Modular device for manufacturing an aircraft seat

Abstract

The utility model discloses a modularized device for manufacturing an aircraft seat, which comprises a main body mechanism, the main body mechanism comprises a base, a plurality of positioning modules mounted at the top end of the base, height modules mounted at the top ends of the positioning modules, mounting seats mounted at the top ends of the height modules, clamping modules arranged on the mounting seats and locking pieces mounted on the positioning modules and the height modules, and the base is used for mounting the positioning modules; a plurality of threaded holes are formed in the top end of the base in a rectangular array mode, the positioning module can be conveniently installed at any position of the top end of the base, and the positioning module is used for positioning the positions of the installation base and the clamping module and comprises a U-shaped base arranged at the top end of the base and a plurality of fixing bolts penetrating through the U-shaped base to be meshed in the threaded holes. The U-shaped seat is used for being connected with a height module or a mounting seat, and the modularization device for manufacturing the aircraft seat has the advantages that the clamping mechanism is modularized, and the practicability is high.

Description

Technical Field

[0001] This utility model relates to the field of aircraft seat manufacturing technology, specifically a modular device for manufacturing aircraft seats. Background Technology

[0002] Seats, of course, refer to products that can be used on vehicles such as cars or airplanes. People use various means of transportation for getting around, and seats can provide a comfortable resting environment for the journey, while also providing a certain degree of safety for passengers. The most common types are airplane seats, car seats, and bus seats. With the development of science and technology, there are more and more seats available, and their functions are becoming more and more powerful. Among them, airplane seats are also quite common. In the production process of airplane seats, clamping equipment is required to hold and fix the airplane seats in place, ensuring the stability of the aircraft during the assembly process.

[0003] Existing aircraft seat clamping equipment has the following drawbacks during use: poor modularity, complicated installation and disassembly, and the need to change clamps when clamping aircraft seats of different sizes and shapes, which is quite complicated. Therefore, there is room for improvement. Utility Model Content

[0004] This utility model aims to solve one of the technical problems existing in the prior art or related technologies.

[0005] Therefore, the technical solution adopted by this utility model is as follows: a modular device for manufacturing aircraft seats, comprising: a main body mechanism, the main body mechanism including a base, a plurality of positioning modules mounted on the top of the base, a height module mounted on the top of the positioning modules, a mounting seat mounted on the top of the height module, a clamping module disposed on the mounting seat, and a locking component mounted on the positioning modules and the height modules.

[0006] The top of the base has a rectangular array of multiple threaded holes, and the positioning module includes a U-shaped seat set at the top of the base and multiple fixing bolts that pass through the U-shaped seat and engage in the threaded holes.

[0007] The height module includes a support member disposed at the top of the U-shaped base and a plurality of first insert rods fixed at the bottom of the support member and extending into the U-shaped base.

[0008] The mounting base includes a support at the top of the support member, a plurality of second insert rods fixed at the bottom of the support member and fitted into the support member, and an air tube installed on one side of the support member and communicating with the inner cavity of the support member.

[0009] The clamping module includes a piston movably disposed in the inner cavity of the support, a round rod with one end connected to the piston and the other end extending out of the support, a spring sleeved on the round rod with one end connected to the piston and the other end connected to the inner wall of the support, a rectangular plate fixed to the end of the round rod, a support rod with one end connected to the rectangular plate and the other end embedded in the top of the support, and a clamping block fixed to the end of the support rod.

[0010] In a preferred embodiment, the present invention can be further configured such that the locking element includes a side plate, a fixing rod symmetrically fixed to the side plate, and a magnet installed on the inner side of the side plate.

[0011] In a preferred embodiment, the present invention can be further configured as follows: a plurality of first slots are symmetrically opened at the top of the U-shaped seat, the first insert rod is fitted into the first slot, a first insertion hole is opened laterally on one side of the U-shaped seat and passes through the first slot, a first through hole is opened laterally on the first insert rod, and a locking member on one side of the U-shaped seat passes through the first insertion hole and the first through hole.

[0012] In a preferred embodiment, the present invention can be further configured as follows: a second slot is opened at the top of the support member, the first insert rod is fitted into the second slot, a second insertion hole is opened laterally on the side of the support member to pass through the second slot, a second through hole is opened laterally on the second insert rod, and a locking member on one side of the support member passes through the second insertion hole and the second through hole.

[0013] In a preferred embodiment, the present invention can be further configured such that: the top end of the support has a sliding groove, and the support rod is slidably fitted into the sliding groove.

[0014] In a preferred embodiment, the present invention can be further configured such that: the support has an internal cavity, and the piston is fitted into the cavity.

[0015] By adopting the above technical solution, the beneficial effects achieved by this utility model are as follows:

[0016] 1. In this utility model, a modular design is adopted, with a base and multiple threaded holes arranged in a rectangular array on the base. A positioning module, mounting base, clamping module, and locking element are also provided. Through this design, the positioning module can be installed at any position on the base. The mounting base containing the clamping module is then installed on the positioning module via the locking element, forming a multi-directional clamping mechanism. The clamping position can be adjusted according to the shape of the aircraft seat without changing the clamps. Furthermore, the positioning module and mounting base are connected via the locking element, making installation and disassembly convenient and effectively increasing the ease of clamping during aircraft seat production.

[0017] 2. In this utility model, a height module is provided, which is located between the positioning module and the mounting base. By increasing or decreasing the number of height modules, the height of the mounting base can be adjusted, that is, the height of the clamping module can be adjusted, which facilitates clamping and fixing the aircraft seat at different positions. At the same time, the height module is also connected to the positioning module and the mounting base through locking components, which makes installation and disassembly convenient and further increases the practicality. Attached Figure Description

[0018] Figure 1 This is a schematic diagram of the structure of this utility model;

[0019] Figure 2 This is an exploded structural diagram of the present invention;

[0020] Figure 3 This is a schematic diagram of the positioning module structure of this utility model;

[0021] Figure 4 This is a schematic diagram of the height module structure of this utility model.

[0022] Figure 5 This is a partial structural cross-sectional view of the present invention;

[0023] Figure 6 This is a partial exploded structural diagram of the present invention.

[0024] Figure label:

[0025] 100. Main body; 110. Base; 111. Threaded hole; 120. Positioning module; 121. U-shaped seat; 1211. First slot; 1212. First insertion hole; 122. Fixing bolt; 130. Height module; 131. Support; 1311. Second slot; 1312. Second insertion hole; 132. First insertion rod; 1321. First through hole; 140. Mounting seat; 141. Support; 1411. Slide groove; 1412. Cavity; 142. Second insertion rod; 1421. Second through hole; 143. Air pipe; 150. Clamping module; 151. Piston; 152. Round rod; 153. Spring; 154. Rectangular plate; 155. Support rod; 156. Clamping block; 160. Locking element; 161. Side plate; 162. Fixing rod; 163. Magnet. Detailed Implementation

[0026] To make the objectives, technical solutions, and advantages of this utility model clearer, the present utility model will be further described in detail below with reference to specific embodiments and accompanying drawings. It should be noted that, unless otherwise specified, the embodiments and features of the present utility model can be combined with each other.

[0027] Some embodiments of this utility model are described below with reference to the accompanying drawings.

[0028] Example 1:

[0029] Combination Figure 1-6 As shown, this embodiment provides a modular device for manufacturing aircraft seats, including: a main body 100.

[0030] The main body 100 includes a base 110, multiple positioning modules 120 mounted on the top of the base 110, a height module 130 mounted on the top of the positioning module 120, a mounting seat 140 mounted on the top of the height module 130, a clamping module 150 disposed on the mounting seat 140, and a locking element 160 mounted on the positioning module 120 and the height module 130.

[0031] The base 110 is used to install the positioning module 120. The top of the base 110 has multiple threaded holes 111 arranged in a rectangular array, which makes it convenient for the positioning module 120 to be installed at any position on the top of the base 110.

[0032] The positioning module 120 is used to position the mounting base 140 and the clamping module 150. It includes a U-shaped seat 121 set at the top of the base 110 and a plurality of fixing bolts 122 that pass through the U-shaped seat 121 and engage in the threaded holes 111. The U-shaped seat 121 is used to connect with the height module 130 or the mounting base 140. The fixing bolts 122 pass through the U-shaped seat 121 and engage in the threaded holes 111 on the base 110, which can ensure the stability of the U-shaped seat 121.

[0033] The height module 130 is used to increase the height of the mounting base 140 and the clamping module 150, so as to facilitate clamping the aircraft seat at different height positions. It includes a support member 131 set at the top of the U-shaped base 121 and a plurality of first insert rods 132 fixed at the bottom of the support member 131 and extending into the U-shaped base 121.

[0034] Multiple first slots 1211 are symmetrically opened at the top of the U-shaped base 121. The first insert rod 132 is fitted into the first slot 1211 to ensure the stability of the support member 131. A first insertion hole 1212 is opened laterally on one side of the U-shaped base 121, passing through the first slot 1211. A first through hole 1321 is opened laterally on the first insert rod 132. A locking member 160 on one side of the U-shaped base 121 passes through the first insertion hole 1212 and the first through hole 1321 to lock the support member 131 and the U-shaped base 121 together.

[0035] Mounting base 140 is located at the top of height module 130 and includes a support 141 located at the top of support member 131, a plurality of second insert rods 142 fixed at the bottom of support 141 and fitted into support member 131, and an air pipe 143 installed on one side of support 141 and communicating with the inner cavity of support 141.

[0036] The top of the support member 131 has a second slot 1311, and the first insert rod 132 is fitted into the second slot 1311 to ensure the stability of the support 141. At the same time, the first insert rod 132 of the support member 131 itself is also fitted into the second slot 1311 to facilitate the stacking of the height modules 130. A second insertion hole 1312 is opened laterally on the side of the support member 131 and passes through the second slot 1311. A second through hole 1421 is opened laterally on the second insert rod 142. A locking member 160 on one side of the support member 131 passes through the second insertion hole 1312 and the second through hole 1421 to lock the support member 131 and the support 141 together.

[0037] The clamping module 150 is used to clamp and fix the aircraft seat. It includes a piston 151 movably disposed within the cavity of the support 141; a round rod 152 with one end connected to the piston 151 and the other end extending out of the support 141; a spring 153 sleeved on the round rod 152 and connected at one end to the piston 151 and the other end to the inner wall of the support 141; a rectangular plate 154 fixed to the end of the round rod 152; a support rod 155 with one end connected to the rectangular plate 154 and the other end fitted into the top of the support 141; and a clamping block 156 fixed to the end of the support rod 155. The support 141 has an internal cavity 1412, within which the piston 151 is fitted. An air tube 143 connects to this cavity. The cavity 1412 is connected. When high-pressure air is sent into the piston 151 through the air pipe 143, it drives the piston 151 to move. The movement of the piston 151 drives the rectangular plate 154 to move through the round rod 152. The movement of the rectangular plate 154 drives the support rod 155 to move. The movement of the support rod 155 drives the clamping block 156 to move, clamping the aircraft seat. A sliding groove 1411 is opened at the top of the support 141. The support rod 155 slides and fits in the sliding groove 1411 to ensure the stability of the clamping block 156 during movement. The spring 153 is used to drive the piston 151 to reset after the piston 151 loses gas pressure, that is, to drive the clamping block 156 to reset.

[0038] The locking component 160 is used to lock two adjacent modules. It includes a side plate 161, a fixing rod 162 symmetrically fixed on the side plate 161, and a magnet 163 installed on the inner side of the side plate 161. The side plate 161 is used to install the fixing rod 162 and drive the fixing rod 162 to move. The fixing rod 162 can lock two adjacent modules. The magnet 163 is used to attract the U-shaped seat 121 or the support component 131 to ensure the stability of the side plate 161, that is, to ensure the stability of the locking component 160. At the same time, the magnetic attraction setting makes it convenient to install and remove the locking component 160, that is, to facilitate the installation and removal between adjacent modules.

[0039] The working principle and usage process of this utility model are as follows: In use, the positioning module 120 is placed on the base 110. The position of the positioning module 120 is adjusted according to the shape of the aircraft seat. After adjustment, the fixing bolt 122 is passed through the U-shaped seat 121 and engaged in the threaded hole 111 on the base 110, thus fixing the positioning module 120. The number of height modules 130 can be increased or decreased as needed. Pulling the locking member 160 on one side of the positioning module 120 inserts the first insertion rod 132 at the bottom of the support member 131 into the first slot 1211 at the top of the U-shaped seat 121. The locking member 160 is then released. At this time, the fixing rod 162 passes through the first insertion hole 1212 on the U-shaped seat 121 and the first through hole 1321 on the first insertion rod 132, thus connecting the support member 131 and the U-shaped seat 121. 1. Lock together, pull out the locking piece 160 on one side of the support member 131, insert the second insertion rod 142 at the bottom of the support 141 into the second slot 1311 on the support member 131, release the locking piece 160, at this time the fixing rod 162 passes through the second insertion hole 1312 on the support member 131 and the second through hole 1421 on the second insertion rod 142, locking the mounting base 140 and the support member 131 together, thus completing the installation of the entire clamping mechanism. When clamping the aircraft seat, high-pressure gas is injected into the cavity 1412 of the support 141 through the air pipe 143, which drives the piston 151 to move. The movement of the piston 151 drives the rectangular plate 154 to move through the round rod 152. The movement of the rectangular plate 154 drives the clamping block 156 to move through the support rod 155, thus clamping and fixing the aircraft seat.

[0040] Although embodiments of the present invention have been shown and described, those skilled in the art will understand that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the claims and their equivalents.

Claims

1. A modular device for manufacturing aircraft seats, comprising: The main body (100) is characterized in that the main body (100) includes a base (110), a plurality of positioning modules (120) installed on the top of the base (110), a height module (130) installed on the top of the positioning module (120), a mounting seat (140) installed on the top of the height module (130), a clamping module (150) disposed on the mounting seat (140), and a locking member (160) installed on the positioning module (120) and the height module (130); The top of the base (110) has a rectangular array of multiple threaded holes (111), and the positioning module (120) includes a U-shaped seat (121) set at the top of the base (110) and multiple fixing bolts (122) that pass through the U-shaped seat (121) and engage in the threaded holes (111). The height module (130) includes a support member (131) disposed at the top of the U-shaped seat (121) and a plurality of first inserts (132) fixed at the bottom of the support member (131) and extending into the U-shaped seat (121); The mounting base (140) includes a support (141) disposed at the top of the support member (131), a plurality of second insert rods (142) fixed at the bottom of the support (141) and fitted into the support member (131), and an air tube (143) installed on one side of the support (141) and communicating with the inner cavity of the support (141). The clamping module (150) includes a piston (151) movably disposed in the inner cavity of the support (141), a round rod (152) with one end connected to the piston (151) and the other end extending out of the support (141), a spring (153) sleeved on the round rod (152) with one end connected to the piston (151) and the other end connected to the inner wall of the support (141), a rectangular plate (154) fixed to the end of the round rod (152), a support rod (155) with one end connected to the rectangular plate (154) and the other end fitted into the top of the support (141), and a clamping block (156) fixed to the end of the support rod (155).

2. A modular device for manufacturing aircraft seats according to claim 1, characterized in that, The locking element (160) includes a side plate (161), a fixing rod (162) symmetrically fixed on the side plate (161), and a magnet (163) installed on the inner side of the side plate (161).

3. A modular device for manufacturing aircraft seats according to claim 1, characterized in that, The top of the U-shaped base (121) has a plurality of first slots (1211) symmetrically opened. The first insert rod (132) is fitted into the first slot (1211). The U-shaped base (121) has a first insertion hole (1212) opened laterally on one side, which passes through the first slot (1211). The first insert rod (132) has a first through hole (1321) opened laterally. The locking member (160) on one side of the U-shaped base (121) passes through the first insertion hole (1212) and the first through hole (1321).

4. A modular device for manufacturing aircraft seats according to claim 1, characterized in that, The top of the support member (131) has a second slot (1311), the first insert rod (132) is fitted into the second slot (1311), a second insertion hole (1312) is opened laterally on the side of the support member (131) and passes through the second slot (1311), a second through hole (1421) is opened laterally on the second insert rod (142), and a locking member (160) on one side of the support member (131) passes through the second insertion hole (1312) and the second through hole (1421).

5. A modular device for manufacturing aircraft seats according to claim 1, characterized in that, The top of the support (141) has a groove (1411), and the support rod (155) is slidably fitted into the groove (1411).

6. A modular device for manufacturing aircraft seats according to claim 1, characterized in that, The support (141) has a cavity (1412) inside, and the piston (151) is fitted into the cavity (1412).

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