民用飞机刹车系统CCAR 25.735条款适航研究

介绍了民用飞机适航规章CCAR-25-R4最新版并与前一版本R3版在刹车系统主条款25.735条进行对比分析,详细解释了R4版与R3版的不同之处及更改原因,阐述了R4版735条的详细要求,提供了刹车系统的适航思路及符合性方法建议。最后进行了小结并提出了下一步目标。     

Gd、Y 对ZK60 镁合金腐蚀行为的影响

通过盐雾腐蚀实验并结合SEM和XRD分析,研究了稀土元素对锻造态ZK60镁合金腐蚀行为的影响.结果表明,ZK60合金耐蚀性较差,而在ZK60中添Gd、Y后的合金,其耐蚀性明显提高.腐蚀时间相同时,两种合金的微观腐蚀形貌不相同,ZK60合金腐蚀坑的形成时间较早(14 d),而添加Gd、Y后的ZK60合金腐蚀坑的形成时间较晚(21 d),添加Gd、Y后ZK60合金的腐蚀产物相对致密.两种镁合金的腐蚀产物均为Mg(OH)2,Mg(OH)2腐蚀产物膜极易发生开裂,形成网块状的腐蚀产物膜.腐蚀产物膜的进一步生长、开裂和脱落,加速了材料的腐蚀流失.     

MA60飞机水上漂浮特性研究

MA60飞机的水漂浮特性是通过从初始淹没深度、漂浮的稳定性、水的渗漏途径、有效漂浮时间和应急撤离时间等方面进行分析和论证的,证明其漂浮特性能满足水上迫降后乘员应急撤离的要求。     

Influence of welding parameters on microstructure and mechanical properties of electron beam welded Ti60 to GH3128 joint with a Cu interlayer

Effects of welding parameters on the microstructure and mechanical properties of Ti/Cu/Ni joint welded by electron beam were investigated. High welding heat input increased the melting quantity of Ti60 titanium alloy and promoted the formation of Ti–Cu intermetallic compounds (IMC) such as Ti₂Cu and Ti₃Cu₄, increasing the brittleness of the joints. Low welding heat input was not conducive to the complete melting of the copper interlayer, and the unmelted copper reduced the performance of the joints. Under the optimal welding parameters, Ti–Ni IMCs in the weld would be replaced by (Cu, Ni) solid solutions ((Cu, Ni)_ss). However, Ti–Cu IMC layers cannot be eliminated entirely by changing the welding parameters. The maximum tensile strength of the joints was 201 MPa. The fracture of the joints occurred at the Ti–Cu IMC layer, which was a typical brittle fracture.     

含C60的RDX-CMDB推进剂性能研究

通过燃速、爆热、活化能和温度分布等参数的测试和计算，发现C(60)能显著提高推进剂的火焰温度和燃烧表面温度，降低压强指数，使平台区范围变宽且向高压方向移动，推进剂的爆热也提高约10％。此外从反应机理上提出C(60)-Pbx络合物的催化作用，改善了RDX－CMDB推进剂燃烧性能；富集物（含10％C(60)的烟炱）中C(60)主要以分子状态存在，因此它能把C(60)均匀分散到推进剂中，而且保持C(60)化学活性，比纯C(60)的催化效果更好。     

黑鹰直升机旋翼桨叶防/除冰系统研究

旋翼系统是直升机的关键动部件之一,旋翼桨叶结冰会降低直升机性能,危及飞行安全。为了使直升机具备全天候飞行能力,有必要在直升机上安装旋翼桨叶防/除冰系统。黑鹰直升机上装备的电热防除冰系统是美国西科斯基公司最早开发的比较成功的一款旋翼防/除冰系统。详细介绍黑鹰直升机旋翼防/除冰系统的发展历程和设计特点,对比了UH-60A和UH-60M直升机上防/除冰系统的异同。     

Experimental research on electrochemical machining of titanium alloy Ti60 for a blisk

Ti60(Ti–5.6Al–4.8Sn–2Zr–1Mo–0.35Si–0.7Nd) is a high-temperature titanium alloy that is now used for important components of aircraft engines. Electrochemical machining(ECM) is a promising technique that has several advantages, such as a high machining rate, and can be used on a wide range of difficult-to-process materials. In this paper, orthogonal experiments are conducted to investigate ECM of Ti60, with the aim of determining the influences of some electrochemical process parameters on the surface roughness. The most important parameter is found to be the frequency of the pulsed power supply. It is found that using suitably optimized parameters for ECM can greatly decrease the surface roughness of a workpiece. A surface roughness of approximately 0.912 lm can be obtained with the following optimal parameters: Na Cl electrolyte concentration 13wt%, voltage20 V, pulse frequency 0.4 k Hz, duty cycle 0.3, temperature 23 °C, and anode feed rate 0.5 mm/min.Furthermore, blisk blades have been successfully processed using these optimized parameters.