CN216590986U

CN216590986U - Composite material forming tool for aviation

Info

Publication number: CN216590986U
Application number: CN202220053997.7U
Authority: CN
Inventors: 阮理数; 李宏军
Original assignee: Xi'an Ruixin Aviation Technology Co ltd
Current assignee: Xi'an Ruixin Aviation Technology Co ltd
Priority date: 2022-01-07
Filing date: 2022-01-07
Publication date: 2022-05-24
Anticipated expiration: 2032-01-07

Abstract

The utility model relates to a frock technical field specifically is a combined material shaping frock for aviation, including operation panel, base, cylinder, transmission shaft, depression bar, mould and lubricating arrangement, the lower fixed surface of base and operation panel is connected, and the fixed surface of cylinder and operation panel is connected, and the transmission shaft is connected with the surface transmission of cylinder, and the depression bar rotates with the surface of transmission shaft to be connected, and the mould is placed on the surface of operation panel, and the depression bar is connected with mould surface centre gripping, and lubricating arrangement sets up on the operation panel surface, and lubricating arrangement includes the bracing piece, and the bracing piece is connected with the fixed surface of operation panel. The utility model discloses, through setting up lubricating arrangement, be convenient for lubricate the depression bar fast, avoid most depression bars wearing and tearing to appear in long-time use, the user is difficult to maintain it, easily causes its the condition that the card dun can't be used that appears, and then reduces the fault rate of frock, improves its stability.

Description

Composite material forming tool for aviation

Technical Field

The utility model relates to a frock technical field especially relates to an aeronautical combined material shaping frock.

Background

The shaping frock can be applied to the shaping of multiple combined material spare part for the aviation, and the operation is convenient, and simple structure is easy to carry out, nevertheless because current equipment adds man-hour and need use cylinder and depression bar to carry out the centre gripping to the frock, and wearing and tearing appear in the long-time use of most depression bars, the user is difficult to maintain it, easily causes its the unable condition of using of card pause to appear, increases the fault rate of frock, reduces its stability, improves this needs.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving the defects existing in the prior art and providing a composite material forming tool for aviation.

In order to achieve the above purpose, the utility model adopts the following technical scheme: the utility model provides a combined material shaping frock for aviation, includes operation panel, base, cylinder, transmission shaft, depression bar, mould and lubricating arrangement, the lower fixed surface of base and operation panel is connected, the fixed surface of cylinder and operation panel is connected, the transmission shaft is connected with the surface transmission of cylinder, the depression bar rotates with the surface of transmission shaft to be connected, the mould is placed on the surface of operation panel, the depression bar is connected with mould surface centre gripping, lubricating arrangement sets up on the operation panel surface, lubricating arrangement includes the bracing piece, the bracing piece is connected with the fixed surface of operation panel.

Preferably, the upper surface of the supporting rod is fixedly connected with a cross rod, the surface of the cross rod is fixedly connected with a power motor, a driving end of the power motor is fixedly connected with a guide wheel, and the guide wheel is rotatably connected with the surface of the cross rod.

Preferably, the surface of the guide wheel is in transmission connection with a rotating belt, the surface of the rotating belt is fixedly connected with a moving rod, the moving rod is located above the operating platform, and the inner wall of the moving rod is in sliding connection with an oil tank.

Preferably, the lower surface of the oil tank is connected with an oil guide pipe in a sliding manner, one end of the oil guide pipe, which is far away from the oil tank, is fixedly connected with an extension spring, and one end of the extension spring, which is far away from the oil guide pipe, is fixedly connected with the lower surface of the oil tank.

Preferably, a separating device is arranged on the surface of the operating platform and comprises a jack, an ejector rod is connected to the surface of the jack in a transmission mode, a bottom plate is fixedly connected to the surface of the ejector rod, and the bottom plate abuts against the lower surface of the mold.

Preferably, the inner wall sliding connection of bottom plate has the connecting rod, the one end fixedly connected with connecting block of bottom plate is kept away from to the connecting rod, the one end fixedly connected with fixture block of connecting rod is kept away from to the connecting block, the one end of fixture block and the surperficial joint of mould.

Preferably, one side fixedly connected with fixed spring that the connecting rod is close to each other, the inner wall fixedly connected with stabilizing spring of bottom plate, stabilizing spring keeps away from the one end fixedly connected with bolt of bottom plate, stabilizing spring's one end and the surface joint of connecting block are kept away from to the bolt.

Compared with the prior art, the utility model discloses an advantage lies in with positive effect:

1. the utility model discloses in, through setting up lubricating arrangement, open motor power, the guide pulley atress will change the area simultaneously and drive rotatoryly, the carriage release lever atress in succession removes, when the oil tank reachs the depression bar top, oil pipe is led in the pulling, extension spring atress deformation back expansion simultaneously, lubricating oil is through leading oil pipe filling transmission shaft surface immediately, through setting up lubricating arrangement, be convenient for lubricate the depression bar fast, avoid wearing and tearing to appear in the long-time use of most depression bars, the user is difficult to maintain it, easily cause its the condition that the card pause can't be used that appears, and then reduce the fault rate of frock, improve its stability.

Drawings

Fig. 1 is a schematic perspective view of the composite material forming tool for aviation of the present invention;

FIG. 2 is a schematic view of a main structure of a lubricating device in the composite material forming tool for aviation;

FIG. 3 is a schematic view of an exploded structure of a lubricating device in the composite material forming tool for aviation;

FIG. 4 is a schematic view of a main structure of a separating device in the composite material forming tool for aviation of the present invention;

fig. 5 is the utility model provides a separator's decomposition structure schematic diagram in combined material shaping frock for aviation.

Illustration of the drawings:

1. an operation table; 2. a base; 3. a cylinder; 4. a drive shaft; 5. a pressure lever; 6. a mold; 7. a lubricating device; 71. a support bar; 72. a cross bar; 73. a power motor; 74. a guide wheel; 75. rotating the belt; 76. a travel bar; 77. an oil tank; 78. an oil guide pipe; 79. an extension spring; 8. a separation device; 81. a jack; 82. a top rod; 83. a base plate; 84. a connecting rod; 85. connecting blocks; 86. a clamping block; 87. fixing the spring; 88. a stabilizing spring; 89. and (4) a bolt.

Detailed Description

Referring to fig. 1-5, the present invention provides a technical solution: the utility model provides a combined material shaping frock for aviation, including operation panel 1, base 2, cylinder 3, transmission shaft 4, depression bar 5, mould 6 and lubricating arrangement 7, base 2 and operation panel 1's lower fixed surface is connected, cylinder 3 and operation panel 1's fixed surface is connected, transmission shaft 4 is connected with cylinder 3's surface transmission, depression bar 5 rotates with transmission shaft 4's surface to be connected, mould 6 places the surface at operation panel 1, depression bar 5 is connected with 6 surperficial centre gripping of mould, lubricating arrangement 7 sets up on operation panel 1 surface.

The specific arrangement and function of the lubricating device 7 and the separating device 8 will be described in detail below.

In this embodiment: the lubricating device 7 comprises a supporting rod 71, the supporting rod 71 is fixedly connected with the surface of the operating platform 1, a cross rod 72 is fixedly connected to the upper surface of the supporting rod 71, a power motor 73 is fixedly connected to the surface of the cross rod 72, a guide wheel 74 is fixedly connected to the driving end of the power motor 73, and the guide wheel 74 is rotatably connected with the surface of the cross rod 72 and is matched with a rotating belt 75 through the power motor 73, so that the moving rod 76 can be controlled to move back and forth conveniently.

Specifically, a rotating belt 75 is connected to the surface of the guide wheel 74 in a transmission manner, a moving rod 76 is fixedly connected to the surface of the rotating belt 75, the moving rod 76 is located above the operating platform 1, an oil tank 77 is connected to the inner wall of the moving rod 76 in a sliding manner, and the oil tank 77 can conveniently slide to the upper surface of the transmission shaft 4 needing lubrication at any time by arranging the moving rod 76.

Specifically, the lower surface of the oil tank 77 is slidably connected with an oil guide pipe 78, one end of the oil guide pipe 78, which is far away from the oil tank 77, is fixedly connected with an extension spring 79, one end of the extension spring 79, which is far away from the oil guide pipe 78, is fixedly connected with the lower surface of the oil tank 77, and lubricating oil is conveniently and accurately injected to the surface of the compression bar 5 by the matching of the extension spring 79 and the oil guide pipe 78.

Specifically, the surface of operation panel 1 is provided with separator 8, and separator 8 includes jack 81, and the surface transmission of jack 81 is connected with ejector pin 82, and the fixed surface of ejector pin 82 is connected with bottom plate 83, and bottom plate 83 offsets with the lower surface of mould 6, through setting up jack 81 and ejector pin 82, is convenient for with mould 6 and operation panel 1 quick separation.

Specifically, the inner wall sliding connection of bottom plate 83 has connecting rod 84, and the one end fixedly connected with connecting block 85 of bottom plate 83 is kept away from to connecting rod 84, and the one end fixedly connected with fixture block 86 of connecting rod 84 is kept away from to connecting block 85, and the one end of fixture block 86 and the surperficial joint of mould 6 are convenient for be connected mould 6 and bottom plate 83 steady, and mould 6 drops when avoiding separating through setting up fixture block 86 and fixed spring 87's cooperation.

Specifically, one side fixedly connected with fixed spring 87 that connecting rod 84 is close to each other, the inner wall fixedly connected with stabilizing spring 88 of bottom plate 83, the one end fixedly connected with bolt 89 of bottom plate 83 is kept away from to stabilizing spring 88, and the one end that stabilizing spring 88 was kept away from to bolt 89 is connected with the surface joint of connecting block 85.

In this embodiment: through the cooperation that sets up stabilizing spring 88 and bolt 89, be convenient for further fix connecting block 85, further strengthen being connected between mould 6 and the bottom plate 83.

The working principle is as follows: by arranging the lubricating device 7, turning on the power motor 73, simultaneously applying force to the guide wheel 74 to drive the rotating belt 75 to rotate, sequentially applying force to move the moving rod 76, pulling the oil guide pipe 78 when the oil tank 77 reaches the upper part of the pressure lever 5, simultaneously applying force to deform and then expanding the extension spring 79, immediately filling lubricating oil into the surface of the transmission shaft 4 through the oil guide pipe 78, conveniently and quickly lubricating the pressure lever 5 by arranging the lubricating device 7, avoiding abrasion of most pressure levers 5 in long-time use, difficulty in maintenance of the pressure levers by a user, easy blockage and incapability of the pressure levers, further reducing the fault rate of the tool, improving the stability of the tool, and by arranging the separating device 8, pulling the bolt 89, simultaneously applying force to tighten the stabilizing spring 88, sequentially applying force to separate the bolt 89 from the surface of the connecting block 85, immediately pulling the connecting block 85, and sequentially applying force to pull the fixing spring 87 to deform, the fixture blocks 86 are simultaneously stressed to be away from the die 6, the die 6 is immediately placed on the surface of the bottom plate 83, the connecting blocks 85 are immediately loosened, the fixing springs 87 rebound after losing constraint successively, the connecting rods 84 are pulled, the fixture blocks 86 are simultaneously stressed to be inserted into the surface of the die 6, after machining is completed, the jacks 81 are opened, the ejector rods 82 are simultaneously stressed to lift the die 6, and the separating device 8 is arranged, so that the die 6 can be conveniently and quickly separated, the work load of a user is reduced, the production efficiency of equipment is improved, and the economic benefit of the user is improved.

Claims

1. The utility model provides a combined material shaping frock for aviation, includes operation panel (1), base (2), cylinder (3), transmission shaft (4), depression bar (5), mould (6) and lubricating arrangement (7), its characterized in that: the base (2) is fixedly connected with the lower surface of the operating platform (1), the cylinder (3) is fixedly connected with the surface of the operating platform (1), the transmission shaft (4) is in transmission connection with the surface of the cylinder (3), the pressure lever (5) is in rotation connection with the surface of the transmission shaft (4), the die (6) is placed on the surface of the operating platform (1), the lubricating device (7) is arranged on the surface of the operating platform (1), the lubricating device (7) comprises a supporting rod (71), the supporting rod (71) is fixedly connected with the surface of the operating platform (1), the upper surface of the supporting rod (71) is fixedly connected with a cross rod (72), the surface of the cross rod (72) is fixedly connected with a power motor (73), the driving end of the power motor (73) is fixedly connected with a guide wheel (74), and the guide wheel (74) is rotatably connected with the surface of the cross rod (72).

2. The composite material molding tool for aviation as claimed in claim 1, wherein: the surface of the guide wheel (74) is connected with a rotating belt (75) in a transmission way, and the surface of the rotating belt (75) is fixedly connected with a moving rod (76).

3. The composite material molding tool for aviation as claimed in claim 2, wherein: the moving rod (76) is positioned above the operating platform (1), and an oil tank (77) is connected to the inner wall of the moving rod (76) in a sliding manner.

4. The composite material molding tool for aviation as claimed in claim 3, wherein: the lower surface sliding connection of oil tank (77) has oil pipe (78), the one end fixedly connected with extension spring (79) that oil pipe (78) kept away from oil tank (77), the one end that oil pipe (78) was kept away from in extension spring (79) is connected with the lower surface fixed connection of oil tank (77).

5. The composite material molding tool for aviation as claimed in claim 1, wherein: the surface of operation panel (1) is provided with separator (8), separator (8) include jack (81), the surface transmission of jack (81) is connected with ejector pin (82), the fixed surface of ejector pin (82) is connected with bottom plate (83).

6. The composite material molding tool for aviation as claimed in claim 5, wherein: the inner wall sliding connection of bottom plate (83) has connecting rod (84), the one end fixedly connected with connecting block (85) of bottom plate (83) are kept away from in connecting rod (84), one end fixedly connected with fixture block (86) of connecting rod (84) are kept away from in connecting block (85), the one end of fixture block (86) and the surface joint of mould (6).

7. The composite material molding tool for aviation as claimed in claim 6, wherein: one side fixedly connected with fixed spring (87) that connecting rod (84) are close to each other, inner wall fixedly connected with stabilizing spring (88) of bottom plate (83), the one end fixedly connected with bolt (89) of bottom plate (83) are kept away from in stabilizing spring (88), the surface joint of the one end of stabilizing spring (88) and connecting block (85) is kept away from in bolt (89).