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在扩展覆盖范围的抗荷服中对一种概念性腹部膀胱约束装置进行离心机人体评级。

Centrifuge man-rating of a conceptual internal abdominal bladder restraint in an extended coverage anti-G suit.

作者信息

Balldin U I, Krock L P, Danielsson C H, Johansson S A

机构信息

Armstrong Laboratory, Brooks AFB, Texas 78235-5104, USA.

出版信息

SAFE J. 1996 Jul;26(2):42-6.

Abstract

An extended coverage anti-G suit, has been demonstrated to improve +Gz tolerance substantially. In some pilots/subjects, however, the abdominal bladder of the anti-G suit may expand excessively upward and inward causing discomfort and pain. This man-rating was performed to evaluate the effects on +Gz protection of an internal abdominal bladder restraint in the Swedish Tactical Flight Combat Suit (TFCS) used in conjunction with pressure breathing during G (PBG). The tests were executed in the Armstrong Laboratory Centrifuge at Brooks AFB with four Swedish test fighter pilots. The centrifuge profiles included gradual onset runs (GOR, relaxed) and rapid onset runs (ROR, with straining), as well as simulated aerial combat maneuver (SACM) runs up to +9 Gz until subjects experienced light loss or fatigue or surpassed 228 s. All subjects withstood 60 s at +9 Gz during GOR and ROR runs with and without abdominal bladder restraint. No difference There was no difference in SACM duration times. In three of four subjects, abdominal pain or discomfort experienced without abdominal bladder restraint disappeared with the addition of a bladder restraint. Ratings of perceived exertion (after 5 peaks at +9 Gz in the SACM), subjective +Gz tolerance, overall comfort, fatigue, and heat stress demonstrated no relevant differences with and without abdominal bladder restraint. Therefore, to enhance comfort, it seems possible to modify the TFCS by adding an abdominal bladder internal restraint without compromising its operational +Gz protection.

摘要

一种扩展覆盖的抗荷服已被证明能显著提高对正加速度(+Gz)的耐受性。然而,在一些飞行员/受试者中,抗荷服的腹部气囊可能会过度向上和向内扩张,导致不适和疼痛。此次人体评级旨在评估瑞典战术飞行作战服(TFCS)中腹部内部气囊约束装置在与G值作用期间的压力呼吸(PBG)配合使用时,对+Gz防护效果的影响。测试在布鲁克斯空军基地的阿姆斯特朗实验室离心机上,由四名瑞典测试战斗机飞行员进行。离心机测试剖面包括逐渐增加加速度的运行(GOR,放松状态)和快速增加加速度的运行(ROR,用力状态),以及模拟空战机动(SACM)运行,加速度可达+9Gz,直至受试者出现轻度失能或疲劳,或超过228秒。在有和没有腹部气囊约束的情况下,所有受试者在GOR和ROR运行中都能在+9Gz下承受60秒。SACM持续时间没有差异。在四名受试者中的三名中,没有腹部气囊约束时所经历的腹痛或不适在增加气囊约束后消失。主观用力程度评级(在SACM中+9Gz下达到5个峰值后)、主观+Gz耐受性、总体舒适度、疲劳程度和热应激在有和没有腹部气囊约束的情况下均无显著差异。因此,为提高舒适度,似乎可以通过添加腹部内部气囊约束来改进TFCS,而不会损害其在操作中的+Gz防护能力。

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