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An aircraft seat with head cushioning and anti-collision function

An aircraft seat and anti-collision technology, which is applied to aircraft parts, seat layout, crew accommodation, etc., can solve the problems of losing protection of passengers, failure to protect passengers, and seat falling off, etc.

Active Publication Date: 2022-06-07
SHENZHEN LOTUT INNOVATION DESIGN CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

NTSB U.S. air accident investigators found a fact in the investigation that the seats designed in 1953 to withstand 9 G overloads did not play a very good role in protecting passengers during the crash. During the collision of G's plane, the supporting legs of the plane seat broke, causing the passenger to fly up from the seat fixed by the seat belt and hit the passenger in front
The fuselage and floor of the plane are still intact, and the safety belt of the plane is not broken, but the seat of the plane has fallen off, so the passengers who are tied to the seat with the safety belt, because the safety integrity of the plane seat is destroyed, lost The role of protecting passengers

Method used

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  • An aircraft seat with head cushioning and anti-collision function
  • An aircraft seat with head cushioning and anti-collision function
  • An aircraft seat with head cushioning and anti-collision function

Examples

Experimental program
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Effect test

Embodiment 1

[0025] Example one, as figure 1 As shown in the figure, an aircraft seat with head buffering and anti-collision function according to an embodiment of the present invention includes a seat cushion 1, a backrest 2 is provided on one side of the top of the seat cushion 1, and a backrest 2 is provided in the middle of both sides of the backrest 2 Armrest 3, the top of the backrest 2 is provided with a headrest, the headrest includes a headrest body 4, and headrest side wings 5 ​​are provided on both sides of the headrest body 4. The headrest side wings 5 ​​are all movably connected by bolts 8, a support frame 6 is arranged in the headrest side wings 5, a buffer 7 is arranged between the headrest side wings 5 ​​and the support frame 6, A buffer area 9 is provided in the middle of the opposite side of the headrest side wings 5, and a fastener 10 and a connecting piece 11 are provided at the bottom of the opposite side of the headrest side wings 5 ​​on both sides. The fasteners 10 a...

Embodiment 2

[0026] Example two, as figure 2 As shown, the buffer 7 is pearl cotton, the buffer 9 is filled with foam particles, and the foam particles are made of pearl cotton.

Embodiment 3

[0027] Example three, as figure 2 As shown, the headrest body 4 is filled with pearl cotton, the support frame 6 is made of low-alloy steel material, and the diameter of the circular hole at the center of the connecting piece 11 is slightly larger than the diameter of the fixing piece 14 .

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PUM

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Abstract

The invention discloses an aircraft seat with head cushioning and anti-collision function, comprising a seat cushion, a backrest is arranged on one side of the top of the seat cushion, armrests are arranged in the middle of both sides of the backrest, and a headrest is arranged on the top of the backrest. The headrest includes a headrest body, and both sides of the headrest body are provided with headrest wings, and the headrest body and the headrest wings on both sides are movably connected by bolts. A supporting frame is arranged in the side of the pillow, and a buffer is provided between the side of the headrest and the supporting frame. Fasteners and connectors are provided on the bottom of one side, and vertical grooves and horizontal grooves are arranged in the fasteners, and the horizontal grooves are located at the lower right of the vertical grooves, and the vertical grooves A spring washer 1 is arranged at the bottom of the groove. Beneficial effect: the buffer zone can effectively prevent the passenger's head from colliding with other objects due to forward tilt.

Description

technical field [0001] The present invention relates to the technical field of seats, in particular to an aircraft seat with a head buffering and anti-collision function. Background technique [0002] In the 1970s, with the new technological revolution and the development of science and technology, a large number of alloy materials began to be used in aircraft seats. Aircraft seats are getting lighter and lighter, but the overloads experienced by aircraft seats have continued to the 9 G overload required in the 1952's. Since 1980, the normal landing speed of large jet airliners can reach 280 km / h, and the braking overload acting on the human body during the crash can reach 25G. The aircraft is still installed in accordance with the previous standard. chair. On January 25, 1990, Colombian Airlines Flight 052, a Boeing 707 with old-fashioned seats crashed on the mountains of Long Island near the New York Airport due to running out of fuel. The plane fell into two pieces unde...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D11/06
CPCB64D11/0619Y02T50/40
Inventor 王忠林
Owner SHENZHEN LOTUT INNOVATION DESIGN CO LTD
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