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抗G应变动作的初步性能:呼吸需求和呼吸系统影响

Pilot performance of the anti-G straining maneuver: respiratory demands and breathing system effects.

作者信息

Whitley P E

机构信息

Department of Neurosurgery, Medical College of Pennsylvania, Philadelphia, USA.

出版信息

Aviat Space Environ Med. 1997 Apr;68(4):312-6.

PMID:9096827
Abstract

INTRODUCTION

The anti-G straining maneuver (AGSM) is still an important part of pilot protection for G-induced loss of consciousness. The specific requirements for and the effects of breathing systems on the performance of the AGSM are essential elements to designing compatible breathing systems.

METHODS

Subject pools of 27 and 34 naval aviators were recruited and used to measure the inhalatory and exhalatory flow requirements for the AGSM and the breathing system effects of mask cavity pressure during AGSM performance on the Naval Air Warfare Center Dynamic Flight Simulator at acceleration levels up to 8 Gz.

RESULTS

The mean peak inhalatory flow was 125.5 L.min-1 (n = 135, SD = 42.1) with a maximum value of 274 L.min-1. The mean peak exhalatory flow was 154.4 L.min-1 (n = 135, SD = 49.6) with a maximum value of 308 L.min-1. For the effects of the breathing system on AGSM performance, inhalatory mask cavity pressures were not above 30 mmHg with the majority less than 10 mmHg. Exhalatory mask cavity pressures did not exceed 60 mmHg but predominated in the 20-30 mmHg range. In comparison to accepted guidelines, 67-77% of inhalatory mask cavity pressures were below and 91% of the exhalatory mask cavity pressures were above the Air Standardization and Coordination Committee (ASCC) limit of +/- 14 mmHg.

CONCLUSIONS

The difference in the peak inhalatory and exhalatory flows measured during this study and clinically can be attributed to different test conditions and performer techniques. The reduction in inhalatory flow with increasing G is consistent with the increase in breathing difficulty due to the G load and the inflation of the anti-G suit. However, exhalatory mechanics appear unaffected by the G load and the inflation of the anti-G suit. Since 23-33% of the inhalatory mask cavity pressures were above this ASCC limit, improvements in regulator performance are still needed. For exhalatory effects of the breathing system, the main contributor is the mask valve. While no pilot suffered unconsciousness or expressed complaints with the breathing systems used, these exposures were of short duration. The additional work of breathing during a combat engagement may further compromise the pilot's ability to retain consciousness with the AGSM.

摘要

引言

抗G应变动作(AGSM)仍是预防飞行员因G力导致意识丧失的重要措施。呼吸系统对抗G应变动作性能的具体要求和影响是设计兼容呼吸系统的关键要素。

方法

招募了27名和34名海军飞行员作为受试者,在海军空战中心动态飞行模拟器上,以高达8Gz的加速度水平,测量抗G应变动作的吸气和呼气流量要求,以及抗G应变动作执行过程中面罩腔压力对呼吸系统的影响。

结果

平均吸气峰值流量为125.5L·min⁻¹(n = 135,标准差 = 42.1),最大值为274L·min⁻¹。平均呼气峰值流量为154.4L·min⁻¹(n = 135,标准差 = 49.6),最大值为308L·min⁻¹。对于呼吸系统对抗G应变动作性能的影响,吸气时面罩腔压力不高于30mmHg,大多数低于10mmHg。呼气时面罩腔压力不超过60mmHg,但主要集中在20 - 30mmHg范围内。与公认指南相比,67 - 77%的吸气面罩腔压力低于、91%的呼气面罩腔压力高于空军标准化与协调委员会(ASCC)规定的±14mmHg限值。

结论

本研究测量的吸气和呼气峰值流量与临床情况的差异可归因于不同的测试条件和执行者技术。随着G值增加吸气流量降低,这与G负荷和抗G服充气导致的呼吸困难增加相一致。然而,呼气机制似乎不受G负荷和抗G服充气的影响。由于23 - 33%的吸气面罩腔压力高于该ASCC限值,仍需要改进调节器性能。对于呼吸系统的呼气影响,主要因素是面罩阀。虽然没有飞行员因所使用的呼吸系统而失去意识或表示不适,但这些暴露时间较短。战斗过程中额外的呼吸负荷可能会进一步削弱飞行员通过抗G应变动作保持意识的能力。

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