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A head and neck guard for an ejection rescue seat of a fighter pilot

A protection device and technology for pilots, applied in the field of ejection and life-saving for fighter pilots, can solve the problems of large space occupied by airbags, poor individual adaptability, and large space occupation, and achieve the effects of reducing head and neck injuries, satisfying light weight and simple structure

Inactive Publication Date: 2019-01-15
TSINGHUA UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] However, the patent US 7,878,452 B2 has three technical defects: it adopts a mechanical structure completely, and the structure is complex; it takes up a lot of space and is heavy; the ability of the lateral pillars to limit the left and right movement of the head is limited
The patent US 2013 / 0187003 A1 has two technical defects: the way of enveloping the head and neck with the airbag takes up a lot of space, which is extremely unfavorable for the aerodynamic performance of the seat system during flight; the head is fixed to the seat through the rear airbag Forward flexion position, not flexible drive, poor individual adaptability, may cause head and neck injury

Method used

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  • A head and neck guard for an ejection rescue seat of a fighter pilot
  • A head and neck guard for an ejection rescue seat of a fighter pilot
  • A head and neck guard for an ejection rescue seat of a fighter pilot

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Embodiment Construction

[0027] The present invention will be described in further detail below in conjunction with the accompanying drawings.

[0028] The invention relates to a head and neck protection device for a fighter pilot's ejection lifesaving seat. The head and neck protection device is composed of an air bag 1, a scroll spring power device 2 nested inside and outside, a rotating shaft 3, and a headrest panel 4; the air bag 1 is composed of a lateral air bag 5 and a horizontal air bag 6; the power device 2 is composed of Housing 21, stop pin 22, reel 23, scroll spring 24, ratchet 25, ratchet 26 form; Reel 23 is made up of housing two 231, stop pin two 232, scroll spring two 233. The power unit 2 and the airbag 1 are one on each side, and are fixedly connected together. The rotating shaft 3 is installed on the casing 21 of the power unit 2 and can rotate relative to the casing 21 of the power unit 2. The headrest panel 4 is fixed on the rotating shaft 3. It cannot move relative to the axis 3...

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PUM

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Abstract

A head and neck guard for an ejection rescue seat of a fighter pilot includes a headrest panel. The headrest panel is arranged on that rotating shaft, the two sides of the rotating shaft are connectedwith the airbag through a volute spring power device nested inside and outside. An air bag is compose of a lateral air bag and a transverse air bag. When the ejection seat is not activated, and whennot working, rotation of the drum is restricted by a stop pin in a powder unit. The rotation of the rotary shaft is limited by the stopper pin 2 in the drum, so that the headrest panel is in a fixed state and does not affect the pilot to normally fly the aircraft. When the ejection seat is started, the stopper pin is ejected by the gas, so that the drum can be rotated under the drive of the volutespring, and the head rest panel on the rotary shaft is driven to rotate forward to follow the head movement. At that same time, the air bag is star to start to support the head and neck, and the forward movement distance of the head can also be reduced. The head and neck guard not only solves the problem that the head is fixed to a specific position, but also avoids the problem that the head andneck of the human body are damaged by rigid driving.

Description

technical field [0001] The invention relates to the technical field of ejection lifesaving for fighter pilots, in particular to a head and neck protection device for a fighter pilot ejection lifesaving seat. Background technique [0002] Many fighter jets have crashed in air combat and training, and ejection rescue is the last resort to save the lives of pilots when fighter jets crash. However, the acceleration of up to 16-25G during ejection can cause cervical spine fractures, neck breaks, and concurrent brain damage, and even death. At the beginning of the ejection, the pilot's head and neck are affected by the acceleration, and the head is bowed forward; after the ejection, the pilot's head is hit by the airflow, and it will be violently thrown backwards or sideways, which can easily cause head and neck injuries. injury or even death. [0003] US patents US 7,878,452 B2 and US 2013 / 0187003 A1 have reported two types of deployable headrest devices; the specific technical...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D25/10B64D25/115
CPCB64D25/10
Inventor 宋润滋索双富贾晓红王子羲郭飞王洋王文杰
Owner TSINGHUA UNIV
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