Automatic cutting device for preformed foam inner core of aero seat

Abstract

The utility model discloses an automatic cutting device for a preformed foam inner core of an aero seat. The automatic cutting device comprises a rack, the forming frame is arranged on the rack, and the interior of the forming frame can be connected with a foam plate; the driving mechanism is arranged on the rack; the cutting mechanism is connected to the output end of the driving mechanism and comprises a thermal fuse, and the thermal fuse is attached to the outer wall of the forming frame; and the cutting mechanism is driven by the driving mechanism to keep reciprocating motion, so that the thermal fuse is attached to the outer wall of the forming frame to move. According to the automatic cutting device for the preformed foam inner core of the aero seat, the cutting mechanism is driven by the driving mechanism to keep sliding, so that the thermal fuse on the cutting mechanism moves along the forming frame, the thermal fuse abuts against a foam board connected with the interior of the forming frame in the moving process, the foam board is cut into the shape of the edge of the forming frame, and the cutting efficiency is improved. According to the cutting device, a foam plate in a special shape can be preliminarily cut, so that subsequent secondary cutting is facilitated, and the production efficiency of producing a foam core material in a special shape can be improved.

Description

TECHNICAL FIELD

[0001] The utility model relates to aviation seat production technical field, concretely relates to an aviation seat preform foam inner core automatic cutting device. BACKGROUND

[0002] The aviation seat or the high speed rail seat is usually made of carbon fiber material, utilizes the characteristics that carbon fiber material has light weight and high hardness, and is made into the aviation seat or the high speed rail seat, can reduce the whole machine weight. In the carbon fiber seat production process, especially the rib part of the seat back, it is hollow inside, and when producing, the carbon fiber cloth needs to be wrapped outside the foam core material according to the shape of the foam core material, and after fixing, the foam core material inside is taken out, and finally the carbon fiber rib with hollow inside is made.

[0003] According to the invention patent application with publication number CN110561554A and publication date of December 13, 2019, a kind of foam board hot cutting device is disclosed, including base and the feeding platform of base setting, the upper portion of base is connected with the F-shaped support of symmetrical distribution through slide rail, the upper end of this F-shaped support is installed with speed reducer respectively, and the lower end horizontal part is fixed with electric heating device respectively, and the upper and lower horizontal parts are connected with shaft respectively through bearing;The upper end of the shaft is connected with the output end of speed reducer, and the shaft surface is provided with annular groove of uniform distribution;Between the shaft, a plurality of electric heating wires are connected in cooperation;The contact part of electric heating wire and shaft is located in annular groove, and is connected with electric heating device by electric connection mode.The main technical effect is: it can improve cutting quality, safe and reliable.

[0004] When cutting the foam core material, since the overall shape of the rib has a certain arc, the core material inside it should also have a certain arc to ensure that the rib produced finally has a certain arc, so when producing, the foam board needs to be cut first, so that one side has a certain arc, for this purpose, an aviation seat preform foam inner core automatic cutting device is proposed, which aims to provide a device for conveniently and conveniently cutting foam board with arc. UTILITY MODEL CONTENTS

[0005] The utility model aims at providing an aviation seat preform foam inner core automatic cutting device, which aims at providing a device for conveniently and conveniently cutting foam board with arc.

[0006] In order to achieve the above-mentioned purpose, the utility model provides the following technical scheme:

[0007] The aviation seat preform foam inner core automatic cutting device comprises a rack, and further comprises:

[0008] A forming frame is arranged on the rack, and the forming frame is internally connectable with a foam board.

[0009] The driving mechanism is arranged on the frame;

[0010] The cutting mechanism is connected to the output end of the driving mechanism, and the cutting mechanism comprises a hot fuse which is attached to the outer wall of the forming frame.

[0011] The cutting mechanism is driven by the driving mechanism to keep reciprocating movement, so that the hot fuse moves while being attached to the outer wall of the forming frame.

[0012] Preferably, the forming frame comprises a plurality of fixing strips and a plurality of forming strips, and the fixing strips and the forming strips are sequentially connected to form a frame-shaped structure.

[0013] Preferably, the suction mechanism is arranged inside the frame, the frame is fixedly provided with a fixed plate, the fixed plate is provided with a ventilation hole, the suction mechanism comprises a suction pump, a connecting pipeline and a suction box, the suction box is fixedly installed on the fixed plate, the ventilation hole is in communication with the suction box, one end of the connecting pipeline is in communication with the suction box, and the other end of the connecting pipeline is in communication with the suction pump.

[0014] Preferably, the cutting mechanism comprises a mounting beam, the number of the driving mechanisms is two, the two driving mechanisms are arranged on the two sides of the forming frame respectively, and the two ends of the mounting beam are fixedly connected to the output ends of the two driving mechanisms.

[0015] Preferably, the cutting mechanism further comprises a first mounting plate and a second mounting plate, the mounting beam is slidably connected with a first connecting screw and a second connecting screw, the first mounting plate and the second mounting plate are slidably connected to the mounting beam, one end of the hot fuse is connected to the first mounting plate, and the other end of the hot fuse is connected to the second mounting plate.

[0016] Preferably, the first mounting plate and the second mounting plate are provided with sliding blocks at the ends thereof, the sliding blocks are provided with fastening screws, one end of the hot fuse is connected to the fastening screw on the first mounting plate, the second mounting plate is provided with a tension spring, and the other end of the hot fuse is connected to the tension spring by passing through the fastening screw on the second mounting plate.

[0017] Preferably, the first mounting plate and the second mounting plate are provided with sliding blocks at the ends thereof, the sliding blocks are provided with fastening screws, one end of the hot fuse is connected to the fastening screw on the first mounting plate, the second mounting plate is provided with a tension spring, and the other end of the hot fuse is connected to the tension spring by passing through the fastening screw on the second mounting plate.

[0018] In the above technical scheme, the aviation seat preform foam inner core automatic cutting device has the following beneficial effects:

[0019] The utility model discloses, through drive mechanism drive cutting mechanism keeps sliding, make hot fuse on cutting mechanism along the forming frame movement, with the foamed board of connecting in the process of hot fuse movement, abuts, cut the foamed board into the shape of forming frame edge, can realize to the foamed board of special shape preliminary cutting, in order to facilitate subsequent secondary cutting, can improve the production efficiency of the production special shape foamed core material. BRIEF DESCRIPTION OF DRAWINGS

[0020] In order to more clearly illustrate the technical scheme in the embodiments of the present application or prior art, the drawings needed to be used in the embodiments will be briefly introduced as follows. Obviously, the drawings in the following description only some embodiments of the utility model are recorded, and other drawings can also be obtained according to these drawings for the ordinary skilled in the art.

[0021] Figure 1 The overall structure schematic diagram provided by the embodiments of the utility model is shown in the drawings.

[0022] Figure 2 The cutting mechanism structure schematic diagram provided by the embodiments of the utility model is shown in the drawings.

[0023] Figure 3 The hot fuse installation position schematic diagram provided by the embodiments of the utility model is shown in the drawings.

[0024] Figure 4 The A place enlarged structure schematic diagram provided by the embodiments of the utility model is shown in the drawings.

[0025] Figure 5 The drive mechanism structure schematic diagram provided by the embodiments of the utility model is shown in the drawings.

[0026] Figure 6 The forming frame structure schematic diagram provided by the embodiments of the utility model is shown in the drawings.

[0027] Figure 7 The adsorption structure installation position structure schematic diagram provided by the embodiments of the utility model is shown in the drawings.

[0028] Explanation of reference signs:

[0029] 1, rack; 11, fixed plate; 12, vent hole; 2, forming frame; 21, fixed strip; 22, forming strip; 23, arc surface; 3, drive mechanism; 31, drive motor; 32, screw; 33, mounting seat; 34, guide rod; 35, sliding block; 4, cutting mechanism; 41, hot fuse; 42, mounting beam; 43, first mounting plate; 44, second mounting plate; 45, first connecting screw; 46, second connecting screw; 47, sliding block; 48, fastening screw; 49, tension spring; 5, adsorption mechanism; 51, suction pump; 52, connecting pipeline; 53, suction box. DETAILED DESCRIPTION

[0030] In order to make the technical personnel of the prior art better understand the technical scheme of the utility model, the utility model will be described in further detail below with reference to the drawings.

[0031] Please refer to Figure 1 7, the automatic cutting device of aviation seat preform foam inner core, including frame 1, still including:

[0032] The forming frame 2 is arranged on the frame 1, and the foam plate can be connected inside the forming frame 2;

[0033] The driving mechanism 3 is arranged on the frame 1;

[0034] The cutting mechanism 4 is connected to the output end of the driving mechanism 3, and the cutting mechanism 4 includes a hot melt wire 41, and the hot melt wire 41 is attached to the outer wall of the forming frame 2;

[0035] The cutting mechanism 4 is driven by the driving mechanism 3 to keep reciprocating motion, so that the hot melt wire 41 attached to the outer wall of the forming frame 2 moves.

[0036] Specifically, the forming frame 2 is fixedly installed on the frame 1, and the forming frame 2 is a hollow structure, which can be used to place the foam plate to be cut. In use, the foam plate to be cut is placed in the forming frame 2, and the size of the foam plate is preferably matched with the size of the forming frame 2, so that the foam plate can be simply positioned.

[0037] The driving mechanism 3 is arranged on the frame 1, and the cutting mechanism 4 is connected to the output end of the driving mechanism 3. The cutting mechanism 4 includes a hot melt wire 41. In use, the cutting mechanism 4 is driven by the driving mechanism 3 to keep reciprocating motion on the frame 1, so that the hot melt wire 41 keeps moving along the outer wall of the forming frame 2. The hot melt wire 41 keeps moving and abuts against the foam plate in the forming frame 2. The foam plate is cut by abutting against the hot melt wire 41. Since the hot melt wire 41 is attached to the outer wall of the forming frame 2 during movement, the foam plate can be cut into a plate with the same shape as the side wall of the forming frame 2, which is convenient for subsequent slitting.

[0038] The utility model discloses a driving mechanism 3 drives the cutting mechanism 4 to keep sliding, so that the hot melt wire 41 on the cutting mechanism 4 moves along the forming frame 2. During the movement of the hot melt wire 41, the foam plate connected inside the forming frame 2 abuts, and the foam plate is cut into the shape of the edge of the forming frame 2. The special-shaped foam plate can be preliminarily cut, so that subsequent secondary cutting is facilitated, and the production efficiency of special-shaped foam core material can be improved.

[0039] As an embodiment provided by the utility model, Figure 6As shown, the forming frame 2 includes a fixing strip 21 and a forming strip 22. There are several fixing strips 21 and forming strips 22. The fixing strips 21 and forming strips 22 are connected in sequence to form a frame structure.

[0040] Specifically, there are two fixing strips 21 and two forming strips 22. The two ends of the two fixing strips 21 are respectively connected to the two ends of the two forming strips 22. That is, the fixing strips 21 and the forming strips 22 are connected in sequence to form a frame structure with a hollow interior, which is used to accommodate foam boards of a certain size.

[0041] Preferably, an arc-shaped surface 23 is provided on the outer wall of the forming strip 22. The arc-shaped surface 23 can be designed according to production requirements. When it is necessary to produce a completely straight rib, the arc-shaped surface 23 can be a planar structure, which is convenient for producing different types of ribs.

[0042] As an embodiment of this utility model, it also includes an adsorption mechanism 5 disposed inside the frame 1. A fixed plate 11 is fixedly installed on the frame 1. The forming frame 2 and the driving mechanism 3 are both disposed on the fixed plate 11. A ventilation hole 12 is provided on the outer wall of the fixed plate 11. Preferably, the ventilation hole 12 is located on the fixed plate 11 and inside the forming frame 2. The adsorption mechanism 5 includes a suction pump 51, a connecting pipe 52, and a suction box 53. The suction pump 51 is fixedly installed inside the frame 1. The suction box 53 is fixedly installed at the bottom of the fixed plate 11 and is connected to the ventilation hole 12, that is, the suction box 53 is connected to the outside through the ventilation hole 12. One end of the connecting pipe 52 is connected to the input end of the suction pump 51, and the other end is connected to the suction box 53. During use, the suction pump 51 performs suction to remove the air located at the ventilation hole 12, forming a negative pressure. The foam board to be cut is adsorbed onto the fixed plate 11 by the negative pressure to prevent displacement during the cutting process.

[0043] There are several ventilation holes 12, which are arranged in a rectangular array on the fixed plate 11. The shape of the suction box 53 is adapted to the distribution of the ventilation holes 12, so as to ensure that all ventilation holes 12 can be connected to the suction box 53.

[0044] As a further embodiment of the present invention, the cutting mechanism 4 includes a mounting beam 42, and the number of driving mechanisms 3 is two. The two driving mechanisms 3 are respectively arranged on both sides of the forming frame 2. The two ends of the mounting beam 42 are respectively fixedly connected to the output ends of the two driving mechanisms 3. The two driving mechanisms 3 simultaneously drive the mounting beam 42 to move on the frame 1, ensuring that the two ends of the hot melt wire 41 remain relatively synchronized when moving, thereby preventing uneven cutting, improving cutting quality, ensuring the smoothness and flatness of the cutting edge, and facilitating subsequent secondary cutting.

[0045] As further embodiments of the present application, as shown in Figure 3 , Figure 4 and Figure 5 , the cutting mechanism 4 further comprises a first mounting plate 43 and a second mounting plate 44, the first connecting screw 45 and the second connecting screw 46 are slidingly connected to the mounting beam 42, the first mounting plate 43 is slidingly connected to the first connecting screw 45, and the second mounting plate 44 is slidingly connected to the second connecting screw 46. The spacing between the first mounting plate 43 and the second mounting plate 44 or the height of the first mounting plate 43 and the second mounting plate 44 on the mounting beam 42 can be adjusted by adjusting the first connecting screw 45 and the second connecting screw 46. One end of the hot wire 41 is connected to the first mounting plate 43, and the other end is connected to the second mounting plate 44.

[0046] As further embodiments of the present application, as shown in Figure 4 , sliding blocks 47 are provided at the ends of the first mounting plate 43 and the second mounting plate 44, fastening screws 48 are provided on the sliding blocks 47, one end of the hot wire 41 is connected to the fastening screw 48 on the first mounting plate 43, a tension spring 49 is provided on the second mounting plate 44, and the other end of the hot wire 41 is connected to the tension spring 49 by passing around the fastening screw 48 on the second mounting plate 44. Preferably, the sliding blocks 47 are located below the top surface of the forming frame 2 in the horizontal position, one end of the hot wire 41 is fixed by the fastening screw 48 on the first mounting plate 43, and the other end is connected to the tension spring 49 by passing around the fastening screw 48 on the second mounting plate 44, so that both ends of the hot wire 41 are located below the top surface of the forming frame 2, which can ensure that the hot wire 41 always adheres to the top of the forming frame 2 during the process, and ensures the cutting accuracy. The other end of the hot wire 41 is connected to the tension spring 49, and the elasticity of the tension spring 49 always keeps the hot wire 41 tight, ensuring that it can still fit the top of the forming frame 2 after replacing different forming frames 2.

[0047] As further embodiments of the present application, as shown in Figure 5As shown, the driving mechanism 3 comprises a driving motor 31, a screw rod 32, a mounting base 33, a guide rod 34 and a sliding block 35. The mounting base 33 is fixedly installed on the outer wall of one side of the rack 1, specifically, the mounting base 33 is fixedly installed on the outer wall of one side of the fixed plate 11. The driving motor 31 is fixedly installed on the outer wall of one side of the mounting base 33, the screw rod 32 is rotationally connected in the mounting base 33, and one end of the screw rod 32 penetrates and extends to the outside of the mounting base 33, the one end of the screw rod 32 outside the mounting base 33 is fixedly connected to the driving motor 31, and the driving motor 31 can drive the screw rod 32 to keep rotating. The number of the guide rods 34 is two, and the two guide rods 34 are symmetrically installed in the mounting base 33. The sliding block 35 is slidingly connected to the guide rod 34, and the sliding block 35 is threadedly connected to the screw rod 32. When the driving motor 31 drives the screw rod 32 to keep rotating, the screw rod 32 can drive the sliding block 35 to keep sliding along the guide rod 34. One end of the mounting beam 42 is connected to the sliding block 35.

[0048] Working principle:

[0049] Before cutting, the foam plate to be cut is placed in the forming frame 2, and then the switch of the suction pump 51 is started, and the foam plate is adsorbed on the fixed plate 11 by negative pressure;

[0050] Then the switch of the driving motor 31 is started, the driving motor 31 drives the screw rod 32 to keep rotating, the sliding block 35 moves along the guide rod 34, and the mounting beam 42 moves, so that the hot melting wire 41 attached to the forming frame 2 moves along the forming strip 22 of the forming frame 2, the foam plate is cut, after a single cutting is completed, the switches of the suction pump 51 and the driving motor 31 are turned off, the cut and formed foam plate is taken out, a new foam plate is replaced, and then the suction pump 51 and the driving motor 31 are started in turn, the foam plate is adsorbed and the mounting beam 42 is reset, and the foam plate can be cut at the same time.

[0051] The tensile spring 49 mentioned in the text meets the technical requirements of the technical scheme of the utility model.

[0052] Those skilled in the art can understand that other similar connection methods can also achieve the utility model. For example, welding, bonding or screwing and the like.

[0053] The above only describes certain exemplary embodiments of the utility model by way of illustration, and it is needless to say that those skilled in the art can modify the described embodiments in various ways without departing from the spirit and scope of the utility model. Therefore, the above drawings and description are illustrative in nature and should not be understood as limiting the scope of protection of the claims of the utility model.

Claims

1. An automatic cutting device for pre-molded foam cores of aircraft seats, comprising a frame (1), characterized in that, Also includes: A molding frame (2) is set on the frame (1), and a foam board may be connected inside the molding frame (2); The drive mechanism (3) is mounted on the frame (1); A cutting mechanism (4) is connected to the output end of the drive mechanism (3). The cutting mechanism (4) includes a hot melt wire (41) which is attached to the outer wall of the forming frame (2). The cutting mechanism (4) is driven by the driving mechanism (3) to keep reciprocating so that the hot melt wire (41) moves against the outer wall of the forming frame (2).

2. The automatic cutting device for pre-molded foam cores of aircraft seats according to claim 1, characterized in that, The forming frame (2) includes a fixing strip (21) and a forming strip (22). There are several fixing strips (21) and forming strips (22). The fixing strips (21) and forming strips (22) are connected in sequence to form a frame structure.

3. The automatic cutting device for pre-molded foam cores of aircraft seats according to claim 1, characterized in that, It also includes an adsorption mechanism (5) set inside the frame (1). A fixing plate (11) is fixedly set on the frame (1). A ventilation hole (12) is opened on the fixing plate (11). The adsorption mechanism (5) includes a suction pump (51), a connecting pipe (52) and a suction box (53). The suction box (53) is fixedly installed on the fixing plate (11). The ventilation hole (12) is connected to the suction box (53). One end of the connecting pipe (52) is connected to the suction box (53), and the other end of the connecting pipe (52) is connected to the suction pump (51).

4. The automatic cutting device for pre-molded foam core of aircraft seats according to claim 1, characterized in that, The cutting mechanism (4) includes a mounting beam (42), and there are two driving mechanisms (3). The two driving mechanisms (3) are respectively arranged on both sides of the forming frame (2), and the two ends of the mounting beam (42) are respectively fixedly connected to the output ends of the two driving mechanisms (3).

5. The automatic cutting device for pre-molded foam core of aircraft seats according to claim 4, characterized in that, The cutting mechanism (4) further includes a first mounting plate (43) and a second mounting plate (44). A first connecting screw (45) and a second connecting screw (46) are slidably connected on the mounting beam (42). The first mounting plate (43) and the second mounting plate (44) are both slidably connected to the mounting beam (42). One end of the hot melt wire (41) is connected to the first mounting plate (43), and the other end of the hot melt wire (41) is connected to the second mounting plate (44).

6. The automatic cutting device for pre-molded foam cores of aircraft seats according to claim 5, characterized in that, The first mounting plate (43) and the second mounting plate (44) are each provided with a sliding block (47), and a fastening screw (48) is provided on the sliding block (47). One end of the hot melt wire (41) is connected to the fastening screw (48) on the first mounting plate (43). A tension spring (49) is provided on the second mounting plate (44), and the other end of the hot melt wire (41) passes around the fastening screw (48) on the second mounting plate (44) and is connected to the tension spring (49).

7. The automatic cutting device for pre-molded foam core of aircraft seats according to claim 1, characterized in that, The drive mechanism (3) includes a drive motor (31), a lead screw (32), a mounting base (33), a guide rod (34), and a slider (35). The mounting base (33) is fixedly installed on the outer wall of one side of the frame (1). The drive motor (31) is fixedly installed on the outer wall of one side of the mounting base (33). The lead screw (32) is rotatably connected to the inside of the mounting base (33), and one end of the lead screw (32) passes through and extends to the outside of the mounting base (33). The end of the lead screw (32) located outside the mounting base (33) is connected to the drive motor (31). The guide rod (34) is fixedly installed inside the mounting base (33). The slider (35) is threadedly connected to the lead screw (32), and the slider (35) is slidably connected to the guide rod (34).

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