{"currentpage":1,"firstResult":0,"maxresult":10,"pagecode":5,"pageindex":{"endPagecode":5,"startPagecode":1},"records":[{"abstractinfo":"为研究不同<span style=\"color:red\">壳体</span><span style=\"color:red\">材料</span>对破片撞击带壳Comp B装药的影响,利用AUTODYN-2D软件建立破片撞击带壳炸药模型,对破片撞击、起爆不同<span style=\"color:red\">壳体</span>炸药的过程进行数值仿真.采用“升—降”法确定破片撞击带壳炸药的临界起爆速度,并定量分析了临界起爆速度随<span style=\"color:red\">壳体</span>密度、强度的变化规律,仿真计算结果能够较好地符合Jacobs-Roslund经验准则.<span style=\"color:red\">壳体</span><span style=\"color:red\">材料</span>采用钨合金时,临界起爆速度较高强工具钢提高了22.5％,较中强钢提高了24.4％,较铝提高了38.8％.仿真结果表明破片撞击起爆带有高密度、高强度<span style=\"color:red\">材料</span><span style=\"color:red\">壳体</span>的炸药时,临界速度更高.为传统弹药的改进及不敏感战斗部的设计提供了<span style=\"color:red\">壳体</span><span style=\"color:red\">材料</span>选择的依据.","authors":[{"authorName":"濮赞泉","id":"31d8089a-190e-40da-82d2-01db665a13cf","originalAuthorName":"濮赞泉"},{"authorName":"郑宇","id":"1c91b5f2-fba7-4b22-abcd-37fc054ed427","originalAuthorName":"郑宇"},{"authorName":"刘晓军","id":"627d0ddc-ffd9-41ff-9211-da021ca091e0","originalAuthorName":"刘晓军"},{"authorName":"王勇","id":"58795480-6917-4054-8863-5da722067cfb","originalAuthorName":"王勇"}],"doi":"","fpage":"12","id":"4e337511-7663-4ce4-b689-283425a74633","issue":"5","journal":{"abbrevTitle":"BQCLKXYGC","coverImgSrc":"journal/img/cover/BQCLKXYGC.jpg","id":"4","issnPpub":"1004-244X","publisherId":"BQCLKXYGC","title":"兵器材料科学与工程   "},"keywords":[{"id":"726e7a73-2507-4672-9246-6e83eb5a4817","keyword":"破片","originalKeyword":"破片"},{"id":"8fe4ec4b-d36d-4b59-ac1c-831349bcf4f2","keyword":"冲击起爆","originalKeyword":"冲击起爆"},{"id":"2d258205-adbb-4d0b-80b8-992d9d5536e3","keyword":"<span style=\"color:red\">壳体</span><span style=\"color:red\">材料</span>","originalKeyword":"壳体材料"},{"id":"18f7cbea-e662-4a78-833f-4ee6ec6baf8d","keyword":"数值模拟","originalKeyword":"数值模拟"}],"language":"zh","publisherId":"bqclkxygc201505004","title":"破片对不同<span style=\"color:red\">壳体</span>炸药冲击起爆研究","volume":"38","year":"2015"},{"abstractinfo":"热固型缠绕复合<span style=\"color:red\">材料</span><span style=\"color:red\">壳体</span>以其优异的性能在航空、军事和工业等领域得到了广泛应用,目前,制约其应用和发展的主要瓶颈是<span style=\"color:red\">壳体</span>的成本和性能,而<span style=\"color:red\">壳体</span>成型工艺直接决定了其最终性能和成本,由于缠绕<span style=\"color:red\">壳体</span>为中空结构,因此可以采用加热<span style=\"color:red\">壳体</span>内部金属芯模或内衬的方法实现缠绕后的或正在缠绕的复合<span style=\"color:red\">材料</span>的固化成型.即原位成型,本文介绍复合<span style=\"color:red\">材料</span><span style=\"color:red\">壳体</span>原位成型新工艺,建立筒型<span style=\"color:red\">壳体</span>内加热固化过程的数学模型,利用有限元法对筒体固化过程中的温度和固化度进行了数值模拟分析,该研究为实现<span style=\"color:red\">壳体</span>高效、优质且低成本成型提供新思路,为原位成型工艺设计、模拟和参数优化提供分析模型和方法.","authors":[{"authorName":"许家忠","id":"ceabd65d-3297-4741-ab82-6b79e38293de","originalAuthorName":"许家忠"},{"authorName":"乔明","id":"43bb6562-513e-4398-bda4-e62a8edd1d71","originalAuthorName":"乔明"},{"authorName":"尤波","id":"3f7573ee-24fe-41e9-9c9c-d278f703c46a","originalAuthorName":"尤波"},{"authorName":"王新颖","id":"430bad0c-8e47-4c54-91af-e06ac0332a27","originalAuthorName":"王新颖"}],"doi":"","fpage":"191","id":"3381667d-ff51-40dd-8b5c-0b26a9b23f14","issue":"2","journal":{"abbrevTitle":"CLKXYGY","coverImgSrc":"journal/img/cover/CLKXYGY.jpg","id":"14","issnPpub":"1005-0299","publisherId":"CLKXYGY","title":"材料科学与工艺"},"keywords":[{"id":"e90c6191-0bdb-48f7-bbd4-6a7d4b14a3e8","keyword":"热固型复合<span style=\"color:red\">材料</span>","originalKeyword":"热固型复合材料"},{"id":"5cd802bb-317f-43ba-a14c-e166811d09c5","keyword":"纤维缠绕<span style=\"color:red\">壳体</span>","originalKeyword":"纤维缠绕壳体"},{"id":"5308aa28-5d46-40be-99a2-090a8df6cabd","keyword":"内加热固化","originalKeyword":"内加热固化"},{"id":"c9e35281-e1a4-4011-aa1b-fe5f66ace436","keyword":"数值模拟","originalKeyword":"数值模拟"}],"language":"zh","publisherId":"clkxygy200902011","title":"纤维缠绕复合<span style=\"color:red\">材料</span><span style=\"color:red\">壳体</span>原位成型工艺研究","volume":"17","year":"2009"},{"abstractinfo":"本文叙述了碳复合<span style=\"color:red\">材料</span><span style=\"color:red\">壳体</span>放置15年后进行的结构试验,并对其各项性能进行对比和分析,从而得出<span style=\"color:red\">壳体</span>的老化性能.本研究将对今后碳复合<span style=\"color:red\">材料</span>产品的研制、生产和用具有较重要的参考价值.","authors":[{"authorName":"田晶","id":"a74c6dd6-91c7-41ab-be28-f39327c4e0c1","originalAuthorName":"田晶"},{"authorName":"田开谟","id":"d29c2f7b-633f-4030-9475-1e56c6fde05e","originalAuthorName":"田开谟"},{"authorName":"陈光烈","id":"c51d36ca-6558-418a-9e18-72a76964c992","originalAuthorName":"陈光烈"}],"doi":"10.3969/j.issn.1003-0999.2001.06.012","fpage":"33","id":"c374856c-1219-4219-a7a5-3500e41d7bba","issue":"6","journal":{"abbrevTitle":"BLGFHCL","coverImgSrc":"journal/img/cover/BLGFHCL.jpg","id":"6","issnPpub":"1003-0999","publisherId":"BLGFHCL","title":"玻璃钢/复合材料"},"keywords":[{"id":"a615f6cf-9fca-46f9-90a5-3cc5021ea050","keyword":"碳复合<span style=\"color:red\">材料</span>","originalKeyword":"碳复合材料"},{"id":"8f2b5543-6bd7-468b-b07f-5225634f71b5","keyword":"老化","originalKeyword":"老化"},{"id":"f438c627-ffd2-42b6-8b17-9ecb3ac9111c","keyword":"试验","originalKeyword":"试验"}],"language":"zh","publisherId":"blgfhcl200106012","title":"碳复合<span style=\"color:red\">材料</span><span style=\"color:red\">壳体</span>老化性能","volume":"","year":"2001"},{"abstractinfo":"针对T800HB/环氧复合<span style=\"color:red\">材料</span><span style=\"color:red\">壳体</span>易在封头部位产生复杂的应力状态,导致<span style=\"color:red\">壳体</span>低压破坏的问题,通过采用金属接头结构优化与封头补强措施,使T800HB/环氧复合<span style=\"color:red\">材料</span><span style=\"color:red\">壳体</span>的爆破压力由28.2 MPa提高到36.4 MPa,纤维强度发挥率由65.7％提升至85.6％.","authors":[{"authorName":"周伟江","id":"fee7fca3-2555-497d-9541-b67db83e6347","originalAuthorName":"周伟江"},{"authorName":"廖英强","id":"23ebb5ed-947e-4477-8a6d-8aca320bd8f4","originalAuthorName":"廖英强"},{"authorName":"张世杰","id":"a22c2ecf-424d-41f3-b6c3-b3f60c5703a2","originalAuthorName":"张世杰"},{"authorName":"尤丽虹","id":"a93dac7c-7389-438f-a3ee-6f67ccdc1815","originalAuthorName":"尤丽虹"}],"doi":"10.3969/j.issn.1007-2330.2014.03.026","fpage":"95","id":"68b691cf-f3cb-4ccf-bd20-de11222e3a33","issue":"3","journal":{"abbrevTitle":"YHCLGY","coverImgSrc":"journal/img/cover/YHCLGY.jpg","id":"77","issnPpub":"1007-2330","publisherId":"YHCLGY","title":"宇航材料工艺   "},"keywords":[{"id":"4ddc1820-680d-40d3-bdc0-5581f04ff7ad","keyword":"复合<span style=\"color:red\">材料</span><span style=\"color:red\">壳体</span>","originalKeyword":"复合材料壳体"},{"id":"a9f28b03-de77-4d10-bc74-de996f3d1267","keyword":"碳纤维","originalKeyword":"碳纤维"},{"id":"0c73dc04-5bed-4e4e-8b4b-051d673f8d63","keyword":"应变","originalKeyword":"应变"},{"id":"cbac3a10-fd37-4633-9e29-100d122c17f7","keyword":"纤维强度转化率","originalKeyword":"纤维强度转化率"}],"language":"zh","publisherId":"yhclgy201403026","title":"T800HB/环氧复合<span style=\"color:red\">材料</span><span style=\"color:red\">壳体</span>爆破性能分析","volume":"44","year":"2014"},{"abstractinfo":"针对复杂多筋<span style=\"color:red\">壳体</span>的结构特点,以及VARTM整体成型工艺特点,提出了一种新型的易碎模成型模具.在常规模具的基础上设计与制造了该易碎模,利用真空辅助灌注工艺成功制造了<span style=\"color:red\">壳体</span>的样机,满足了产品设计技术要求,为内部有交错筋的<span style=\"color:red\">壳体</span>结构复合<span style=\"color:red\">材料</span>产品的模具设计技术提供了一种新的思路.","authors":[{"authorName":"刘归","id":"f5baea9c-6991-41b2-802e-5778aaa0aa2a","originalAuthorName":"刘归"},{"authorName":"柴朋军","id":"c8989459-291e-45e3-b062-5554c25d7355","originalAuthorName":"柴朋军"},{"authorName":"刘海鑫","id":"f4f4852e-8718-474b-bae1-3530197e391e","originalAuthorName":"刘海鑫"},{"authorName":"赵志颖","id":"11aa3c81-f887-4f44-b2c3-743a185658eb","originalAuthorName":"赵志颖"},{"authorName":"彭飞","id":"ee2b89ba-991a-431c-878b-eaac267ef9dc","originalAuthorName":"彭飞"},{"authorName":"王齐崧","id":"26bac283-462f-4db6-9d04-43c1cbb4b4b2","originalAuthorName":"王齐崧"}],"doi":"","fpage":"72","id":"6e31302b-d074-4328-92d2-453067c6d3bb","issue":"10","journal":{"abbrevTitle":"BLGFHCL","coverImgSrc":"journal/img/cover/BLGFHCL.jpg","id":"6","issnPpub":"1003-0999","publisherId":"BLGFHCL","title":"玻璃钢/复合材料"},"keywords":[{"id":"cae43737-adfb-4afe-b945-1557cb662f0e","keyword":"复合<span style=\"color:red\">材料</span>","originalKeyword":"复合材料"},{"id":"5957857b-96f5-453a-a74d-917b350fa980","keyword":"复杂多筋结构","originalKeyword":"复杂多筋结构"},{"id":"01a21e38-3506-43cc-abce-7c4f8a4b1466","keyword":"模具设计","originalKeyword":"模具设计"},{"id":"7c8e05f0-0a30-4e07-966c-0fb5adf1c89a","keyword":"易碎模","originalKeyword":"易碎模"}],"language":"zh","publisherId":"blgfhcl201510014","title":"复杂多筋复合<span style=\"color:red\">材料</span><span style=\"color:red\">壳体</span>的模具设计技术研究","volume":"","year":"2015"},{"abstractinfo":"采用不锈钢纤维作为聚酰胺的导电填料,通过注塑工艺制备复合<span style=\"color:red\">材料</span>地雷<span style=\"color:red\">壳体</span>.在<span style=\"color:red\">壳体</span>内部放置电子引信并连接电点火头,于微波暗室中进行峰值功率为1GW的超宽带电磁脉冲辐射下的毁伤效应实验.超宽带脉冲能量主要分布在10MHz～2GHz范围内,当<span style=\"color:red\">壳体</span>放置天线前的距离＞0.5m时,内部的电子引信能正常工作；数值计算表明完整<span style=\"color:red\">壳体</span>的屏蔽效能＞25dB,与实验结果相一致.当<span style=\"color:red\">壳体</span>存在单个直径＜4.5mm圆孔时,实验结果与数值计算均表明其对屏蔽效能影响微小.复合<span style=\"color:red\">材料</span><span style=\"color:red\">壳体</span>有助于提高电子引信地雷在战场高功率电磁环境下的生存能力.","authors":[{"authorName":"罗先南","id":"a2e2a7b9-8418-48a1-8a8d-38b99ffe699c","originalAuthorName":"罗先南"},{"authorName":"方向","id":"eaae8431-1f33-46cb-88ed-c2ccaff2f736","originalAuthorName":"方向"},{"authorName":"高振儒","id":"45517ec7-95b1-447a-861a-5941c9073993","originalAuthorName":"高振儒"},{"authorName":"刘君","id":"b74d314f-f488-47c1-96e0-8f2af300a4c8","originalAuthorName":"刘君"},{"authorName":"方鲲","id":"edae675c-a2f1-4906-b273-93dceb593b0b","originalAuthorName":"方鲲"}],"doi":"10.3969/j.issn.1001-9731.2013.15.032","fpage":"2276","id":"c7ef5bc1-4368-488e-810d-1edd27112aa2","issue":"15","journal":{"abbrevTitle":"GNCL","coverImgSrc":"journal/img/cover/GNCL.jpg","id":"33","issnPpub":"1001-9731","publisherId":"GNCL","title":"功能材料"},"keywords":[{"id":"da3ecc6d-f13f-4748-b3f9-31eda52824b5","keyword":"复合<span style=\"color:red\">材料</span>","originalKeyword":"复合材料"},{"id":"3e783ea9-fb5b-4154-b50d-65f894311244","keyword":"地雷<span style=\"color:red\">壳体</span>","originalKeyword":"地雷壳体"},{"id":"848167e7-e008-4141-a322-60ee44e95055","keyword":"超宽带","originalKeyword":"超宽带"},{"id":"21c82c66-6da3-49fb-be30-e35c3b357e92","keyword":"电磁脉冲","originalKeyword":"电磁脉冲"},{"id":"8a3de387-04ab-4876-96fb-f8fe46bb4453","keyword":"屏蔽效能","originalKeyword":"屏蔽效能"}],"language":"zh","publisherId":"gncl201315032","title":"复合<span style=\"color:red\">材料</span>地雷<span style=\"color:red\">壳体</span>超宽带脉冲屏蔽效能计算与实验","volume":"44","year":"2013"},{"abstractinfo":"本文推导出了复合<span style=\"color:red\">材料</span>层合<span style=\"color:red\">壳体</span>的三维本构方程,修正了Reddy和Liu论文中的错误.","authors":[{"authorName":"杨宜谦","id":"f56e070a-27d0-4283-87e8-eae4bf6813aa","originalAuthorName":"杨宜谦"}],"doi":"10.3969/j.issn.1003-0999.1999.04.002","fpage":"5","id":"2438a141-df1a-489d-9663-ae3b4c14747e","issue":"4","journal":{"abbrevTitle":"BLGFHCL","coverImgSrc":"journal/img/cover/BLGFHCL.jpg","id":"6","issnPpub":"1003-0999","publisherId":"BLGFHCL","title":"玻璃钢/复合材料"},"keywords":[{"id":"68bce6dd-46d2-49ca-a2c8-2b472cdd93f8","keyword":"复合<span style=\"color:red\">材料</span>","originalKeyword":"复合材料"},{"id":"5e0aa63a-d438-4fd3-8408-7091a574645b","keyword":"<span style=\"color:red\">壳体</span>","originalKeyword":"壳体"},{"id":"b5f298f0-de30-4109-8458-da20ed22d6f8","keyword":"三维本构方程","originalKeyword":"三维本构方程"}],"language":"zh","publisherId":"blgfhcl199904002","title":"复合<span style=\"color:red\">材料</span>层合<span style=\"color:red\">壳体</span>的三维本构方程","volume":"","year":"1999"},{"abstractinfo":"采用ALGOR非线性<span style=\"color:red\">材料</span>机械运动仿真模块模拟复合<span style=\"color:red\">材料</span>水雷<span style=\"color:red\">壳体</span>自由跌落与地面接触、碰撞、受力的全过程;分四种状态进行自由跌落过程模拟分析,研究了碰撞地面和跌落姿态对水雷<span style=\"color:red\">壳体</span>自由跃落碰撞过程的影响;通过碰撞过程载荷、应力、应变、位移等响应数据的分析对比,得出复合<span style=\"color:red\">材料</span>水雷<span style=\"color:red\">壳体</span>抗自由跌落冲击性能的研究结论,为复合<span style=\"color:red\">材料</span>水雷<span style=\"color:red\">壳体</span>抗冲击性能评价提供理论支撑.","authors":[{"authorName":"宗方勇","id":"387eea2d-b0c5-48a1-a76f-bdd44286540b","originalAuthorName":"宗方勇"},{"authorName":"柴朋军","id":"82766488-b30f-4f67-9e65-2f0335f0e699","originalAuthorName":"柴朋军"}],"doi":"","fpage":"90","id":"a24b2abd-60d6-478e-8e64-00e8e194fb26","issue":"12","journal":{"abbrevTitle":"BLGFHCL","coverImgSrc":"journal/img/cover/BLGFHCL.jpg","id":"6","issnPpub":"1003-0999","publisherId":"BLGFHCL","title":"玻璃钢/复合材料"},"keywords":[{"id":"540d748b-4903-4c81-92ca-cacfd25e7130","keyword":"复合<span style=\"color:red\">材料</span>","originalKeyword":"复合材料"},{"id":"97c9dc63-6853-49ee-808c-cf5c39407feb","keyword":"水雷<span style=\"color:red\">壳体</span>","originalKeyword":"水雷壳体"},{"id":"51960634-4e2d-4780-a459-9fc8cb16b245","keyword":"自由跌落","originalKeyword":"自由跌落"},{"id":"5f4dae84-8a9e-4449-adc1-063450053cd1","keyword":"碰撞","originalKeyword":"碰撞"},{"id":"8fcaa031-8384-42a1-b7e2-dff0b2c0916b","keyword":"冲击","originalKeyword":"冲击"}],"language":"zh","publisherId":"blgfhcl201612017","title":"复合<span style=\"color:red\">材料</span>水雷<span style=\"color:red\">壳体</span>抗自由跌落冲击性能数值模拟分析","volume":"","year":"2016"},{"abstractinfo":"通过浇注体、复丝和容器性能测试，较系统地研究了高性能低粘度的树脂基体配方，探讨了锥形<span style=\"color:red\">壳体</span>的成型工艺条件，初步研究了容器纤维含量的精确控制方法，摸索了湿法成型<span style=\"color:red\">壳体</span>表面的处理技术。用国产碳纤维缠绕的锥形容器PV/W值达30.6 km，环向纤维强度转化率达78.2%，实验结果表明，该工艺路线是可行的。","authors":[{"authorName":"刘炳禹","id":"018781d9-305b-4556-ad9b-eba222f2c4c2","originalAuthorName":"刘炳禹"},{"authorName":"王晓洁","id":"2dd0f3bc-ddd3-4d9a-8087-32c59a431a5f","originalAuthorName":"王晓洁"},{"authorName":"韩建平","id":"b186185b-debf-43ea-b994-31e8c50beb70","originalAuthorName":"韩建平"},{"authorName":"尤丽虹","id":"eb0cfe01-54f8-46f3-8392-afbc5266e22b","originalAuthorName":"尤丽虹"}],"doi":"10.3969/j.issn.1007-2330.2000.04.005","fpage":"26","id":"695eea13-9977-4c22-a132-3e0a5c08e0c5","issue":"4","journal":{"abbrevTitle":"YHCLGY","coverImgSrc":"journal/img/cover/YHCLGY.jpg","id":"77","issnPpub":"1007-2330","publisherId":"YHCLGY","title":"宇航材料工艺   "},"keywords":[{"id":"76f1dbb6-596d-4070-a342-c481fcb920db","keyword":"碳纤维","originalKeyword":"碳纤维"},{"id":"0782f47e-db1a-4455-b9d8-996d8a61a286","keyword":"锥形<span style=\"color:red\">壳体</span>","originalKeyword":"锥形壳体"},{"id":"d5acfd34-c123-476e-b6d0-879eb51043b8","keyword":"成型技术","originalKeyword":"成型技术"}],"language":"zh","publisherId":"yhclgy200004005","title":"碳纤维复合<span style=\"color:red\">材料</span>锥形<span style=\"color:red\">壳体</span>成型技术初探","volume":"30","year":"2000"},{"abstractinfo":"为了提高固体火箭发动机(SRM)的外载荷承载能力,研究了其复合<span style=\"color:red\">材料</span><span style=\"color:red\">壳体</span>的失效机制,提出了复合<span style=\"color:red\">材料</span><span style=\"color:red\">壳体</span>的增强改进结构形式.通过提高复合<span style=\"color:red\">材料</span>外缠绕层的轴向刚度和横向弯曲刚度,使得连接区域内的内、外缠绕层的轴向变形相协调,改善了内、外缠绕层的轴向承载分配,使增强改进后的复合<span style=\"color:red\">材料</span><span style=\"color:red\">壳体</span>结构的承载能力提高了124％,而结构质量增加低于10％.研究结果表明:SRM复合<span style=\"color:red\">材料</span><span style=\"color:red\">壳体</span>承载能力的关键因素是连接区域内复合<span style=\"color:red\">材料</span>内、外缠绕层的刚度匹配设计,只有保证连接区域内的刚度匹配和位移变形相协调,才能充分发挥复合<span style=\"color:red\">材料</span><span style=\"color:red\">壳体</span>的承载能力.","authors":[{"authorName":"侯晓","id":"b903f6dc-45df-4053-a1f2-693a555fb22e","originalAuthorName":"侯晓"},{"authorName":"秦谊","id":"60bf6fa3-e6d1-418d-a3af-fa07f4822c2a","originalAuthorName":"秦谊"},{"authorName":"丁文辉","id":"10bc50a3-d10b-4932-b37c-9283df34b65f","originalAuthorName":"丁文辉"}],"doi":"","fpage":"1343","id":"9ef0f9f6-d90e-47e4-8621-25d5616aa9c6","issue":"5","journal":{"abbrevTitle":"FHCLXB","coverImgSrc":"journal/img/cover/FHCLXB.jpg","id":"26","issnPpub":"1000-3851","publisherId":"FHCLXB","title":"复合材料学报"},"keywords":[{"id":"0566b665-2b26-4c0a-9a1d-c269daf2517a","keyword":"固体火箭发动机","originalKeyword":"固体火箭发动机"},{"id":"a40360f8-dd9f-4aac-b7b1-cd1f0adf7160","keyword":"复合<span style=\"color:red\">材料</span><span style=\"color:red\">壳体</span>","originalKeyword":"复合材料壳体"},{"id":"6d1da687-e326-40af-aee1-aae294584bed","keyword":"失效","originalKeyword":"失效"},{"id":"36811723-33cd-45a6-8ca2-11e0aedb569b","keyword":"刚度匹配","originalKeyword":"刚度匹配"},{"id":"4f60be59-4d2c-4615-b663-eef0deec9ac8","keyword":"增强改进结构","originalKeyword":"增强改进结构"}],"language":"zh","publisherId":"fhclxb201405032","title":"固体火箭发动机复合<span style=\"color:red\">材料</span><span style=\"color:red\">壳体</span>承载力分析","volume":"31","year":"2014"}],"totalpage":5535,"totalrecord":55346}