Mounting structure of airborne operating platform

Abstract

The invention relates to a mounting structure of an airborne operating platform, and relates to the technical field of aircraft component testing, the mounting structure comprises a track, a frame body and a machine body arranged on the frame body, a plate body is arranged on the frame body in a manner of extending towards the upper part of the track, and the plate body is provided with rollers used for being clamped and slidably connected to the track; clamping jaws are arranged on the plate body and located on the two sides of the plate body in a hinged mode, a plurality of fixing openings are formed in the rail in the length direction of the rail, and a driving piece used for driving the clamping jaws on the two sides to rotate at the hinged position on the plate body at the same time so as to drive the clamping jaws on the two sides to be inserted into the fixing openings at the same time is arranged on the plate body and comprises a driving block, a connecting rod and a driving part. Connecting rods are hinged to the two sides of the driving block, the ends, away from the driving block, of the connecting rods on the two sides are hinged to the clamping jaw, and the driving part is used for driving the driving block to ascend and descend. The device has the advantages that the position of the airborne operation table is adjusted, and therefore the internal space of a cabin is effectively utilized.

Description

Technical Field

[0001] The present invention relates to the technical field of aircraft component testing, and more particularly to an installation structure of an airborne operation console. Background Art

[0002] Artificial precipitation, also known as artificial rainfall augmentation, refers to the process of artificially supplementing some necessary conditions for precipitation formation according to the principle of natural precipitation formation, promoting the rapid condensation or coalescence of cloud droplets into raindrops, and falling to the ground. The method is to select the appropriate timing according to the physical characteristics of different clouds and use aircraft or rockets to disperse catalysts such as dry ice, silver iodide, and salt powder into the clouds, causing the clouds to precipitate or increase the precipitation amount, so as to relieve or alleviate farmland drought, increase the reservoir irrigation water volume or water supply capacity, or increase the power generation water volume, etc.

[0003] When the related technology uses an aircraft for artificial rainfall, an operation console needs to be arranged inside the cabin of the aircraft. The operation console is usually fixedly arranged on the floor inside the aircraft cabin by means of bolts. The operation console is fixed inside the cabin by bolts, which is not convenient for adjusting the position of the cabin, and thus the space inside the cabin cannot be effectively utilized. Summary of the Invention

[0004] Aiming at the deficiencies of the existing technology, the purpose of the present invention is to provide an installation structure of an airborne operation console that is convenient for adjusting the position and thus effectively utilizes the space inside the cabin.

[0005] The above invention purpose of the present invention is achieved through the following technical solutions: An installation structure of an airborne operation console, including a track, a frame body, and a machine body arranged on the frame body. The track is used to be fixedly connected to the floor inside the aircraft cabin by bolts. A plate body extends upward toward the track on the frame body. Rollers for clamping and sliding connection on the track are arranged on the plate body. Claw jaws are hinged on both sides of the plate body. A plurality of fixing ports are opened along the length direction of the track on the track. A driving member is arranged on the plate body for driving the claw jaws on both sides to rotate simultaneously at the hinged positions on the plate body, so as to drive the claw jaws on both sides to be inserted into the fixing ports simultaneously. The driving member includes a driving block, a connecting rod, and a driving part. Connecting rods are hinged on both sides of the driving block. The ends of the connecting rods on both sides away from the driving block are hinged on the claw jaws. The driving part is used to drive the driving block to move up and down.

[0006] In a preferred example of the present invention, it can be further configured as: the driving part includes a driving electric cylinder fixedly arranged on the plate body and located between the claw jaws on both sides, and the driving block is fixedly arranged on the driving end of the driving electric cylinder.

[0007] In a preferred example, the present invention can be further configured as follows: a slot is formed on one of the jaws, and a plug block for being inserted into the slot is provided on the other jaw.

[0008] In a preferred example, the present invention can be further configured as follows: a fixing member for preventing the plug block from disengaging from the slot is provided on the driving block.

[0009] In a preferred example, the present invention can be further configured as follows: the fixing member includes a fixing electric cylinder and a fixing rod. The fixing rod is fixedly arranged on the driving end of the fixing electric cylinder. The fixing electric cylinder is arranged on the surface of the driving block facing away from the plate body. Fixing holes for the fixing rod to pass through are formed on the plug block and the two jaws.

[0010] In a preferred example, the present invention can be further configured as follows: the plate body includes a first connecting plate and a second connecting plate. The first connecting plate is arranged on the frame body. The jaws are hinged to the second connecting plate. An adjusting groove is formed on the second connecting plate. The length direction of the adjusting groove is arranged perpendicular to the length direction of the track. An adjusting block slidably connected in the adjusting groove is provided on the first connecting plate. An adjusting member for fixing the adjusting block to any position after movement is arranged in the adjusting groove.

[0011] In a preferred example, the present invention can be further configured as follows: the adjusting member includes a screw rod and an adjusting motor. The screw rod is rotatably arranged in the adjusting groove along the length direction of the adjusting groove. The adjusting block is sleeved and threadedly connected to the screw rod. The adjusting motor is fixedly arranged on the first connecting plate, and the adjusting motor is used for driving the screw rod to rotate.

[0012] In a preferred example, the present invention can be further configured as follows: the track includes a plurality of connecting rails spliced together. Connecting grooves and connecting blocks that cooperate with each other are respectively arranged on the opposite surfaces of adjacent connecting rails. Bolts for detachably connecting the connecting blocks into the connecting grooves are arranged on the connecting rails.

[0013] In summary, the present invention includes at least one of the following beneficial technical effects: By driving the rollers on the plate body to move on the track, it is convenient to adjust the position of the airborne operation console along the length direction of the track. When multiple operation consoles need to be arranged in the aircraft cabin, it is convenient to utilize the space inside the cabin by adjusting the position of the airborne operation console. When it is necessary to fix the airborne operation console to the adjusted position, the driving part drives the driving block to descend, so that both ends of the connecting rod rotate at the hinge points on the driving block and the jaw. At this time, the connecting rod can drive the jaw to rotate at the hinge point on the plate body, so that the jaw is inserted into the fixing port, thereby preventing the frame body from moving on the track by the jaw and the fixing port, and fixing the airborne operation console to the moved position, improving the fixing effect of the airborne operation console. Description of the Drawings

[0014] Figure 1 is a schematic structural diagram of the frame body and the fuselage used in the embodiment of the present application.

[0015] Figure 2 is a partial schematic structural diagram of the plate body and the roller used in the embodiment of the present application.

[0016] Figure 3 is a schematic cross-sectional structural diagram of the driving member used in the embodiment of the present application; Figure 4 is a schematic structural diagram of the connecting rail used in the embodiment of the present application.

[0017] In the figure, 100, track; 110, frame body; 111, fuselage; 112, roller; 120, plate body; 121, jaw; 122, fixing port; 123, driving block; 124, connecting rod; 125, driving electric cylinder; 126, slot; 127, plug; 130, fixing electric cylinder; 131, fixing rod; 140, first connecting plate; 141, second connecting plate; 142, adjusting slot; 143, adjusting block; 144, screw; 145, adjusting motor; 150, connecting rail; 151, connecting slot; 152, connecting block. Detailed Description of the Invention

[0018] The present invention will be further described in detail below with reference to the accompanying drawings.

[0019] Combined with Figure 1 and Figure 2 , an installation structure of an airborne operation console disclosed in the present invention includes a track 100, a frame body 110 and a fuselage 111 provided on the frame body 110. The track 100 is used to be fixed to the floor inside the aircraft cabin by bolts. A plate body 120 extends upward on the frame body 110 toward the track 100. A roller 112 for clamping and sliding connection on the track 100 is provided on the plate body 120. The cross-section of the track 100 is rectangular, and the cross-section of the roller 112 is "H"-shaped.

[0020] Combined with Figure 1 and Figure 3 , on the plate body 120 and hinged on both sides of the plate body 120 are clamping jaws 121. The clamping jaws 121 are integrally arranged in a "V" shape. Along the length direction of the track 100, a plurality of fixing openings 122 are formed in the track 100. On the plate body 120, there is a driving member for driving the clamping jaws 121 on both sides to rotate simultaneously at the hinged positions on the plate body 120, so as to drive the clamping jaws 121 on both sides to be inserted into the fixing openings 122 at the same time. The driving member includes a driving block 123, a connecting rod 124 and a driving part. On both sides of the driving block 123, the connecting rods 124 are hinged. The ends of the connecting rods 124 on both sides away from the driving block 123 are hinged on the clamping jaws 121. The driving part is used to drive the driving block 123 to move up and down.

[0021] By adopting the above technical solution, by driving the roller 112 on the plate body 120 to move on the track 100, it is convenient to adjust the position of the airborne operating platform along the length direction of the track 100. When multiple operating platforms need to be arranged in the cabin of the aircraft, it is convenient to utilize the space inside the cabin by adjusting the position of the airborne operating platform; when it is necessary to fix the airborne operating platform to the adjusted position, the driving part drives the driving block 123 to descend, so that the two ends of the connecting rod 124 rotate at the hinged positions on the driving block 123 and the clamping jaws 121. At this time, the connecting rod 124 can drive the clamping jaws 121 to rotate at the hinged positions on the plate body 120, so that the clamping jaws 121 are inserted into the fixing openings 122, thereby preventing the frame body 110 from moving on the track 100 and fixing the airborne operating platform to the moved position, improving the fixing effect of the airborne operating platform.

[0022] As Figure 3 shown, the driving part includes a driving electric cylinder 125 fixedly arranged on the plate body 120 and located between the clamping jaws 121 on both sides. The driving block 123 is fixedly arranged on the driving end of the driving electric cylinder 125.

[0023] By adopting the above technical solution, the driving electric cylinder 125 drives the driving block 123 to move up and down, so that the clamping jaws 121 can be moved into or out of the fixing openings 122. The structure of the driving electric cylinder 125 is simple and convenient for maintenance, improving the driving effect of driving the driving block 123 to move up and down.

[0024] As Figure 3 shown, a slot 126 is formed in one of the clamping jaws 121, and a plug 127 for inserting into the slot 126 is arranged on the other clamping jaw 121.

[0025] By adopting the above technical solution, when the two clamping jaws 121 approach each other, the insertion block 127 can be driven to be inserted into the insertion slot 126, thereby improving the insertion effect of the two clamping jaws 121 inserted into the fixing port 122, and indirectly improving the fixing effect of the airborne operating platform.

[0026] As Figure 3 shown, a fixing member for preventing the insertion block 127 from detaching from the insertion slot 126 is provided on the driving block 123.

[0027] By adopting the above technical solution, the setting of the fixing member can prevent the insertion block 127 from detaching from the insertion slot 126, thereby preventing the separation between the two clamping jaws 121, and further improving the fixing effect of fixing the airborne operating platform to the moved position.

[0028] As Figure 3 shown, the fixing member includes a fixing electric cylinder 130 and a fixing rod 131. The fixing rod 131 is fixedly arranged on the driving end of the fixing electric cylinder 130. The fixing electric cylinder 130 is arranged on the surface of the driving block 123 facing away from the plate body 120. Fixing holes for the fixing rod 131 to pass through are formed on the insertion block 127 and the two clamping jaws 121.

[0029] By adopting the above technical solution, after the two clamping jaws 121 approach each other and drive the insertion block 127 to be inserted into the insertion slot 126, at this time, the fixing electric cylinder 130 drives the fixing rod 131 to descend, so that the fixing rod 131 passes through the fixing holes on the insertion block 127 and the two clamping jaws 121, thereby preventing the insertion block 127 from detaching from the insertion slot 126, fixing the insertion block 127 to the insertion slot 126, and preventing the separation between the two clamping jaws 121, indirectly improving the fixing effect of the clamping jaws 121 on the airborne operating platform.

[0030] As Figure 3 shown, the plate body 120 includes a first connecting plate 140 and a second connecting plate 141. The first connecting plate 140 is arranged on the frame body 110. The clamping jaw 121 is hinged to the second connecting plate 141. The fixing electric cylinder 130 is fixedly arranged on the surface of the second connecting plate 141 facing away from the first connecting plate 140. An adjusting groove 142 is formed on the second connecting plate 141. The length direction of the adjusting groove 142 is arranged along the direction perpendicular to the length direction of the track 100. An adjusting block 143 slidably connected in the adjusting groove 142 is arranged on the first connecting plate 140. An adjusting member for fixing the adjusting block 143 to any moved position is arranged in the adjusting groove 142; the roller 112 is arranged on the surface of the second connecting plate 141 facing away from the first connecting plate 140.

[0031] By adopting the above technical solution, the adjusting member drives the adjusting block 143 to move within the adjusting groove 142, so that the adjusting block 143 drives the first connecting plate 140 to move, enabling the first connecting plate 140 to drive the frame 110 to adjust the position of the airborne operation console along the length direction perpendicular to the track 100. By further adjusting the position of the airborne operation console, the space inside the aircraft cabin can be further utilized.

[0032] As Figure 3 shown, the adjusting member includes a screw rod 144 and an adjusting motor 145. The screw rod 144 is rotatably arranged in the adjusting groove 142 along the length direction of the adjusting groove 142. The adjusting block 143 is sleeved and threadedly connected to the screw rod 144. The adjusting motor 145 is fixedly arranged on the first connecting plate 140, and the adjusting motor 145 is used to drive the screw rod 144 to rotate.

[0033] By adopting the above technical solution, the adjusting motor 145 drives the screw rod 144 to rotate. Since the adjusting block 143 is slidably arranged in the adjusting groove 142, the adjusting block 143 will not rotate along with the rotation of the screw rod 144, so that the adjusting block 143 moves along the length direction of the screw rod 144, and the adjusting block 143 drives the first connecting plate 140 to move. The arrangement of the screw rod 144 can fix the frame 110 to any moved position, thereby improving the fixing effect of the frame 110.

[0034] As Figure 4 shown, the track 100 includes a plurality of connecting rails 150 spliced together. Opposite surfaces of adjacent connecting rails 150 are respectively provided with a mating connecting groove 151 and a connecting block 152. Bolts are provided on the connecting rails 150 for detachably connecting the connecting block 152 into the connecting groove 151.

[0035] By adopting the above technical solution, the arrangement of a plurality of connecting rails 150 facilitates the adjustment of the length of the track 100, thereby increasing the adjustment range of the airborne operation console, and further utilizing the space inside the cabin; the arrangement of the connecting groove 151 and the connecting block 152 improves the splicing effect between adjacent connecting rails 150, and the arrangement of bolts facilitates the fixing of adjacent connecting rails 150, thereby improving the fixing effect of adjacent splicing rails.

[0036] The implementation principle of this embodiment is as follows: When it is necessary to adjust the position of the airborne operation console, the frame 110 is driven to move, so that the plate body 120 drives the roller 112 to move on the track 100. After moving to the specified position on the track 100, the driving cylinder 125 is driven to drive the driving block 123 to move, so that the driving block 123 drives the connecting rod 124 to rotate. The connecting rod 124 can drive the clamping jaws 121 on both sides to rotate, so that the clamping jaws 121 on both sides are simultaneously inserted into the fixing ports 122. At this time, the plug 127 and the slot 126 cooperate with each other, and the fixing cylinder 130 is driven to drive the fixing rod 131 to descend, so that the fixing rod 131 is inserted into the fixing hole, so that the plug 127 is fixed to the slot 126. The adjusting motor 145 is driven to drive the screw rod 144 to rotate, so that the adjusting block 143 drives the first connecting plate 140 to move. The first connecting plate 140 can drive the frame 110 to move in the length direction perpendicular to the track 100, so as to adjust the position of the airborne operation console. When multiple operation consoles need to be arranged in the cabin of the aircraft, it is convenient to effectively utilize the space inside the cabin; and when replacing the airborne operation consoles with different specifications inside the cabin, it is convenient to adjust the positions of multiple operation consoles with different specifications, so that multiple operation consoles with different specifications can effectively utilize the space inside the cabin.

[0037] The embodiments of this specific implementation manner are all preferred embodiments of the present invention, and do not limit the protection scope of the present invention accordingly. Therefore, all equivalent changes made according to the structure, shape, and principle of the present invention should be covered within the protection scope of the present invention.

Claims

1. An installation structure of an airborne operating console, characterized in that: It includes a track (100), a frame (110) and a body (111) disposed on the frame (110). The track (100) is used to be fixed to the floor inside the aircraft cabin by bolts. A plate body (120) extends upward toward the track (100) on the frame (110). Rollers (112) for clamping and slidingly connecting to the track (100) are provided on the plate body (120). Claw jaws (121) are hingedly disposed on both sides of the plate body (120). A plurality of fixing openings (122) are formed in the track (100) along the length direction of the track (100). A driving member is provided on the plate body (120) for driving the claw jaws (121) on both sides to rotate simultaneously at the hinged joints on the plate body (120), so as to drive the claw jaws (121) on both sides to be inserted into the fixing openings (122) simultaneously. The driving member includes a driving block (123), a connecting rod (124) and a driving part. Connecting rods (124) are hingedly disposed on both sides of the driving block (123). The ends of the two connecting rods (124) away from the driving block (123) are hingedly disposed on the claw jaws (121). The driving part is used to drive the driving block (123) to move up and down.

2. The installation structure of the airborne operation console according to claim 1, characterized in that: The driving part includes a driving electric cylinder (125) fixedly disposed on the plate body (120) and located between the claw jaws (121) on both sides. The driving block (123) is fixedly disposed on the driving end of the driving electric cylinder (125).

3. The installation structure of the airborne operation console according to claim 1, characterized in that, A slot (126) is formed in one of the claw jaws (121), and a plug block (127) for being inserted into the slot (126) is provided on the other claw jaw (121).

4. The installation structure of the airborne operation console according to claim 3, characterized in that, A fixing member for preventing the plug block (127) from disengaging from the slot (126) is provided on the driving block (123).

5. The installation structure of the airborne operation console according to claim 4, wherein, The fixing member includes a fixing electric cylinder (130) and a fixing rod (131). The fixing rod (131) is fixedly disposed on the driving end of the fixing electric cylinder (130). The fixing electric cylinder (130) is disposed on the surface of the driving block (123) facing away from the plate body (120). Fixing holes for allowing the fixing rod (131) to pass through are formed in the plug block (127) and the two claw jaws (121).

6. The installation structure of the airborne operation console according to claim 1, characterized in that, The plate body (120) includes a first connecting plate (140) and a second connecting plate (141). The first connecting plate (140) is disposed on the frame (110). The claw jaws (121) are hingedly disposed on the second connecting plate (141). An adjusting groove (142) is formed in the second connecting plate (141). The length direction of the adjusting groove (142) is arranged perpendicular to the length direction of the track (100). An adjusting block (143) slidably connected in the adjusting groove (142) is provided on the first connecting plate (140). An adjusting member for fixing the adjusting block (143) to any position after movement is provided in the adjusting groove (142).

7. The installation structure of the airborne operation console according to claim 6, characterized in that, The adjusting member includes a screw rod (144) and an adjusting motor (145). The screw rod (144) is rotatably arranged in the adjusting groove (142) along the length direction of the adjusting groove (142). The adjusting block (143) is sleeved and threadedly connected to the screw rod (144). The adjusting motor (145) is fixedly arranged on the first connecting plate (140), and the adjusting motor (145) is used to drive the screw rod (144) to rotate.

8. The installation structure of the airborne operation console according to claim 1, characterized in that The track (100) includes a plurality of connecting rails (150) spliced together. On the opposite surfaces of adjacent connecting rails (150), there are respectively provided a connecting groove (151) and a connecting block (152) that cooperate with each other. Bolts for detachably connecting the connecting block (152) into the connecting groove (151) are provided on the connecting rail (150).

Images