期刊文献+

M-3抗荷动作的呼吸循环效应 被引量:7

Effects of M-3 maneuver on respiration and circulation
原文传递
导出
摘要 为了阐明M-3动作的G防护原理,在+1GZ条件下研究了其呼吸循环效应并与M-1和L-1动作进行了对比。实验中,测量了12名航空医学生实施上述三种抗G动作时的胸内压、每搏输出量、心水平收缩压、呼吸流率及呼吸压力等参量。结果显示,M-3、M-1动作呼气相及L-1动作屏气期胸内压分别为8.1、8.7及8.8kPa,三种动作每搏输出量分别减少16.4%、19.9%及23.2%。M-3动作胸内压升高值、每搏输出量减少值、心水平收缩压及呼吸频率与M-1动作无显著性差异(P>0.05),而与L-1动作有显著性差异(P<0.05)。M-3动作的平均吸气流率、平均呼气流率及呼(吸)气量显著高于M-1动作(P<0.05)。M-3动作的声门关闭度和声门呼气阻力小于M-1动作。实施抗G动作时,为了减轻每搏输出量的降低程度,应该采取措施,增加回心血量。 To explore the protective machanism of M-3 maneuver, its effects on respiration andcirculation were studied and compared with M-1 and L-1 maneuvers under + 1 Gz. Subjects were 12aviation medical students. Intrapleural pressure, stroke volume (SV), respiratory flow, respiratory pressure,heart-level systolic pressure were measured during these anti-G maneuvers. The results showedthat intrapleural pressure during expiratory phase of M-3 and M-1 and holding breath phase of L-1 were8. 1, 8- 7, and 8. 8 kPa respectively,while SV decreased 16. 4%, 19. 9%,and 23. 2% respectively in M-3,M-1and L-1 maneuvres. During M-3 maneuver, the increased value of intraplueral pressure, decreasedvalue of SV,heart-level systolic pressure and respiratory frequency compared with the M-1 maneuverhad no significant difference (P<0.05 );compared with those of L-1 maneuver,the difference was significant (P<0.05). Mean inspiratory flow,mean expiratory flow and expiratory (inspiratory) volume during M-3 maneuver were higher than those of M-1 maneuver (P<0.05). The closing degree of glottisand expiratory resistance of glottis during M-3 maneuver are less than those of M-1 maneuver. Measuresfor enhancing return of blood to heart should be adopt in order to alleviate reduction of the SV duringanti-G maneuver.
出处 《中华航空医学杂志》 CSCD 1995年第1期21-25,共5页
关键词 对抗动作 抗荷 M-3抗荷动作 呼吸循环效应 Anti-G maneuver Intraplueral pressure Stroke volume Respiratory flow
  • 相关文献

参考文献2

  • 1李兵林.关于呼吸防护装备的呼吸阻力负荷[J]军队卫生杂志,1985(03).
  • 2马瑞山,倪鹤鹦,张立藩.飞行人员航空供氧装备外加呼吸阻力容许水平的测定[J]第四军医大学学报,1985(01).

同被引文献100

引证文献7

二级引证文献79

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部