Aircraft seat

Abstract

The utility model relates to the technical field of aircraft seats, in particular to an aircraft seat. Comprising a chair body, one side of the chair body is provided with a storage groove and an insertion groove, a plate body is inserted in the storage groove, a sliding groove is formed in the plate body, a hinge rod is installed in the insertion groove, a rotating shaft is connected to the hinge rod in a matched mode, the rotating shaft is slidably connected into the sliding groove, supporting blocks are fixedly connected to the positions, located on the two sides of the plate body, of the rotating shaft, and locking nails are in threaded connection to the two supporting blocks. And the hinge rod is rotatably connected with the rotating shaft through a connecting piece. The connecting piece is a bolt. And a rubber pad is arranged at the rotating joint of the rotating shaft and the bolt. The beneficial effects are that passengers can easily realize isolation from adjacent passengers according to needs, thus greatly reducing virus spread risks, improving travel safety and comfort, and providing separation and privacy for passengers.

Description

Technical Field

[0001] This utility model relates to the field of aircraft seat technology, and more specifically to an aircraft seat. Background Technology

[0002] In today's air travel environment, passengers are increasingly concerned about hygiene and safety during their journeys. While traditional aircraft seat designs can meet basic seating needs, they are significantly inadequate in preventing virus transmission, protecting passenger privacy, and providing isolation spaces. Furthermore, they fail to offer separation and privacy between passengers. Therefore, developing an aircraft seat that can effectively isolate passengers from their neighbors is of paramount importance. Utility Model Content

[0003] This invention provides an aircraft seat that allows passengers to easily isolate themselves from their neighbors as needed, thereby greatly reducing the risk of virus transmission, improving the safety and comfort of travel, and providing separation and privacy between passengers.

[0004] An aircraft seat includes a chair with a storage slot and a recess on one side. A plate is inserted into the storage slot, and a sliding groove is provided inside the plate. A hinge rod is installed in the recess, and a pivot is connected to the hinge rod. The pivot is slidably connected in the sliding groove. Support blocks are fixed to both sides of the pivot on both sides of the plate, and locking pins are threaded onto both support blocks.

[0005] The hinge rod and the rotating shaft are rotatably connected by a connector.

[0006] The connecting component is a bolt.

[0007] A rubber pad is provided at the rotatable connection between the shaft and the bolt.

[0008] A lug is fixed to the hinge rod, and a stud is rotatably connected to the lug. The lower end of the stud is threaded to the side of the chair. Attached Figure Description

[0009] The present invention will now be described in further detail with reference to the accompanying drawings and specific implementation methods.

[0010] Figure 1 This is a structural diagram of an aircraft seat panel in its stowed state.

[0011] Figure 2 A structural diagram showing the board used as a horizontal tabletop;

[0012] Figure 3 A schematic diagram of a plate used as a small baffle;

[0013] Figure 4A structural diagram showing the use of a large-area baffle that acts laterally on the plate.

[0014] Figure 5 This is a structural diagram of a chair;

[0015] Figure 6 A structural schematic diagram of the plate assembly;

[0016] Figure 7 This is a schematic diagram of the plate structure;

[0017] Figure 8 This is a schematic diagram of the rotating shaft.

[0018] Figure 9 This is a schematic diagram of the hinged rod structure;

[0019] Figure 10 This is a schematic diagram of the support block.

[0020] As shown in the figure: Chair 101; Storage slot 102; Slot 103; Arc groove 104; Magnet 105; Hinge rod 201; Rotating shaft 202; Bolt 203; Support block 204; Locking nail 205; Ear plate 206; Stud 207; Board 301; Slide 302; Groove 303. Detailed Implementation

[0021] See Figures 1 to 10 The diagram shows an embodiment of the present invention that enables isolation from adjacent passengers;

[0022] An aircraft seat includes a chair 101. A storage groove 102 and a slot 103 are provided on one side armrest of the chair 101. A plate 301 is inserted into the storage groove 102. A sliding groove 302 is provided inside the plate 301. A hinge rod 201 is installed in the slot 103. A pivot 202 is connected to the hinge rod 201. The pivot 202 is slidably connected in the sliding groove 302. Support blocks 204 are fixedly connected to both sides of the pivot 202 on the plate 301. Locking pins 205 are threadedly connected to both support blocks 204.

[0023] Normally, the panel 301 is stored in the storage slot 102. The slot 302 allows the panel 301 to slide on the pivot 202. When the panel 301 slides upwards, two locking pins 205 are tightened against the panel 301, locking its position relative to the pivot 202. This allows the panel 301 extending from the chair 101 to function as a small partition, providing partial isolation from adjacent passengers and effectively addressing the shortcomings of existing aircraft seats in isolating passengers. Figure 3As shown, passengers can easily isolate themselves from their seatmates as needed, thereby greatly reducing the risk of virus transmission and improving the safety and comfort of travel. At the same time, it provides separation and privacy between passengers, thus maintaining good social distancing without reducing seat density.

[0024] When it is necessary to remove the panel 301 for use as a tabletop, loosen the two locking screws 205 and completely pull the panel 301 out of the slot 103. After the lower end of the panel 301 contacts the pivot 202, rotate the panel 301 towards the other armrest until it is horizontal. The upper end of the panel 301 rests against the other armrest of the chair 101, thus completing the conversion of the panel 301 into a tabletop. Figure 2 As shown, when the board 301 is horizontally mounted on the two handrails, the board 301 also adheres to the two support blocks 204. The two support blocks 204 provide further support for the board 301, making the board 301 more stable during use.

[0025] See Figure 4 , 6 Figures 8 and 9 show schematic diagrams of an embodiment of the present invention, which uses a large-area baffle that can act laterally.

[0026] The hinge rod 201 and the rotating shaft 202 are rotatably connected by a connector;

[0027] The hinge rod 201 and the rotating shaft 202 are rotatably connected. Therefore, after the plate 301 is completely pulled out of the slot 103, the rotating shaft 202 can be rotated upwards by 90 degrees. The rotating shaft 202 will drive the plate 301 to rotate upwards by 90 degrees simultaneously. After adjusting the position of the plate 301 relative to the rotating shaft 202, the two locking screws 205 are tightened onto the plate 301 to fix its position relative to the rotating shaft 202. Figure 4 As shown, it is used to isolate passengers from those sitting next to it. At this time, the area of ​​the horizontally placed panel 301 that blocks the view between it and the adjacent seat becomes larger, and it can also be used as a large horizontal light shield or baffle.

[0028] See Figure 6 and 8 A schematic diagram of an embodiment of fixing the angle of the rotating shaft 202 according to the present invention is shown;

[0029] The connecting component is a bolt 203;

[0030] A rubber pad is provided at the rotatable connection between the rotating shaft 202 and the bolt 203;

[0031] The rubber pad increases the rotational friction, which makes it easier to fix the angle between the adjusted rotating shaft 202 and the hinge rod 201. After the rotating shaft 202 is rotated to the vertical position, the user removes the external force rubber pad to fix the position of the rotated shaft 202, thus completing the adjustment of the hinge rod 201 and the plate 301.

[0032] Further details:

[0033] The surface of the plate 301 is bonded with an anti-slip rubber pad;

[0034] It increases the friction between the object and the plate, preventing the object placed on the plate 301 from easily sliding due to vibration during flight.

[0035] See Figure 4 , 6 Figures 9 and 1 show schematic diagrams of embodiments of the present invention applicable to use for shielding at different height positions;

[0036] A lug 206 is fixedly connected to the hinge rod 201, and a stud 207 is rotatably connected to the lug 206. The lower end of the stud 207 is threaded to the side of the chair 101.

[0037] When plate 301 is as follows Figure 4 When used horizontally as shown, manually rotate the stud 207. The stud 207, through its threaded connection with the chair 101, drives the ear plate 206 and the hinge rod 201 to move upward. The hinge rod 201 drives the horizontally placed plate 301 to move upward, thereby changing the vertical position of the horizontally placed plate 301. This is suitable for use for blocking at different heights.

[0038] The upper end of the stud 207 is fixed with a rotating disc, which makes it easy to control the rotation of the stud 207 by holding the rotating disc.

[0039] See Figure 6 A schematic diagram of an embodiment of the present invention, which facilitates the lifting of the plate 301, is shown.

[0040] Grooves 303 are provided on both sides of the upper end of the plate 301;

[0041] The two grooves 303 facilitate manual upward lifting of the plate 301 to remove it from the slot 103.

[0042] See Figure 2 , 5 Figures 6 and 7 show schematic diagrams of an embodiment of the fixing plate 301 according to the present invention;

[0043] A magnet 105 is fixed to the other side of the chair 101, and a magnetic block is fixed to the groove 303 on the plate 301 near the magnet 105.

[0044] When the groove 303 on the board 301 is horizontally mounted and used as a table, the groove 303 on the board 301 will be embedded in the magnet 105, thereby limiting the horizontal movement of the board 301 and preventing the board 301 from moving horizontally during use.

[0045] Furthermore, the magnetic block in the groove 303 will magnetically attract the magnet 105, thereby further limiting the horizontal plate 301 and preventing the plate 301 from being easily lifted. The plate 301 will only be lifted and put away when a certain external force is manually applied.

[0046] See Figure 3 and 5 A schematic diagram of an embodiment of the easy-to-tighten locking pin 205 according to the present invention is shown;

[0047] The chair 101 has arc-shaped grooves 104 below the two locking pins 205; the two arc-shaped grooves 104 provide enough space to manually operate and tighten the two locking pins 205.

Claims

1. An aircraft seat, characterized in that, The chair (101) has a storage slot (102) and a slot (103) on one side. A plate (301) is inserted into the storage slot (102). A sliding groove (302) is opened inside the plate (301). A hinge rod (201) is installed in the slot (103). A pivot (202) is connected to the hinge rod (201). The pivot (202) is slidably connected in the sliding groove (302). Support blocks (204) are fixedly connected to both sides of the pivot (202) on the plate (301). Locking pins (205) are threaded onto both support blocks (204).

2. An aircraft seat according to claim 1, characterized in that, The hinge rod (201) and the rotating shaft (202) are rotatably connected by a connector.

3. An aircraft seat according to claim 2, characterized in that, The connecting component is a bolt (203).

4. An aircraft seat according to claim 3, characterized in that, A rubber pad is provided at the rotatable connection between the shaft (202) and the bolt (203).

5. An aircraft seat according to claim 1, characterized in that, The surface of the plate (301) is bonded with an anti-slip rubber pad.

6. An aircraft seat according to claim 1, characterized in that, An ear plate (206) is fixedly connected to the hinge rod (201), and a stud (207) is rotatably connected to the ear plate (206). The lower end of the stud (207) is threaded to the side of the chair (101).

7. An aircraft seat according to claim 6, characterized in that, A screw plate is fixed to the upper end of the stud (207).

8. An aircraft seat according to claim 5, characterized in that, Grooves (303) are provided on both sides of the upper end of the plate (301).

9. An aircraft seat according to claim 8, characterized in that, A magnet (105) is fixed to the other side of the chair (101), and a magnetic block is fixed in the groove (303) on the plate (301) near the magnet (105).

10. An aircraft seat according to claim 1, characterized in that, The chair (101) has an arc-shaped groove (104) located below the two locking pins (205).

Images