Department of Orthopaedic Surgery, National University of Singapore, Singapore .
Am J Sports Med. 2010 Apr;38(4):816-23. doi: 10.1177/0363546509350465. Epub 2010 Jan 21.
Structural changes of articular cartilage at the point of peak displacement compression during a landing impact are unknown.
Extent of damage and deformation is significantly different for superficial, middle, and deep cartilage zones at peak displacement compression during simulated landing impact compared with after impact.
Controlled laboratory study.
Explants were extracted from porcine tibial cartilages and divided into 3 test conditions: nonimpact control, impact and release, and impact and hold. Impact compression, with peak deformation of 2 mm, was applied based on a single 10-Hz haversine to simulate landing impact. For impact and release, explants were subjected to formalin fixation on removal of load after impact. For impact and hold, explants were immediately immersed in formalin with peak deformation maintained at 2 mm. After fixation, the explants underwent histology, whereby Mankin scores and cartilage thicknesses were obtained.
Peak stresses of 9.8 to 28.1 MPa were noted during impact compression. For impact and release, substantial cartilage defects such as surface fraying and fissures were observed. For impact and hold, explants exhibited less severe matrix damage, such as superficial irregularities and tidemark disruption. Mankin scores were lower (indicating less damage; P <.05) in impact and hold than in impact and release condition. Superficial cartilage zone thickness was reduced (P <.05) in both impact and hold and impact and release conditions, relative to nonimpact control.
Not only does the loading phase of impact compression play a role in introducing substantial damage and deformation to cartilage, the unloading phase contributes to overall cartilage damage by exacerbating fissure propagation from surface lesions. Clinical Relevance Imaging of clinical injuries may underestimate the magnitude of cartilage compression that occurred during injury. Cartilage tissue engineering scaffolds must be designed to cope with the effects of loading and unloading phases, especially at the superficial zone, so that the repair site can function as well as does the neighboring native cartilage.
在着陆冲击时的峰值位移压缩点处,关节软骨的结构变化尚不清楚。
与冲击后相比,在模拟着陆冲击时的峰值位移压缩过程中,浅层、中层和深层软骨区的损伤和变形程度有显著差异。
对照实验室研究。
从猪胫骨软骨中提取样本,并分为 3 种测试条件:非冲击对照、冲击释放和冲击保持。冲击压缩,峰值变形为 2mm,应用基于 10Hz 正弦波的单一冲击来模拟着陆冲击。对于冲击释放,样本在冲击后去除负荷时进行福尔马林固定。对于冲击保持,样本在峰值变形保持在 2mm 的情况下立即浸入福尔马林。固定后,样本进行组织学检查,获得 Mankin 评分和软骨厚度。
冲击压缩过程中记录到 9.8 至 28.1MPa 的峰值应力。对于冲击释放,观察到明显的软骨缺陷,如表面磨损和裂缝。对于冲击保持,样本表现出较轻的基质损伤,如浅层不规则和潮痕破坏。冲击保持的 Mankin 评分低于冲击释放(表明损伤较小;P<.05)。与非冲击对照相比,冲击保持和冲击释放条件下的浅层软骨区厚度均减少(P<.05)。
冲击压缩的加载阶段不仅对软骨造成了严重的损伤和变形,卸载阶段还通过加剧表面损伤处的裂缝扩展,导致整体软骨损伤。临床意义:对临床损伤的影像学检查可能低估了损伤过程中发生的软骨压缩程度。软骨组织工程支架的设计必须考虑到加载和卸载阶段的影响,特别是在浅层,以确保修复部位能够像相邻的天然软骨一样正常发挥功能。