中华航空航天医学杂志
中華航空航天醫學雜誌
중화항공항천의학잡지
CHINESE JOURNAL OF AEROSPACE MEDICINE
2013年
1期
34-38,封2
,共6页
吴迪%伍骥%郑超%黄蓉蓉%卜伟平%柳松杨
吳迪%伍驥%鄭超%黃蓉蓉%蔔偉平%柳鬆楊
오적%오기%정초%황용용%복위평%류송양
航空%踝关节%外侧韧带,踝%关节囊%踝损伤%生物力学
航空%踝關節%外側韌帶,踝%關節囊%踝損傷%生物力學
항공%과관절%외측인대,과%관절낭%과손상%생물역학
Aviation%Ankle joint%Lateral ligament,ankle%Joint capsule%Ankle injuries%Biomechanics
目的 模拟空降兵着陆瞬间踝关节由跖屈位到内翻位的变化,测定外侧副韧带及关节囊等软组织损伤时的负荷,并分析其在受力过程中所表现的特性,为研制新式伞兵护踝及伞靴提供理论依据. 方法 采用人体踝关节标本6具,通过自制夹具固定在MTS-858生物材料试验机上,施加轴向力,轴向压缩范围10 cm,当负荷曲线出现峰值时停止.记录负荷峰值及达到峰值的时间,绘制负荷-时间曲线. 结果 模拟空降兵着陆瞬间踝关节由跖屈位到内翻位试验中,标本踝关节负荷在达到峰值前随时间逐渐增加,达到峰值后迅速下降.负荷峰值约2207.18 N,达到峰值时间约9.76s.当负荷达到峰值时,踝关节外侧副韧带及关节囊主要呈现钝性断裂损伤,断端极不整齐.全部标本经C型臂摄X线片,均无骨性损伤. 结论 模拟空降兵跳伞着陆瞬间踝关节由跖屈状态到内翻状态下,外侧副韧带及关节囊纤维组织在负荷-时间曲线中表现出“等长收缩”及“等张收缩”特性.本试验为改进护踝或伞靴设计,以更好地防止外侧副韧带及相关软组织损伤提供了一定的理论依据.
目的 模擬空降兵著陸瞬間踝關節由蹠屈位到內翻位的變化,測定外側副韌帶及關節囊等軟組織損傷時的負荷,併分析其在受力過程中所錶現的特性,為研製新式傘兵護踝及傘靴提供理論依據. 方法 採用人體踝關節標本6具,通過自製夾具固定在MTS-858生物材料試驗機上,施加軸嚮力,軸嚮壓縮範圍10 cm,噹負荷麯線齣現峰值時停止.記錄負荷峰值及達到峰值的時間,繪製負荷-時間麯線. 結果 模擬空降兵著陸瞬間踝關節由蹠屈位到內翻位試驗中,標本踝關節負荷在達到峰值前隨時間逐漸增加,達到峰值後迅速下降.負荷峰值約2207.18 N,達到峰值時間約9.76s.噹負荷達到峰值時,踝關節外側副韌帶及關節囊主要呈現鈍性斷裂損傷,斷耑極不整齊.全部標本經C型臂攝X線片,均無骨性損傷. 結論 模擬空降兵跳傘著陸瞬間踝關節由蹠屈狀態到內翻狀態下,外側副韌帶及關節囊纖維組織在負荷-時間麯線中錶現齣“等長收縮”及“等張收縮”特性.本試驗為改進護踝或傘靴設計,以更好地防止外側副韌帶及相關軟組織損傷提供瞭一定的理論依據.
목적 모의공강병착륙순간과관절유척굴위도내번위적변화,측정외측부인대급관절낭등연조직손상시적부하,병분석기재수력과정중소표현적특성,위연제신식산병호과급산화제공이론의거. 방법 채용인체과관절표본6구,통과자제협구고정재MTS-858생물재료시험궤상,시가축향력,축향압축범위10 cm,당부하곡선출현봉치시정지.기록부하봉치급체도봉치적시간,회제부하-시간곡선. 결과 모의공강병착륙순간과관절유척굴위도내번위시험중,표본과관절부하재체도봉치전수시간축점증가,체도봉치후신속하강.부하봉치약2207.18 N,체도봉치시간약9.76s.당부하체도봉치시,과관절외측부인대급관절낭주요정현둔성단렬손상,단단겁불정제.전부표본경C형비섭X선편,균무골성손상. 결론 모의공강병도산착륙순간과관절유척굴상태도내번상태하,외측부인대급관절낭섬유조직재부하-시간곡선중표현출“등장수축”급“등장수축”특성.본시험위개진호과혹산화설계,이경호지방지외측부인대급상관연조직손상제공료일정적이론의거.
Objective To determine the load of causing parachutist's lateral collateral ligament and the joint capsule injuries by investigating the ankle inversion from plantar flexion to varus position under simulated landing state,and to analyze its stress features in order to provide theoretical reference to the development of Chinese Air Force Paratrooper boots and ankle brace.Methods Six human ankle specimens were fixed on the MTS-858 biomechanical testing machine by the self-made fixture.The axial compression range was 10 cm.The axial force was applied until the load curve appeared peak.The force and the time to peak were recorded,as well as the load time curve.Results In the simulation of ankle inversion from plantar flexion to varus position,the average peak force was 2207.18 N,and the average time to the peak was 9.76 s.The load curve showed such feature as gradual increase and sharp drop.The dissection showed that the lateral collateral ligament and the joint capsule had inactive ruptured injuries with irregular section as the peak force applied.X-ray examination indicated no osseous injuries in all specimens.Conclusions The ankle's lateral collateral ligament and joint capsule would show isometric and isotonic contraction features in the load-time curve as overcoming the ankle change from plantar flexion to varus position under simulated landing state.Those would provide theoretical reference in improving paratrooper boots and ankle brace in order to prevent ankle from lateral collateral ligament and the related soft tissue injuries.