed based on the ability to effectively penetrate the air film formed on the interface between the object wall and the cooling medium due to the high temperature difference, where the collision pressure threshold for penetrating the air film is P0. When the speed of the coolant ejected from the jet tube 21 is u, the pressure value generated by the coolant can be calculated according to the Bernoulli equation of fluid mechanics according to formula (1):
[0034] P=0.5ρu 2 (1)
[0035] Where P is the coolant collision pressure, ρ is the coolant density, and u is the coolant injection velocity.
[0036] When formula (2) is satisfied, the coolant ejected from the jet tube 21 can begin to break through the air film formed at the interface between the object wall and the cooling medium due to the excessive temperature difference.
[0037] P=P0 (2)
[0038] According to formulas (1) and (2), it can be deduced that the minimum speed at which the coolant ejected from the multi-stage ejector rod can penetrate the air film formed at the interface between the object wall and the cooling medium due to the high temperature difference is:
[0039]
[0040] The high-pressure jet pump can use this speed as the minimum speed for breaking the film and adjust the cooling liquid speed through the injection speed regulating device 5.
[0041] It is worth noting that Figure 6 As shown, the end of the jet tube 21 inserted into the cavity structure 3 is arc-shaped, that is, the end of the jet tube 21 away from the moving platform 4 is arc-shaped, and a plurality of jet holes 23 are axially inclined on the arc surface. The coolant ejected by the jet hole 23 can not only break through the air film and dissipate heat evenly, but also accelerate the flow of the coolant inside the cavity structure 3. Its main effect on accelerating the flow of the coolant can be quantitatively described by the following formula. When the ejection speed of the coolant is u, the reverse pressure P1 generated in the axial direction can be quantitatively expressed as
[0042] P1=Pcosθ (4)
[0043] When the cavity cross-sectional area is S, the thrust generated by the coolant injection is
[0044] F=P1×S (5)
[0045] When the mass of the coolant in the cavity is M, the acceleration caused by the injection of the heat treatment liquid is
[0046] a=F / M (6)
[0047] On this basis, the speed requirement of the circulation flow of the cooling liquid in the heat treatment process can be further met by adjusting the injection speed of the heat treatment liquid.
[0048] The high-pressure jet pump of this embodiment can set the injection process according to the required injection speed, and the high-pressure jet pump can be a mature industrial product.
[0049] like Figure 3 As shown, a clamping and positioning assembly 6 is provided on the placement table 1, and the clamping and positioning assembly 6 can position and clamp the cavity structure 3 placed on the placement table 1. The clamping and positioning assembly 6 includes a positioning plate 61, and the positioning plate 61 is vertically movably arranged above both sides of the placement table 1. The positioning plate 61 is connected to a positioning drive assembly, and the positioning drive assembly can drive the positioning plate 61 to move so that the positioning plate 61 conflicts with the cavity structure 3 and clamps the cavity structure 3. The drive assembly can be a cylinder or an electric cylinder. It can be understood that by pushing the positioning plates 61 on both sides, the cavity structure 3 can be placed in the center of the placement table 1 to facilitate the insertion of the jet tube 21. Preferably, a guide plate 62 is connected above the positioning plate 61, and the guide plate 62 is inclined to the outside of the two sides of the placement table 1, so as to provide a guiding effect when the cavity structure 3 is placed.
[0050] Preferably, the placement platform 1 includes a liftable lifting platform 12, the upper surface of the lifting platform 12 is used to place the cavity structure 3, and the lower part of the lifting platform 12 is connected to a lifting mechanism, which can drive the lifting platform 12 to move up and down, thereby adjusting the height of the cavity structure 3 to be aligned with the jet tube 21. The lifting mechanism can be a jack or the like.
[0051] The use process of the jet heat treatment device of the present invention, which is suitable for a cavity structure with a large aspect ratio and a thick wall, is as follows:
[0052] (1) Determine the type of heat treatment liquid (air cooling, water cooling, oil cooling, etc.), the heat treatment process flow, etc. according to the basic properties of the cavity structure 3 to be heat treated, the material property requirements after heat treatment, and other information.
[0053] (2) According to the initial heat treatment environment, the basic properties of the cavity structure 3 to be heat treated, the material property requirements after heat treatment and other conditions, the membrane rupture pressure and the injection liquid flow rate of the component heat treatment process are calculated and determined, and the injection liquid injection process is determined.
[0054] (3) Insert the jet tube 21 into the cavity, turn on the high-pressure jet pump, and fill the jet tube 21 with coolant. If the film needs to be broken due to temperature difference, first adjust the flow rate of the jet liquid until the requirement is met, wait until the inner surface temperature of the cavity structure 3 drops to the point where no air film is generated, and then control the baffle 52 again to allow the coolant to be sprayed onto the inner surface of the cavity structure 3 to achieve heat dissipation. Then, the jet speed adjustment device 5 is used to adjust the jet speed of the jet liquid according to the process conditions of the required heat treatment.
[0055] (4) After the heat treatment of the cavity structure 3 is completed, the high-pressure jet pump is first turned off, and then the jet tube 21 is withdrawn, thereby completing the heat treatment of the component with a large aspect ratio and thick wall.
[0056] The jet heat treatment device suitable for cavity structures with large aspect ratios and thick walls of the present invention has a simple structure and ingenious design. By inserting a jet tube into the cavity structure, the coolant is brought into the cavity structure for heat treatment, thereby overcoming the unfavorable factor in traditional heat exchange theory that the air film generated between the heat treatment liquid and the wall of the high-temperature object affects the heat treatment effect, and effectively solves the heat treatment problem of the internal materials of components with large aspect ratios and thick walls.
[0057] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention, rather than to limit it. Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that they can still modify the technical solutions described in the aforementioned embodiments, or make equivalent replacements for some of the technical features therein. However, these modifications or replacements do not deviate the essence of the corresponding technical solutions from the spirit and scope of the technical solutions of the embodiments of the present invention.
Claims
1. A jet heat treatment device suitable for cavity structures with large aspect ratio and wall thickness, characterized in that: It includes a placing table, and the cavity structure to be heat-treated can be placed on the placing table and fixed. A jet device is arranged at one end of the placing table, and the jet device includes a plurality of jet tubes, and the jet tubes are provided with injection holes. The jet tubes can be inserted into the interior of the cavity structure. The jet tubes are connected to a high-pressure jet pump, and the high-pressure jet pump provides power for the coolant required for the heat treatment and can be sprayed from the injection holes on the jet tubes to perform heat treatment on the interior of the cavity structure.
2. The jet heat treatment device suitable for cavity structures with large aspect ratio and wall thickness as claimed in claim 1, characterized in that: A plurality of groups of injection holes are arranged at intervals on the surface of the jet tube, each group of injection holes has four injection holes, and the angle between two adjacent injection holes in the same group is 90 degrees.
3. The jet heat treatment device suitable for cavity structures with large aspect ratio and wall thickness as claimed in claim 1, characterized in that: The jet device comprises a moving platform, a first supporting frame is arranged on the moving platform, the jet tube is arranged on the first supporting frame, and the moving platform can drive the jet tube to move horizontally as a whole.
4. The jet heat treatment device suitable for cavity structures with large aspect ratio and wall thickness as claimed in claim 3, characterized in that: A second support frame is arranged at the end of the placement table, and the second support frame can provide support and guidance for the jet tube.
5. The jet heat treatment device suitable for cavity structures with large aspect ratio and wall thickness as claimed in claim 3, characterized in that: One end of the jet tube close to the mobile station is connected to the infusion tube, which is annular and has a liquid inlet on both sides. The infusion tube is connected to a high-pressure jet pump through the two liquid inlets.
6. The jet heat treatment device suitable for cavity structures with large aspect ratio and wall thickness as claimed in claim 1, characterized in that: The jet pipe is connected with a spray speed regulating device, which can regulate the flow rate and speed of the coolant sprayed from the spray hole of the jet pipe.
7. The jet heat treatment device suitable for cavity structures with large aspect ratio and wall thickness as claimed in claim 6, characterized in that: The spray speed adjustment device includes an adjustment rod, which is inserted into the jet tube. An adjustment baffle is arranged on the adjustment rod. The adjustment baffle is in conflict with the inner wall of the jet tube. There are multiple adjustment baffles and their positions correspond to the spray holes. Rotating the adjustment rod can change the size of the water outlet section of the spray hole.
8. The jet heat treatment device suitable for cavity structures with large aspect ratio and wall thickness as claimed in claim 7, characterized in that: The regulating rod is connected to the regulating mechanism, and the regulating mechanism can drive multiple regulating rods to rotate synchronously to simultaneously adjust the flow rate and speed of the coolant of all the injection ports.
9. The jet heat treatment device suitable for cavity structures with large aspect ratio and wall thickness as claimed in claim 1, characterized in that: The end of the jet tube inserted into the cavity structure is arc-shaped, and a plurality of jet holes are axially inclinedly arranged on the arc-shaped surface.
10. The jet heat treatment device suitable for cavity structures with large aspect ratio and wall thickness as claimed in claim 1, characterized in that: The placement table is provided with a clamping and positioning component, and the clamping and positioning can position and clamp the cavity structure placed on the placement table.