Supporting and protecting device for vacuum arc ion plating of aero-engine blade

Abstract

The invention provides a supporting and protecting device for vacuum arc ion plating of an aero-engine blade, and relates to the field of vacuum arc ion plating of aero-engine blades. The device comprises a limiting block, a dust cover is movably connected to the left side surface of the lower end of the limiting block through a hinge, opening and closing devices are arranged at the front and rear ends, close to the upper end, of the dust cover, and a mounting device is arranged on the inner side surface of the limiting block. A torsional spring in the mounting device is arranged, so that the position of the blade body can be returned after the blade body is subjected to rotary coating, a limiting device is conveniently opened to take out the blade body, meanwhile, a limiting insertion piece is conveniently taken out from a circular block, and the taking and placing efficiency is improved; through the arrangement of the opening and closing device, the blade body can be closed more quickly, the possibility of pollution is reduced, through the arrangement of the clamping device and the opening and closing device, the blade body is quickly exposed for coating, the contact time of the blade part and the outside is shortened, and the possibility of pollution is reduced.

Description

Technical Field

[0001] The invention relates to the field of vacuum arc ion plating of aircraft engine blades, and in particular to a supporting and protecting device for vacuum arc ion plating of aircraft engine blades. Background Art

[0002] Vacuum arc ion plating is a method that uses high-voltage arc discharge to generate plasma, accelerates ions in a vacuum environment, and deposits them onto the surface of the substrate. For aircraft engine blades, metals, alloys, or ceramic materials are usually used as coating materials. The coating material is converted into ions by arc discharge, forming plasma and is accelerated and deposited onto the blade surface. In order to avoid the coating being deposited onto non-deposition surfaces such as the tenon of the aircraft blade during the vacuum arc ion plating process, the aircraft blade is unstable and the problem of touching the clean surface to be deposited during the clamping device occurs. Before the aircraft blade coating is prepared, the surface to be deposited on the aircraft blade needs to be cleaned and then placed in the coating equipment for coating.

[0003] When loading the blades into the coating equipment after cleaning, the problem of holding the clean blade body for loading often occurs, causing surface contamination and unqualified coating bonding strength. In addition, during the transfer process after cleaning, the external environment may cause contamination to the blade surface. Therefore, it is necessary to seek a new vacuum arc ion plating aviation blade protection device. Summary of the Invention

[0004] (1) Technical problems solved In view of the shortcomings of the existing technology, the present invention provides a support and protection device for vacuum arc ion plating of aircraft engine blades, which solves the problem of pollution caused by moving and taking out the blades.

[0005] (2) Technical solution To achieve the above objectives, the present invention is implemented through the following technical solutions: a support and protection device for vacuum arc ion plating of aircraft engine blades, comprising a limit block, the limit block is located at the left surface of the lower end and is movably connected to a dust cover through a hinge, the front and rear ends of the dust cover are provided with an opening and closing device near the upper end, the inner surface of the limit block is provided with a mounting device, the lower end of the limit block is fixedly connected to a magnetic plate, the upper end of the limit block is provided with a clamping device, the upper end of the mounting device is provided with a limit device, the inner side of the mounting device is installed with a blade body, the right end of the limit block is provided with a rotating device, the right end of the rotating device is fixedly connected to a rotating support rod, the lower end of the rotating support rod is rotatably connected to the mounting rod, and a magnet is installed inside the lower part of the dust cover.

[0006] The cam is connected to the second end of the second support rod and the second end of the second support rod is connected to the cam by the fixing mechanism, and the fixing mechanism can be adjusted accordingly. Preferably, the power assembly includes a first fixed plate, an arcuate tooth plate and a gear rod, the first fixed plate is fixedly connected to the front and rear sides of the limit block respectively, the arcuate tooth plate is fixedly connected to the inner surface of the first fixed plate, the gear rod is fixedly connected to the right end of the rotating rod passing through the second fixed plate, and the gear rod is meshed with the surface of the arcuate tooth plate. Preferably, the mounting device includes a limiting rotating disk, a rotating round rod, a torsion spring and a limiting plug-in. The rotating round rod is fixedly connected to the right end of the limiting rotating disk, the torsion spring is sleeved on the side surface of the rotating round rod, one end of the torsion spring is fixedly connected to the inner surface of the limiting block, and the other end of the torsion spring is fixedly connected to the inner surface of the limiting rotating disk. The right end of the rotating round rod passes through the right end of the limiting block and is fixedly connected to the left end of the limiting plug-in. The plug-in part is installed on the inner surface of the limiting rotating disk, and the position where the inner side of the limiting rotating disk contacts the plug-in part is made of rubber. Preferably, the blade body includes a blade portion and an insert portion, the right end of the blade portion is fixedly connected to the left end of the insert portion, and a plurality of limiting slots are provided on the surface of the insert portion.

[0007] Preferably, the limiting device includes a second opening and closing plate, a sliding rod, a limiting head and a sliding groove. The front end of the second opening and closing plate is movably connected to the upper surface of the limiting rotating disk through a hinge. The sliding rod is slidably connected to the inner surface of the second opening and closing plate. The sliding groove is arranged on the upper surface of the second opening and closing plate. The limiting head is fixedly connected to the lower end of the sliding rod. The lower end of the wrench above the sliding rod presses against the second opening and closing plate to limit the second opening and closing plate.

[0008] Preferably, the clamping device includes an inclined rod, an inclined block, a limiting plug plate, a sliding rod, a spring, an opening plate, a downward moving kit and a fixed plug plate, the inclined rod is provided with two and the left end is fixedly connected to the front and rear side surfaces of the dust cover respectively, the right end of the inclined rod is provided with an inclined surface and a limiting hole corresponding to the end of the sliding rod is provided near the inclined surface, the limiting plug plate is fixedly connected to the rear side surface of the inclined block, the inclined block is slidably connected to the inner side surface of the fixed plug plate through the limiting plug plate, the front end of the sliding rod is fixedly connected to the inner side surface of the inclined block, and the rear end of the sliding rod is slidably connected On the inner surface of the fixed plug plate, the spring is sleeved on the side surface of the sliding rod, the front end of the spring is fixedly connected to the inner surface of the inclined block, and the rear end of the spring is fixedly connected to the inner surface of the fixed plug plate. The right end of the inclined block is set with an inclined surface, and the right end of the downward moving kit is slidably sleeved on the side surface of the rotating support rod. The upper end of the support plate is fixedly connected to the lower surface of the downward moving kit, and the lower surface of the downward moving kit is provided with a first limiting groove corresponding to the fixed plug plate, and the lower end edges of the support plate are rotatably connected to rollers, and the rollers correspond to the inclined surfaces provided on the inclined block below.

[0009] Preferably, the rotating device includes a fixed cylinder, an annular gear plate, a gear, a circular block and a shell, the fixed cylinder is fixedly connected to the side surface of the rotating support rod, the right end of the gear is rotatably connected to the left surface of the fixed cylinder, the right end of the circular block is fixedly connected to the left surface of the gear, the interior of the circular block is provided with a second limiting groove corresponding to the limiting plug-in, the left end of the shell is provided with a third limiting groove corresponding to the lower end of the limiting block, the gear and the upper surface of the annular gear plate are meshed and connected, the upper surface of the annular gear plate is four sections, in which the tooth surface and the smooth surface are staggered, the annular gear plate is fixedly connected to the upper surface of the mounting rod and slidably connected to the inner surface of the shell.

[0010] (3) Beneficial effects The present invention provides a support and protection device for vacuum arc ion plating of aircraft engine blades. It has the following beneficial effects: 1. By setting the torsion spring in the installation device, the position of the blade body can be corrected after the blade body is rotary coated, which makes it convenient to open the limit device to remove the blade body. It is also convenient to remove the limit plug-in from the circular block, thereby improving the efficiency of removal and placement.

[0011] 2. After cleaning the blade body, the opening and closing device is set up and installed on the limit rotating disk. The dust cover is manually moved upward to cover the lower end of the blade body and the top end is covered by the first opening and closing plate at the same time, which can quickly close the blade body and reduce the possibility of contamination.

[0012] 3. Through the setting of the clamping device and the opening and closing device, the limit of the dust cover is released when the support plate is pressed down, so that it can move down quickly and cooperate with the magnetic plate to limit the dust cover, so that the blade body is quickly exposed for coating, which reduces the contact time of the blade with the outside world and reduces the possibility of contamination. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Figure 1 This is a schematic diagram of the overall structure of a support and protection device for vacuum arc ion plating of aircraft engine blades proposed by the present invention; Figure 2 This is a schematic diagram of the first internal structure of a support and protection device for vacuum arc ion plating of aircraft engine blades proposed by the present invention; Figure 3 This is a schematic diagram of the second internal structure of a support and protection device for vacuum arc ion plating of aircraft engine blades proposed by the present invention; Figure 4 This is a partial structural schematic diagram of a support and protection device for vacuum arc ion plating of aircraft engine blades proposed by the present invention; Figure 5 This is a schematic diagram of the first structure of an opening and closing device of a support and protection device for vacuum arc ion plating of aircraft engine blades proposed by the present invention; Figure 6 This is a schematic diagram of the second structure of the opening and closing device of the support and protection device for vacuum arc ion plating of aircraft engine blades proposed by the present invention; Figure 7 This is a schematic diagram of the structure of a power assembly of a support and protection device for vacuum arc ion plating of aircraft engine blades proposed by the present invention; Figure 8 This is a schematic structural diagram of an installation device for a support and protection device for vacuum arc ion plating of aircraft engine blades proposed by the present invention; Figure 9 This is a schematic diagram of the blade body structure of a support and protection device for vacuum arc ion plating of aircraft engine blades proposed by the present invention; Figure 10 This is a schematic structural diagram of a limiting device for a support and protection device for vacuum arc ion plating of aircraft engine blades proposed by the present invention; Figure 11 This is a schematic diagram of the first structure of a clamping device for a support and protection device for vacuum arc ion plating of aircraft engine blades proposed by the present invention; Figure 12 This is a schematic diagram of the second structure of a clamping device for a support and protection device for vacuum arc ion plating of aircraft engine blades proposed by the present invention; Figure 13This is a schematic structural diagram of a rotating device of a support and protection device for vacuum arc ion plating of aircraft engine blades proposed by the present invention.

[0014] Among them, 1. Dust cover; 2. Mounting rod; 3. Opening and closing device; 301. First opening and closing plate; 302. Push rod; 303. Moving rod; 304. Power assembly; 30401. First fixed plate; 30402. Arc tooth plate; 30403. Tooth rod; 305. Second fixed plate; 306. Short limit rod; 307. First connecting member; 308. Second connecting member; 309. Sliding groove; 310. Rotating rod; 4. Clamping device; 401. Inclined rod; 402. Inclined block; 403. Limiting plug plate; 404. Sliding rod; 405. Spring; 406. Opening plate; 407, downward moving kit; 408, fixed plug-in plate; 5, mounting device; 501, limiting rotating disk; 502, rotating round rod; 503, torsion spring; 504, limiting plug-in; 6, blade body; 601, blade part; 602, plug-in part; 7, limiting block; 8, rotating device; 801, fixed cylinder; 802, annular gear plate; 803, gear; 804, circular block; 805, outer shell; 9, limiting device; 901, second opening and closing plate; 902, sliding rod; 903, limiting head; 904, slide groove; 10, rotating support rod; 11, magnetic plate. DETAILED DESCRIPTION

[0015] The following will provide a clear and complete description of the technical solutions in the embodiments of the present invention in conjunction with the accompanying drawings. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. All other embodiments obtained by ordinary technicians in this field based on the embodiments of the present invention without making any creative efforts shall fall within the scope of protection of the present invention.

[0016] Example 1: like Figure 1-13 As shown, an embodiment of the present invention provides a support and protection device for vacuum arc ion plating of aircraft engine blades, including a limit block 7, the limit block 7 is located at the left surface of the lower end and is movably connected to a dust cover 1 through a hinge, the front and rear ends of the dust cover 1 are provided with an opening and closing device 3 near the upper end, the inner surface of the limit block 7 is provided with a mounting device 5, the lower end of the limit block 7 is fixedly connected to a magnetic plate 11, the upper end of the limit block 7 is provided with a clamping device 4, the upper end of the mounting device 5 is provided with a limit device 9, the inner side of the mounting device 5 is installed with a blade body 6, the right end of the limit block 7 is provided with a rotating device 8, the right end of the rotating device 8 is fixedly connected to a rotating support rod 10, the lower end of the rotating support rod 10 is rotatably connected to the mounting rod 2, and a magnet is installed inside the lower part of the dust cover 1.

[0017] The magnetic plate 11 is provided with a magnet plate inside and is attracted to the magnet installed inside the dust cover 1. The lower end of the mounting rod 2 and the upper end of the rotating support rod 10 can be provided with existing fixing components such as pins, bolts and other connection methods to fix them in the arc coating equipment.

[0018] The opening and closing device 3 includes a first opening and closing plate 301, a top rod 302, a moving rod 303, a power assembly 304, a second fixed plate 305, a limiting short rod 306, a first connecting member 307, a second connecting member 308, a sliding groove 309 and a rotating rod 310. The second fixed plate 305 is provided with two and is fixedly connected to the left and right ends of the dust cover 1 respectively. The sliding groove 309 is opened on the inner surface of the second fixed plate 305. The rotating rod 310 is rotatably connected to the inner surface of the second fixed plate 305. The two ends of the moving rod 303 are movably connected to the inner surface of the sliding groove 309. The side surfaces of the moving rod 303 are movably connected. The surface is rotatably connected to the inner surface of the top rod 302, the limiting short rod 306 is fixedly connected to the inner surface of the top rod 302, the top rod 302 is movably connected to the inner surface of the sliding groove 309 through the limiting short rod 306 and the moving rod 303, the first opening and closing plate 301 is fixedly connected to the upper end of the top rod 302, the first connecting member 307 is movably connected to the side surface of the moving rod 303, the second connecting member 308 is fixedly connected to the side surface of the power assembly 304, the first connecting member 307 and the second connecting member 308 are movably connected by a positioning pin, and the power assembly 304 is provided at the right end of the rotating rod 310. The first opening and closing plate 301 opens and closes by moving the part upward and then tilting outward so that it will not be caught by the second fixing plate 305 .

[0019] The power assembly 304 includes a first fixed plate 30401, an arc-shaped tooth plate 30402 and a gear rod 30403. The first fixed plate 30401 is fixedly connected to the front and rear sides of the limit block 7 respectively. The arc-shaped tooth plate 30402 is fixedly connected to the inner surface of the first fixed plate 30401. The gear rod 30403 is fixedly connected to the right end of the rotating rod 310 passing through the second fixed plate 305. The gear rod 30403 is meshed with the surface of the arc-shaped tooth plate 30402. The downward movement of the dust cover 1 can drive the gear rod 30403 to move on the arc-shaped gear plate 30402 and then drive the rotating rod 310 to rotate.

[0020] The mounting device 5 includes a limiting rotating disk 501, a rotating round rod 502, a torsion spring 503 and a limiting plug-in 504. The rotating round rod 502 is fixedly connected to the right end of the limiting rotating disk 501, and the torsion spring 503 is sleeved on the side surface of the rotating round rod 502. One end of the torsion spring 503 is fixedly connected to the inner surface of the limiting block 7, and the other end of the torsion spring 503 is fixedly connected to the inner surface of the limiting rotating disk 501. The right end of the rotating round rod 502 passes through the right end of the limiting block 7 and is fixedly connected to the left end of the limiting plug-in 504. The plug-in part 602 is installed on the inner surface of the limiting rotating disk 501, and the position where the inner side of the limiting rotating disk 501 contacts the plug-in part 602 is made of rubber.

[0021] The gap is reduced by setting the rubber inside the limiting rotating disk 501 to prevent arc ions from entering. The blade body 6 includes a blade portion 601 and an insert portion 602 . The right end of the blade portion 601 is fixedly connected to the left end of the insert portion 602 . A plurality of limiting slots are provided on the surface of the insert portion 602 .

[0022] The limiting device 9 includes a second opening and closing plate 901, a sliding rod 902, a limiting head 903 and a sliding groove 904. The front end of the second opening and closing plate 901 is movably connected to the upper surface of the limiting rotating disk 501 through a hinge. The sliding rod 902 is slidably connected to the inner surface of the second opening and closing plate 901. The sliding groove 904 is arranged on the upper surface of the second opening and closing plate 901. The limiting head 903 is fixedly connected to the lower end of the sliding rod 902. The lower end of the wrench above the sliding rod 902 presses against the second opening and closing plate 901 to limit the second opening and closing plate 901.

[0023] The arrangement of the slide bar 902 prevents the plug-in portion 602 from sliding out.

[0024] The clamping device 4 includes an inclined rod 401, an inclined block 402, a limiting plug plate 403, a sliding rod 404, a spring 405, a stretching plate 406, a downward moving kit 407 and a fixed plug plate 408. The inclined rod 401 is provided with two and the left end is fixedly connected to the front and rear side surfaces of the dust cover 1 respectively. The right end of the inclined rod 401 is provided with an inclined surface and a limiting hole corresponding to the end of the sliding rod 404 is provided near the inclined surface. The limiting plug plate 403 is fixedly connected to the rear side surface of the inclined block 402. The inclined block 402 is slidably connected to the inner surface of the fixed plug plate 408 through the limiting plug plate 403. The front end of the sliding rod 404 is fixedly connected to the inner surface of the inclined block 402. The rear end is slidably connected to the inner surface of the fixed plug plate 408, the spring 405 is sleeved on the side surface of the sliding rod 404, the front end of the spring 405 is fixedly connected to the inner surface of the inclined block 402, the rear end of the spring 405 is fixedly connected to the inner surface of the fixed plug plate 408, the right end of the inclined block 402 is set with an inclined surface, the right end of the downward moving kit 407 is slidably sleeved on the side surface of the rotating support rod 10, the upper end of the support plate 406 is fixedly connected to the lower surface of the downward moving kit 407, the lower surface of the downward moving kit 407 is provided with a first limiting groove corresponding to the fixed plug plate 408, and the lower end edge of the support plate 406 is rotatably connected with rollers, and the rollers correspond to the inclined surfaces set on the lower inclined block 402.

[0025] When the opening plate 406 moves downward, it will first release the limit on the inclined rod 401, and will continue to press down after the inclined rod 401 leaves.

[0026] The rotating device 8 includes a fixed cylinder 801, an annular gear plate 802, a gear 803, a circular block 804 and a shell 805. The fixed cylinder 801 is fixedly connected to the side surface of the rotating support rod 10. The right end of the gear 803 is rotatably connected to the left surface of the fixed cylinder 801. The right end of the circular block 804 is fixedly connected to the left surface of the gear 803. The interior of the circular block 804 is provided with a second limiting groove corresponding to the limiting plug-in 504. The left end of the shell 805 is provided with a third limiting groove corresponding to the lower end of the limiting block 7. The gear 803 is meshed with the upper surface of the annular gear plate 802. The upper surface of the annular gear plate 802 is four sections, in which the tooth surface and the smooth surface are staggered. The annular gear plate 802 is fixedly connected to the upper surface of the mounting rod 2 and is slidably connected to the inner surface of the shell 805.

[0027] The rotating device 8 and the clamping device 4 can be arranged in plurality around the rotating support rod 10 and can open the dust cover 1 synchronously to improve efficiency.

[0028] Working principle: After cleaning the blades, snap the plug-in part 602 into the inner part of the limiting rotating disk 501, and use the rubber material to block the gap to reduce the entry of arc ions. Then close the second opening and closing plate 901 through the hinge at the front end, and then put the limiting head 903 on the slide rod 902 into the bottom end along the slide groove 904, and then rotate the slide rod 902 to limit the second opening and closing plate 901 on the limiting rotating disk 501 to limit the plug-in part 602. Then manually close the dust cover 1. Lift up through the hinge on the right end, move the inclined surface of the inclined rod 401 at the upper end of the dust cover 1 to the inner side of the fixed insert plate 408 and push the sliding rod 404 into the fixed insert plate 408, so that the sliding rod 404 slides into the limiting hole on the inclined rod 401 through the action of the spring 405 to limit the dust cover 1. At the same time, the movement of the dust cover 1 drives the gear rod 30403 to move on the first fixed plate 30401, thereby closing the first opening and closing plate 301. If it needs to be transported later, Figure 4The whole is transported in the arc coating equipment. When arc coating is required, the limiting plug-in 504 is clamped in the circular block 804, and then the lower end of the mounting rod 2 and the upper end of the rotating support rod 10 are installed in the arc coating equipment. Then, the downward moving kit 407 is pressed down in the arc coating equipment to make the rollers on both sides of the support plate 406 contact the inclined surface set on the inclined surface block 402, thereby moving the inclined surface block 402 outward, and then driving the sliding rod 404 to move to release the limit on the inclined surface rod 401. At the same time, the limit is released, and the hinge connected to the right end of the dust cover 1 is used as a circle under the influence of the dust cover 1's own gravity. The center moves downward, and the dust cover 1 moves while driving the gear rod 30403 to move on the arc-shaped gear plate 30402, thereby driving the rotating rod 310 to rotate. The rotation of the rotating rod 310 drives the second connecting member 308 to move. The second connecting member 308 moves through the first connecting member 307 to drive the moving rod 303 to move upward in the sliding groove 309. The moving rod 303 moves upward and drives the limiting short rod 306 and the top rod 302 to move upward. Then, the moving rod 303 moves to the arc groove at the edge of the sliding groove 309, thereby driving the top rod 302 to tilt and then drive the first opening and closing plate 30 1 tilts outward to open the first opening and closing plate 301 to expose the blade body 6. At the same time, a magnet is installed under the dust cover 1. When the dust cover 1 moves down, it contacts the position of the magnetic plate 11 and is attracted to limit the dust cover 1. The downward moving kit 407 continues to move downward and moves below the upper slope of the inclined surface of the inclined surface block 402 to the top of the rollers on both sides of the support plate 406 to limit it to a certain extent. The groove on the downward moving kit 407 moves to the fixed plug-in plate 408 for nesting, further producing a limiting effect. Later, when coating is performed, the upper part of the rotating support rod 10 is installed at the output end of the motor. The lower end of the mounting rod 2 is fixedly installed. When the rotating support rod 10 rotates, the gear 803 on the rotating device 8 moves on the annular gear plate 802 and then drives the limiting plug-in 504 to rotate through the circular block 804. The limiting plug-in 504 rotates to drive the limiting rotating disk 501 to rotate, thereby driving the blade body 6 to rotate while rotating around the rotating support rod 10. When the gear 803 moves a distance of a tooth surface segment on the annular gear plate 802, the gear 803 is released from the limit on the smooth surface, and the blade body 6 is returned to its original position by the action of the torsion spring 503, and then the rotation is repeated to perform the coating operation.

[0029] While embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions, and variations may be made to these embodiments without departing from the principles and spirit of the invention, and that the scope of the invention is defined by the appended claims and their equivalents.

Claims

1. A support and protection device for vacuum arc ion plating of aircraft engine blades, comprising a limit block (7), characterized in that: The left side surface of the limit block (7) at the lower end is movably connected to the dust cover (1) through a hinge, and the front and rear ends of the dust cover (1) are provided with an opening and closing device (3) near the upper end. The inner surface of the limit block (7) is provided with a mounting device (5), and the lower end of the limit block (7) is fixedly connected to the magnetic plate (11), and the upper end of the limit block (7) is provided with a clamping device (4). The upper end of the mounting device (5) is provided with a limit device (9), and the inner side of the mounting device (5) is installed with a blade body (6). The right end of the limit block (7) is provided with a rotating device (8), and the right end of the rotating device (8) is fixedly connected to a rotating support rod (10). The lower end of the rotating support rod (10) is rotatably connected to the mounting rod (2), and a magnet is installed inside the lower part of the dust cover (1).

2. The support and protection device for vacuum arc ion plating of aircraft engine blades according to claim 1, characterized in that: The opening and closing device (3) comprises a first opening and closing plate (301), a top rod (302), a moving rod (303), a power assembly (304), a second fixed plate (305), a limiting short rod (306), a first connecting member (307), a second connecting member (308), a sliding groove (309) and a rotating rod (310), wherein two second fixed plates (305) are provided and are respectively fixedly connected to the left and right ends of the dust cover (1), the sliding groove (309) is provided on the inner surface of the second fixed plate (305), the rotating rod (310) is rotatably connected to the inner surface of the second fixed plate (305), the two ends of the moving rod (303) are movably connected to the inner surface of the sliding groove (309), and the moving rod (303) The side surface of the movable rod (303) is rotatably connected to the inner surface of the push rod (302), the limiting short rod (306) is fixedly connected to the inner surface of the push rod (302), the push rod (302) is movably connected to the inner surface of the sliding groove (309) through the limiting short rod (306) and the moving rod (303), the first opening and closing plate (301) is fixedly connected to the upper end of the push rod (302), the first connecting member (307) is movably connected to the side surface of the moving rod (303), the second connecting member (308) is fixedly connected to the side surface of the power assembly (304), the first connecting member (307) and the second connecting member (308) are movably connected via a positioning pin, and the power assembly (304) is provided at the right end of the rotating rod (310).

3. The support and protection device for vacuum arc ion plating of aircraft engine blades according to claim 2, characterized in that: The power assembly (304) comprises a first fixed plate (30401), an arcuate tooth plate (30402) and a gear rod (30403), wherein the first fixed plate (30401) is fixedly connected to the front and rear sides of the limit block (7), respectively, the arcuate tooth plate (30402) is fixedly connected to the inner surface of the first fixed plate (30401), and the gear rod (30403) is fixedly connected to the right end of the rotating rod (310) passing through the second fixed plate (305), and the gear rod (30403) is meshedly connected to the surface of the arcuate tooth plate (30402).

4. The support and protection device for vacuum arc ion plating of aircraft engine blades according to claim 1, characterized in that: The mounting device (5) comprises a limiting rotating disk (501), a rotating round rod (502), a torsion spring (503) and a limiting plug-in (504), wherein the rotating round rod (502) is fixedly connected to the right end of the limiting rotating disk (501), the torsion spring (503) is sleeved on the side surface of the rotating round rod (502), one end of the torsion spring (503) is fixedly connected to the inner surface of the limiting block (7), and the other end of the torsion spring (503) is fixedly connected to the inner surface of the limiting rotating disk (501), the right end of the rotating round rod (502) passes through the right end of the limiting block (7) and is fixedly connected to the left end of the limiting plug-in (504), and the plug-in part (602) is mounted on the inner surface of the limiting rotating disk (501), and the position where the inner side of the limiting rotating disk (501) contacts the plug-in part (602) is made of rubber.

5. The support and protection device for vacuum arc ion plating of aircraft engine blades according to claim 1, characterized in that: The blade body (6) comprises a blade portion (601) and an insert portion (602), the right end of the blade portion (601) is fixedly connected to the left end of the insert portion (602), and a plurality of limiting slots are provided on the surface of the insert portion (602).

6. The support and protection device for vacuum arc ion plating of aircraft engine blades according to claim 4, characterized in that: The limiting device (9) includes a second opening and closing plate (901), a sliding rod (902), a limiting head (903) and a sliding groove (904). The front end of the second opening and closing plate (901) is movably connected to the upper surface of the limiting rotating disk (501) through a hinge. The sliding rod (902) is slidably connected to the inner surface of the second opening and closing plate (901). The sliding groove (904) is arranged on the upper surface of the second opening and closing plate (901). The limiting head (903) is fixedly connected to the lower end of the sliding rod (902). The lower end of the wrench above the sliding rod (902) presses against the second opening and closing plate (901) to limit the second opening and closing plate (901).

7. The support and protection device for vacuum arc ion plating of aircraft engine blades according to claim 1, characterized in that: The clamping device (4) comprises an inclined rod (401), an inclined block (402), a limiting plug plate (403), a sliding rod (404), a spring (405), an opening plate (406), a downward moving kit (407) and a fixed plug plate (408), wherein the inclined rod (401) is provided with two and the left ends are respectively fixedly connected to the front and rear side surfaces of the dust cover (1), the right end of the inclined rod (401) is provided with an inclined surface and a limiting hole corresponding to the end of the sliding rod (404) is provided near the inclined surface, the limiting plug plate (403) is fixedly connected to the rear side surface of the inclined block (402), the inclined block (402) is slidably connected to the inner side surface of the fixed plug plate (408) through the limiting plug plate (403), the front end of the sliding rod (404) is fixedly connected to the inner side surface of the inclined block (402), and the sliding rod (40 4) is slidably connected to the inner surface of the fixed plug plate (408), the spring (405) is sleeved on the side surface of the sliding rod (404), the front end of the spring (405) is fixedly connected to the inner surface of the inclined block (402), the rear end of the spring (405) is fixedly connected to the inner surface of the fixed plug plate (408), the right end of the inclined block (402) is provided with an inclined surface, the right end of the downward moving kit (407) is slidably sleeved on the side surface of the rotating support rod (10), the upper end of the opening plate (406) is fixedly connected to the lower surface of the downward moving kit (407), the lower surface of the downward moving kit (407) is provided with a first limiting groove corresponding to the fixed plug plate (408), and the lower end edge of the opening plate (406) is rotatably connected to a roller, and the roller corresponds to the inclined surface provided on the lower inclined block (402).

8. The support and protection device for vacuum arc ion plating of aircraft engine blades according to claim 4, characterized in that: The rotating device (8) comprises a fixed cylinder (801), an annular gear plate (802), a gear (803), a circular block (804) and a housing (805), wherein the fixed cylinder (801) is fixedly connected to the side surface of the rotating support rod (10), the right end of the gear (803) is rotatably connected to the left side surface of the fixed cylinder (801), the right end of the circular block (804) is fixedly connected to the left side surface of the gear (803), and the inner surface of the circular block (804) is fixedly connected to the left side surface of the gear (803). The upper portion of the housing (805) is provided with a second limiting groove corresponding to the limiting plug-in (504), and the left end of the housing (805) is provided with a third limiting groove corresponding to the lower end of the limiting block (7). The gear (803) and the upper surface of the annular toothed plate (802) are meshed and connected. The upper surface of the annular toothed plate (802) is divided into four sections, in which the toothed surface and the smooth surface are staggered. The annular toothed plate (802) is fixedly connected to the upper surface of the mounting rod (2) and is slidably connected to the inner surface of the housing (805).

Images