Micro-nano cooling liquid sprayer for precision machining of gas turbine blade

By designing a micro-nano-level coolant sprayer with a spray mechanism, a protective cover mechanism, and a locking mechanism, the problem of uneven coolant spraying was solved, achieving uniform cooling and lubrication of gas turbine blades and improving machining accuracy and efficiency.

CN224196449UActive Publication Date: 2026-05-05WUXI YEDAN MASCH MFG CO LTD
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
WUXI YEDAN MASCH MFG CO LTD
Filing Date
2025-05-19
Publication Date
2026-05-05

AI Technical Summary

Technical Problem

The existing coolant spraying is uneven, which cannot effectively cool and lubricate the precision machining area of ​​the gas turbine blades, affecting the machining quality and efficiency.

Method used

A micro-nano-scale coolant sprayer was designed, comprising a spraying mechanism, a protective cover mechanism, and a locking mechanism. The spraying mechanism sprays coolant in a micro-nano-scale mist form, the protective cover mechanism adjusts the spraying range, and the locking mechanism fixes the position of the cover, thereby achieving precise control of the coolant spraying range.

Benefits of technology

The uniform spraying of coolant ensures that the precision machining areas of the gas turbine blades are adequately cooled and lubricated, thereby improving machining accuracy and efficiency.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model relates to the technical field of gas turbine blade machining, and discloses a micro-nano cooling liquid sprayer for gas turbine blade precision machining, which comprises a mounting plate, a storage tank for storing cooling liquid is arranged at the top end of the mounting plate, and a spraying mechanism for spraying the cooling liquid is arranged at the bottom end of the storage tank. And a protective cover mechanism for controlling the spraying range of the cooling liquid is arranged at the bottom end of the spraying mechanism. Cooling liquid in the storage tank is extracted through the spraying mechanism, meanwhile, the cooling liquid is sprayed out in a micro-nano-scale mist form through the spraying mechanism, spraying can effectively cool and lubricate blades, the opening and closing degree of the protective cover mechanism is adjusted according to actual needs through the protective cover mechanism, and therefore the coverage area of spraying is controlled, and the cooling effect is improved. The locking mechanism is arranged to lock the protective cover mechanism, the opening and closing angles of the two cover bodies can be flexibly adjusted, different machining requirements are met, and the function of controlling the spraying range of cooling liquid is achieved.
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Description

Technical Field

[0001] This utility model relates to the field of gas turbine blade processing technology, specifically to a micro-nano level coolant sprayer for precision machining of gas turbine blades. Background Technology

[0002] In the precision machining of gas turbine blades, coolant is needed to cool and lubricate the machining area in order to ensure machining accuracy and blade surface quality. Traditional coolant supply methods are mostly pouring, which has problems such as large coolant consumption, uneven cooling, and difficulty in reaching the tiny gaps in precision machining. Moreover, for micro-nano-scale coolants, the pouring supply method cannot achieve uniform and efficient spraying, which affects the machining quality and efficiency of gas turbine blades.

[0003] Existing coolant sprayers cannot control the spray range of coolant during the precision machining of gas turbine blades, resulting in uneven coolant spraying. This leads to insufficient cooling and lubrication in some machining areas, while other areas may suffer from excessive coolant, affecting the machining effect. Therefore, those skilled in the art provide a micro-nano-scale coolant sprayer for the precision machining of gas turbine blades to solve the problems mentioned in the background art. Utility Model Content

[0004] The purpose of this invention is to provide a micro-nano level coolant sprayer for precision machining of gas turbine blades, which solves the problem of not being able to control the range of coolant spraying in the prior art.

[0005] This utility model provides the following technical solution: a micro-nano level coolant sprayer for precision machining of gas turbine blades, including a mounting plate, a storage tank for storing coolant is provided at the top of the mounting plate, a spraying mechanism for spraying coolant is provided at the bottom of the storage tank, a protective cover mechanism for controlling the spraying range of coolant is provided at the bottom of the spraying mechanism, and a locking mechanism for fixing the range of the protective cover mechanism is provided on the surface of the protective cover mechanism.

[0006] As a preferred embodiment of the above technical solution, the spraying mechanism includes a sprayer body installed at the bottom of the storage tank. The sprayer body is located at the bottom of the mounting plate. A hose is connected through the output end of the sprayer body. A connecting pipe is connected through the output end of the hose. A nozzle is connected through the output end of the connecting pipe.

[0007] As a preferred embodiment of the above technical solution, an installation sleeve is fixedly fitted on the surface of the bottom end of the hose, the installation sleeve is located above the connecting pipe, and a clamp is hinged to the end of the installation sleeve away from the hose.

[0008] As a preferred embodiment of the above technical solution, the protective cover mechanism includes two sets of covers hingedly mounted on the surface of the connecting pipe. The two sets of covers are located outside the nozzle, and telescopic plates are fixedly connected between the two sets of covers. A sleeve rod is hinged to the top of each set of covers.

[0009] As a preferred embodiment of the above technical solution, telescopic rods are slidably fitted onto the surfaces of both sets of sleeves, and locking holes are equidistantly opened on the surface of one set of sleeves. The ends of both sets of telescopic rods away from the two sets of sleeves are hinged to both sides of the surface of the hose through hinges.

[0010] As a preferred embodiment of the above technical solution, the locking mechanism includes a mounting post installed on the outer wall of one of the sets of telescopic rods, a spring being fitted on the surface of the mounting post, and a sleeve plate being slidably fitted on the surface of the mounting post, with the sleeve plate located on one side of the spring.

[0011] As a preferred embodiment of the above technical solution, a plug rod is fixedly installed at the end of the sleeve plate away from the mounting post, and the end of the plug rod away from the sleeve plate is inserted into the interior of one set of lock holes.

[0012] Compared with the prior art, the beneficial effects of this utility model are:

[0013] This invention utilizes a spray mechanism to draw coolant from a storage tank and simultaneously spray it out in a micro-nano mist format, effectively cooling and lubricating the blades. A protective cover mechanism allows for adjustment of the opening and closing angles to control the spray coverage area. A locking mechanism further secures the protective cover, enabling flexible adjustment of the opening angles of the two covers to meet various processing requirements. This design allows for control over the coolant spray range, preventing uneven spraying that could result in insufficient cooling and lubrication of certain processing areas. Attached Figure Description

[0014] Figure 1 This is a three-dimensional structural diagram of a micro-nano-scale coolant sprayer for precision machining of gas turbine blades;

[0015] Figure 2 This is a schematic diagram of the mounting sleeve structure in a micro-nano-scale coolant sprayer for precision machining of gas turbine blades;

[0016] Figure 3 This is a schematic diagram of the spray mechanism in a micro-nano-scale coolant sprayer for precision machining of gas turbine blades;

[0017] Figure 4 This is a schematic diagram of the sleeve rod in a micro-nano-scale coolant sprayer for precision machining of gas turbine blades;

[0018] Figure 5This is a schematic diagram of the locking mechanism in a micro / nano-scale coolant sprayer for precision machining of gas turbine blades.

[0019] Legend:

[0020] 1. Mounting plate; 2. Storage tank; 3. Spraying mechanism; 301. Sprayer body; 302. Hose; 303. Connecting pipe; 304. Nozzle; 4. Mounting sleeve; 401. Hoop; 5. Protective cover mechanism; 501. Cover body; 502. Telescopic plate; 503. Sleeve rod; 504. Telescopic rod; 505. Locking hole; 6. Locking mechanism; 601. Mounting column; 602. Spring; 603. Sleeve plate; 604. Insert rod. Detailed Implementation

[0021] The technical solutions of the present invention will be clearly and completely described below with reference to the accompanying drawings of the embodiments of the present invention.

[0022] Please see Figures 1-5 As shown, this utility model provides a technical solution: a micro-nano-level coolant sprayer for precision machining of gas turbine blades, including a mounting plate 1, a storage tank 2 for storing coolant at the top of the mounting plate 1, and a spraying mechanism 3 for spraying coolant at the bottom of the storage tank 2. The spraying mechanism 3 includes a sprayer body 301 installed at the bottom of the storage tank 2. The sprayer body 301 is located at the bottom of the mounting plate 1. A hose 302 is connected through the output end of the sprayer body 301. A connecting pipe 303 is connected through the output end of the hose 302. A nozzle 304 is connected through the output end of the connecting pipe 303.

[0023] The coolant in the storage tank 2 is drawn by the sprayer body 301 and transmitted to the connecting pipe 303 through the hose 302. Finally, it is sprayed out from the nozzle 304 in the form of micro-nano mist, which can effectively cool and lubricate the blades, thereby improving the processing accuracy and efficiency.

[0024] It should be noted that the model of the sprayer body 301 is YS-PBV-3000. The sprayer body 301 is existing technology and will not be described in detail here.

[0025] As one implementation method in this embodiment, please refer to Figure 1 and Figure 2 As shown, a mounting sleeve 4 is fixedly fitted on the bottom surface of the hose 302. The mounting sleeve 4 is located above the connecting pipe 303, and a clamp 401 is hinged to the end of the mounting sleeve 4 away from the hose 302.

[0026] The mounting sleeve 4 and the clamp 401 serve to fix and support the hose 302, ensuring that the hose 302 will not shake freely when transmitting coolant, thus guaranteeing the stability of the spray.

[0027] As one implementation method in this embodiment, please refer to Figure 1 , Figure 3 and Figure 4 As shown, the bottom end of the spray mechanism 3 is provided with a protective cover mechanism 5 for controlling the spray range of coolant. The protective cover mechanism 5 includes two sets of covers 501 hinged to the surface of the connecting pipe 303. The two sets of covers 501 are located outside the nozzle 304. A telescopic piece 502 is fixedly connected between the two sets of covers 501. A sleeve rod 503 is hinged to the top of each set of covers 501. A telescopic rod 504 is slidably fitted on the surface of each set of sleeve rods 503. Locking holes 505 are equidistantly opened on the surface of one set of sleeve rods 503. The ends of the two sets of telescopic rods 504 away from the two sets of sleeve rods 503 are hinged to both sides of the surface of the hose 302 through a hinge.

[0028] The two sets of covers 501 are connected by two sets of telescopic plates 502. The opening and closing degree of the two sets of covers 501 can be adjusted according to actual needs, thereby controlling the coverage area of ​​the spray. The sleeve rod 503 and telescopic rod 504 at the top of the two sets of covers 501 allow the two sets of covers 501 to be adjusted in the vertical direction to adapt to the needs of different processing angles.

[0029] As one implementation method in this embodiment, please refer to Figure 4 and Figure 5 As shown, the surface of the protective cover mechanism 5 is provided with a locking mechanism 6 for fixing the range of the protective cover mechanism 5. The locking mechanism 6 includes a mounting post 601 installed on the outer wall of one of the sets of telescopic rods 504. A spring 602 is fitted on the surface of the mounting post 601. A sleeve plate 603 is slidably fitted on the surface of the mounting post 601. The sleeve plate 603 is located on one side of the spring 602. A plug rod 604 is fixedly installed at the end of the sleeve plate 603 away from the mounting post 601. The end of the plug rod 604 away from the sleeve plate 603 is inserted into the interior of one of the sets of lock holes 505.

[0030] The engagement of the insert rod 604 with the locking hole 505 allows for the fixation of the telescopic rod 504, thereby stabilizing the opening and closing of the two sets of covers 501 and ensuring precise control of the spray range. The spring 602 provides elastic force to the sleeve plate 603 and the insert rod 604, enabling the insert rod 604 to smoothly insert into or pull out of the locking hole 505. By adjusting the engagement of the insert rod 604 with the locking holes 505 at different positions, the opening and closing angles of the two sets of covers 501 can be flexibly adjusted to meet different processing requirements.

[0031] Working principle: When the gas turbine blades need to be precision machined, the micro-nano-level coolant sprayer starts to work. First, the coolant in the storage tank 2 is drawn by the sprayer body 301 and transferred to the connecting pipe 303 through the hose 302. Finally, it is sprayed out from the nozzle 304 in the form of micro-nano-level mist, which can effectively cool and lubricate the blades, thereby improving the machining accuracy and efficiency. During the spraying process, the mounting sleeve 4 and the clamp 401 at the bottom of the hose 302 play a role in fixing and supporting, ensuring that the hose 302 will not shake randomly when transmitting coolant, thus ensuring the stability of the spray.

[0032] Meanwhile, the protective cover mechanism 5 at the bottom of the spray mechanism 3 can control the spray range of the coolant. The two sets of covers 501 are connected by two sets of telescopic plates 502. The opening and closing degree of the two sets of covers 501 can be adjusted according to actual needs, thereby controlling the coverage area of ​​the spray. The sleeve rod 503 and telescopic rod 504 at the top of the two sets of covers 501 allow the two sets of covers 501 to be adjusted in the vertical direction to adapt to the needs of different processing angles. After the positions of the two sets of covers 501 are adjusted, the telescopic rod 504 is fixed in the required position by inserting the insertion rod 604 into one of the locking holes 505 under the elastic force of the spring 602. This ensures the stability of the protective cover mechanism 5 and realizes precise control of the coolant spray range, providing strong support for the precision machining of gas turbine blades.

[0033] The above embodiments are only used to illustrate the technical solution of this utility model, and are not intended to limit it.

Claims

1. A micro / nano-scale coolant sprayer for precision machining of gas turbine blades, comprising a mounting plate (1), characterized in that: The top of the mounting plate (1) is provided with a storage tank (2) for storing coolant, the bottom of the storage tank (2) is provided with a spray mechanism (3) for spraying coolant, the bottom of the spray mechanism (3) is provided with a protective cover mechanism (5) for controlling the spray range of coolant, and the surface of the protective cover mechanism (5) is provided with a locking mechanism (6) for fixing the range of the protective cover mechanism (5).

2. The micro / nano-scale coolant sprayer for precision machining of gas turbine blades according to claim 1, characterized in that: The spraying mechanism (3) includes a sprayer body (301) installed at the bottom of the storage tank (2). The sprayer body (301) is located at the bottom of the mounting plate (1). A hose (302) is connected through the output end of the sprayer body (301). A connecting pipe (303) is connected through the output end of the hose (302). A nozzle (304) is connected through the output end of the connecting pipe (303).

3. The micro / nano-scale coolant sprayer for precision machining of gas turbine blades according to claim 2, characterized in that: The bottom end of the hose (302) is fixedly fitted with an installation sleeve (4), which is located above the connecting pipe (303). The end of the installation sleeve (4) away from the hose (302) is hinged with a clamp (401).

4. The micro / nano-scale coolant sprayer for precision machining of gas turbine blades according to claim 1, characterized in that: The protective cover mechanism (5) includes two sets of covers (501) hinged to the surface of the connecting pipe (303). The two sets of covers (501) are located outside the nozzle (304). A telescopic piece (502) is fixedly connected between the two sets of covers (501). A sleeve rod (503) is hinged to the top of each set of covers (501).

5. A micro / nano-scale coolant sprayer for precision machining of gas turbine blades according to claim 4, characterized in that: Both sets of sleeve rods (503) have telescopic rods (504) slidably fitted on their surfaces. One set of sleeve rods (503) has locking holes (505) equidistantly opened on its surface. The ends of both sets of telescopic rods (504) away from the two sets of sleeve rods (503) are hinged to both sides of the surface of the hose (302) through hinges.

6. The micro / nano-scale coolant sprayer for precision machining of gas turbine blades according to claim 1, characterized in that: The locking mechanism (6) includes a mounting post (601) installed on the outer wall of one of the telescopic rods (504), a spring (602) is fitted on the surface of the mounting post (601), and a sleeve plate (603) is slidably fitted on the surface of the mounting post (601), with the sleeve plate (603) located on one side of the spring (602).

7. A micro / nano-scale coolant sprayer for precision machining of gas turbine blades according to claim 6, characterized in that: A plug rod (604) is fixedly installed at one end of the sleeve plate (603) away from the mounting post (601), and the other end of the plug rod (604) away from the sleeve plate (603) is inserted into the interior of one set of lock holes (505).