Storage device for high-precision turbine blades
By designing a specific storage device, utilizing the fit between the limiting tube and the turbine blade shaft hole, and controlling the ambient temperature, the problem of damage to high-precision turbine blades during storage and transportation was solved, resulting in a longer service life and greater resistance.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- CHENGDU AEROSPACE SUPERALLOY TECH CO LTD
- Filing Date
- 2025-04-24
- Publication Date
- 2026-04-17
AI Technical Summary
High-precision turbine blades have a shorter service life under traditional storage methods and are easily damaged or even scrapped under force majeure.
A storage device comprising crossbars, connecting bars, load-bearing supports, and limiting tubes was designed. The limiting tubes cooperate with the shaft holes of the turbine blades to restrict their movement. Combined with a structure that keeps the ambient temperature constant, it prevents high-temperature oxidation and improves storage stability.
It effectively prevents turbine blades from being damaged by collisions and high-temperature oxidation during storage and transportation, thus improving service life and enhancing resistance.
Smart Images
Figure CN224129752U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to turbine blades, and more specifically, to a storage device for high-precision turbine blades. Background Technology
[0002] The manufacturing process of turbine blades is quite complex, mainly including: investment casting (manufacturing blades through investment casting process), precision machining (using CNC machine tools to precisely machine the blade blanks to ensure that the dimensions and shape meet the design requirements), heat treatment, surface treatment, etc.
[0003] Before the produced turbine blades reach the subsequent assembly plant or user, they need to be stored in the turbine blade manufacturer's warehouse and transported to the subsequent assembly plant or user by transportation, which may also involve sea transportation.
[0004] The conventional method of storing turbine blades is to lay them flat at approximately equal intervals. Figure 1 On the storage rack shown, after placement, there is a gap between the tips of two adjacent turbine blades to prevent the tips from colliding and affecting performance.
[0005] High-precision turbine blades, such as those used in aerospace, employ... Figure 1 The storage racks shown will reduce the service life of high-precision turbine blades, and in severe cases, render them unusable. Furthermore, in the event of force majeure such as earthquakes, there is a possibility that the high-precision blades may be rendered unusable. Therefore, there is an urgent need for a storage device specifically designed for high-precision turbine blades. Utility Model Content
[0006] To address the aforementioned problems, this utility model provides a high-precision turbine blade storage device, which aims to improve at least one of the problems mentioned in the background art.
[0007] A storage device for high-precision turbine blades includes a first horizontal bar, a second horizontal bar, a first connecting bar, a second connecting bar, and four load-bearing supports. The storage device also includes a third horizontal bar located between the first and second horizontal bars. One end of the third horizontal bar is connected to the first connecting bar, and the other end is connected to the second connecting bar. Several circumferential limiting tubes are arranged on the third horizontal bar in the transverse direction. The distance between two adjacent circumferential limiting tubes is greater than the circumferential dimension of the high-precision turbine blade.
[0008] Optionally, the outer diameter of the circumferential limiting tube is matched with the shaft hole of the turbine blade.
[0009] Optionally, the upper end of the circumferential limiting tube is detachably connected to an axial limiting mechanism, which includes a connecting tube and a limiting cap connected to its upper end.
[0010] Optionally, the connecting pipe is provided with external threads, and the circumferential limiting pipe is provided with internal threads.
[0011] Optionally, the diameter of the limiting cap is less than or equal to the outer diameter of the wheel.
[0012] Optionally, the storage device further includes an ambient temperature constant structure.
[0013] Optionally, the constant ambient temperature structure includes a first pipe, a second pipe, a third pipe, a first elbow pipe, and a second elbow pipe. One end of the first elbow pipe is connected to the first pipe, and the other end is connected to the second pipe. One end of the second elbow pipe is connected to the remaining end of the second pipe, and the other end is connected to the third pipe. The first pipe is installed on the lower surface of the first horizontal bar, the second pipe is installed on the lower surface of the third horizontal bar, and the third pipe is installed on the lower surface of the second horizontal bar.
[0014] Compared with the prior art, the beneficial effects of this utility model are as follows:
[0015] The high-precision turbine blade storage device provided by this utility model improves the service life of high-precision turbine blades through its unique structure and can resist force majeure. Attached Figure Description
[0016] To more clearly illustrate the technical solutions in the embodiments of this application or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are some embodiments of this application. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.
[0017] Figure 1 This is a schematic diagram of the overall structure of the storage rack in the background technology of this utility model;
[0018] Figure 2 This is a schematic diagram of the storage device structure of this utility model;
[0019] Figure 3 This is a schematic diagram of the axial limiting mechanism of this utility model;
[0020] Figure 4 This is a schematic diagram of the structure of this utility model with constant ambient temperature.
[0021] Explanation of reference numerals in the attached drawings: 1. First horizontal bar; 2. Second horizontal bar; 3. Third horizontal bar; 4. Four load-bearing columns; 5. First connecting bar; 6. Second connecting bar; 7. Circumferential limiting tube; 8. Axial limiting mechanism; 9. Connecting tube; 10. Limiting cap; 11. Structure for maintaining constant ambient temperature; 12. First pipe; 13. Second pipe; 14. Third pipe; 15. First elbow pipe; 16. Second elbow pipe. Detailed Implementation
[0022] In the description of this utility model, it should be noted that, unless otherwise explicitly specified and limited, the terms "installation," "connection," and "linking" should be interpreted broadly. For example, they can refer to a fixed connection, an indirect connection through an intermediate medium, or the internal communication of two components or the interaction between two components. Those skilled in the art can understand the specific meaning of the above terms in this utility model according to the specific circumstances.
[0023] In the description of this utility model, it should be understood that the terms "upper," "lower," "front," "rear," "vertical," "horizontal," "top," "bottom," "inner," and "outer," etc., indicating the orientation or positional relationship, are based on the orientation or positional relationship shown in the accompanying drawings and are only for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation, and therefore should not be construed as a limitation of this utility model. In the description of this utility model, "a plurality of" means two or more, unless otherwise precisely specified.
[0024] The terms “first,” “second,” “third,” “fourth,” etc. (if present) in the specification, claims, and accompanying drawings of this application are used to distinguish similar objects and are not necessarily used to describe a particular order or sequence. It should be understood that such data can be interchanged where appropriate so that the embodiments of this application described herein can be implemented, for example, in orders other than those illustrated or described herein. Furthermore, the terms “comprising” and “having,” and any variations thereof, are intended to cover a non-exclusive inclusion; for example, a process, method, system, product, or apparatus that comprises a series of steps or units is not necessarily limited to those steps or units explicitly listed, but may include other steps or units not explicitly listed or inherent to such processes, methods, products, or apparatus.
[0025] To make the objectives, technical solutions, and advantages of the embodiments of this application clearer, the technical solutions of the embodiments of this application will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of this application, not all embodiments. Based on the embodiments of this application, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of this application.
[0026] The technical solution of this utility model will be described in detail below with specific embodiments. These specific embodiments can be combined with each other, and the same or similar concepts or processes may not be described again in some embodiments.
[0027] Please refer to Figures 2-4 , Figure 2 This is a schematic diagram of the storage device structure of this utility model. Figure 3 This is a schematic diagram of the axial limiting mechanism of this utility model. Figure 4 This is a schematic diagram of the structure of this utility model with constant ambient temperature.
[0028] A storage device for high-precision turbine blades includes a first horizontal bar 1, a second horizontal bar 2, a third horizontal bar 3, a first connecting bar 5, a second connecting bar 6, and four load-bearing supports 4. One end of the first connecting bar 5 is connected to one end of the first horizontal bar 1, and the other end is connected to one end of the second horizontal bar 2. One end of the second connecting bar 6 is connected to the remaining end of the first horizontal bar 1, and the other end is connected to the remaining end of the second horizontal bar 2. The four load-bearing supports 4 provide support for the rectangular structure formed by connecting the first horizontal bar 1, the second horizontal bar 2, the first connecting bar 5, and the second connecting bar 6. The third horizontal bar 3 is located between the first horizontal bar 1 and the second horizontal bar 2. One end of the third horizontal bar 3 is connected to the first connecting bar 5, and the other end is connected to the second connecting bar 6. Several circumferential limiting tubes 7 are provided on the third horizontal bar 3 in the transverse direction. The distance between two adjacent circumferential limiting tubes 7 is greater than the circumferential dimension of the high-precision turbine blade.
[0029] By setting the third horizontal bar 3 and the circumferential limiting tube 7, the high-precision turbine blade is placed through its shaft hole during storage. After placement, a portion of the high-precision turbine blade's disc rests on the first horizontal bar 1, and a symmetrical portion rests on the second horizontal bar 2. The circumferential limiting tube 7 restricts the lateral movement of the high-precision turbine blade, effectively preventing wear, collision, and damage to the blade portion (especially the tip) caused by axial movement, even under force majeure.
[0030] In one or more specific embodiments of this utility model, in order to minimize the lateral movement range, the outer diameter of the circumferential limiting tube 7 is matched with the shaft hole of the turbine blade.
[0031] In one or more specific embodiments of this utility model, for better limiting, an axial limiting mechanism 8 is detachably connected to the upper end of the circumferential limiting tube 7. The axial limiting mechanism 8 includes a connecting tube 9 and a limiting cap 10 connected to its upper end. During storage, after the turbine blades are placed, the axial limiting mechanism 8 is connected to the circumferential limiting tube 7 to axially limit the turbine blades, thus preventing the turbine blades from moving upward and further avoiding the risk of collision.
[0032] In one or more specific embodiments of this utility model, the connecting pipe 9 is provided with external threads and the circumferential limiting pipe 7 is provided with internal threads. Through the threaded connection, the storage and retrieval of turbine blades can be quickly realized.
[0033] In one or more specific embodiments of this utility model, in order to obtain a more effective result, the diameter of the limiting cap 10 is not greater than the outer diameter of the wheel.
[0034] In one or more specific embodiments of this utility model, in order to prevent the coating of the stored high-precision turbine blades from oxidizing due to high temperature, the high-precision turbine blade storage device further includes an ambient temperature constant structure 11. The ambient temperature constant structure 11 includes a first pipe 12, a second pipe 13, a third pipe 14, a first elbow pipe 15, and a second elbow pipe 16. One end of the first elbow pipe 15 is connected to the first pipe 12, and the other end is connected to the second pipe 13. One end of the second elbow pipe 16 is connected to the remaining end of the second pipe 13, and the other end is connected to the third pipe 14. The first pipe 12 is installed on the lower surface of the first horizontal bar 1, the second pipe 13 is installed on the lower surface of the third horizontal bar 3, and the third pipe 14 is installed on the lower surface of the second horizontal bar 2. By setting the ambient temperature constant structure 11, when the temperature is abnormal, by introducing refrigerant into the ambient temperature constant structure 11, heat is dissipated not only from the parts of the high-precision turbine blades in contact with the first horizontal bar 1 and the second horizontal bar 2, but also from the shaft hole, which can effectively prevent the coating of the stored high-precision turbine blades from oxidizing due to high temperature.
[0035] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of this utility model, and are not intended to limit it. Although the utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art should understand that modifications can still be made to the technical solutions described in the foregoing embodiments, or equivalent substitutions can be made to some or all of the technical features therein. Such modifications or substitutions do not cause the essence of the corresponding technical solutions to deviate from the scope of the technical solutions of the embodiments of this utility model.
Claims
1. A high-precision turbine blade storage device, comprising a first horizontal bar (1), a second horizontal bar (2), a first connecting bar (5), a second connecting bar (6), and four load-bearing supports (4), characterized in that, The storage device also includes a third horizontal bar (3), which is located between the first horizontal bar (1) and the second horizontal bar (2). One end of the third horizontal bar (3) is connected to the first connecting bar (5), and the other end is connected to the second connecting bar (6). Several circumferential limiting tubes (7) are provided on the third horizontal bar (3) along the lateral direction. The distance between two adjacent circumferential limiting tubes (7) is greater than the circumferential dimension of the high-precision turbine blade.
2. The high-precision turbine blade storage device according to claim 1, characterized in that, The outer diameter of the circumferential limiting tube (7) is matched with the shaft hole of the turbine blade.
3. The high-precision turbine blade storage device of claim 1, wherein, The upper end of the circumferential limiting tube (7) is detachably connected to an axial limiting mechanism (8), which includes a connecting tube (9) and a limiting cap (10) connected to its upper end.
4. The high-precision turbine blade storage device according to claim 3, characterized in that, The connecting pipe (9) is provided with external threads, and the circumferential limiting pipe (7) is provided with internal threads.
5. The high-precision turbine blade storage device according to claim 3, characterized in that, The diameter of the limiting cap (10) is less than or equal to the outer diameter of the wheel.
6. The high-precision turbine blade storage device according to any one of claims 1 to 5, characterized in that The storage device also includes an ambient temperature constant structure (11).
7. The high-precision turbine blade storage device according to claim 6, characterized in that The constant ambient temperature structure (11) includes a first pipe (12), a second pipe (13), a third pipe (14), a first elbow pipe (15), and a second elbow pipe (16). One end of the first elbow pipe (15) is connected to the first pipe (12), and the other end is connected to the second pipe (13). One end of the second elbow pipe (16) is connected to the remaining end of the second pipe (13), and the other end is connected to the third pipe (14). The first pipe (12) is installed on the lower surface of the first horizontal bar (1), the second pipe (13) is installed on the lower surface of the third horizontal bar (3), and the third pipe (14) is installed on the lower surface of the second horizontal bar (2).