{"currentpage":1,"firstResult":0,"maxresult":10,"pagecode":5,"pageindex":{"endPagecode":5,"startPagecode":1},"records":[{"abstractinfo":"通过对现役飞机腐蚀损伤状况的统计分析,研究了现役飞机结构主体材料在环境腐蚀介质中的疲劳损伤特征和基本破坏失效模式,阐述了今后现役军用飞机在腐蚀环境下疲劳使用寿命和日历寿命研究的相关内容,并对现役军用飞机腐蚀疲劳研究的发展提出一些看法.","authors":[{"authorName":"穆志韬","id":"c5f6c700-09d9-4b35-a5e0-eeb751b90f25","originalAuthorName":"穆志韬"},{"authorName":"熊玉平","id":"1a708752-2d13-4a95-8b32-067309a9d5e5","originalAuthorName":"熊玉平"}],"doi":"10.3969/j.issn.1001-1560.2001.12.026","fpage":"49","id":"a5d4b5d1-fa4b-4841-aca7-363d85f44461","issue":"12","journal":{"abbrevTitle":"CLBH","coverImgSrc":"journal/img/cover/CLBH.jpg","id":"7","issnPpub":"1001-1560","publisherId":"CLBH","title":"材料保护"},"keywords":[{"id":"05ffec64-53c8-4b8f-bab8-4fed3e7457f7","keyword":"飞机结构","originalKeyword":"飞机结构"},{"id":"f550bd20-d923-4aa1-80b0-65cbe3f4dbb9","keyword":"腐蚀疲劳","originalKeyword":"腐蚀疲劳"},{"id":"5225e69e-e5ac-4cbb-bbc8-bc569deb41ea","keyword":"腐蚀环境谱","originalKeyword":"腐蚀环境谱"},{"id":"dceabc47-7c66-4f25-88a6-5f846daab6b4","keyword":"腐蚀控制","originalKeyword":"腐蚀控制"}],"language":"zh","publisherId":"clbh200112026","title":"飞机结构主体材料腐蚀损伤特点分析","volume":"34","year":"2001"},{"abstractinfo":"分析了导致海军飞机结构腐蚀的主要因素，基于飞机地面停放环境谱，对航空LY12CZ铝合金件进行了多个当量年限的加速腐蚀试验和热带海洋环境下的暴露试验；对试件表面涂层、金属基体材料腐蚀情况进行观察和测量；根据腐蚀评价指标对试验件腐蚀状况进行了分析比较。结果表明，实验室加速腐蚀结果符合飞机外场服役的腐蚀特征，而材料直接暴露在海洋环境中比外场腐蚀速度更快。对腐蚀深度和腐蚀失重进行测量，给出腐蚀深度的分布特性和加速腐蚀与自然暴露的当量关系，对失重规律进行了研究。","authors":[{"authorName":"胡建军","id":"9528c589-51c1-44f7-9139-b26cbb099e6f","originalAuthorName":"胡建军"},{"authorName":"陈跃良","id":"faa7469a-dde0-4972-8fb3-896980a49478","originalAuthorName":"陈跃良"},{"authorName":"卞贵学","id":"c3d4b5bd-1b11-46b4-9ab3-716626506b79","originalAuthorName":"卞贵学"},{"authorName":"张勇","id":"1c68f5d8-618d-416f-bc0d-27f64348cec4","originalAuthorName":"张勇"},{"authorName":"衣林","id":"94dad186-854f-4782-869c-ba1dc4179035","originalAuthorName":"衣林"}],"doi":"","fpage":"900","id":"47d45a9f-4c64-4843-8bc9-9a09f48987e3","issue":"11","journal":{"abbrevTitle":"FSYFH","coverImgSrc":"journal/img/cover/FSYFH.jpg","id":"25","issnPpub":"1005-748X","publisherId":"FSYFH","title":"腐蚀与防护"},"keywords":[{"id":"03736d1d-ad92-4782-8665-5fcde02a7dec","keyword":"LY12CZ铝合金．力口速腐蚀试验","originalKeyword":"LY12CZ铝合金．力口速腐蚀试验"},{"id":"a9cc0278-84df-4a95-bf5d-09fe2dd8fb65","keyword":"腐蚀当量关系","originalKeyword":"腐蚀当量关系"},{"id":"f56760f6-9bb5-4a58-b71a-17b7d00462d7","keyword":"飞机结构","originalKeyword":"飞机结构"}],"language":"zh","publisherId":"fsyfh201111014","title":"飞机结构加速腐蚀与自然腐蚀","volume":"32","year":"2011"},{"abstractinfo":"结构健康监测(SHM)技术被广泛引入到了飞机设计与维护,本文依据现阶段SHM技术的发展现状,将SHM技术与MSG-3分析思想融合,制定了一种针对采用SHM技术飞机结构的计划维修分析流程.","authors":[{"authorName":"蔡禹舜","id":"a3f993bd-16a1-4f0a-86c2-186b68ecdefc","originalAuthorName":"蔡禹舜"},{"authorName":"朱昊","id":"1634efc5-b214-4b9c-9d7a-c140c85def13","originalAuthorName":"朱昊"},{"authorName":"卿新林","id":"2cbafd37-418b-4ba7-83da-730d9c8bcd4d","originalAuthorName":"卿新林"}],"doi":"10.3969/j.issn.1007-2330.2015.06.015","fpage":"71","id":"119ac337-34e0-4391-9724-afbbc9f816d8","issue":"6","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":"a7a224b5-bfa7-4b19-9792-0e4b656b978f","keyword":"飞机结构","originalKeyword":"飞机结构"},{"id":"2f470f31-f70e-4e5f-ae6e-6c7d81660296","keyword":"复合材料","originalKeyword":"复合材料"},{"id":"6ef7fed5-1cb4-4dc1-a947-3689bf011eda","keyword":"结构健康监测","originalKeyword":"结构健康监测"},{"id":"6ec38dfc-8c77-4a57-ab91-827f304a22c1","keyword":"计划维修分析","originalKeyword":"计划维修分析"},{"id":"6f213c14-0ba5-41d3-96e3-757564671ce8","keyword":"MSG-3","originalKeyword":"MSG-3"}],"language":"zh","publisherId":"yhclgy201506015","title":"基于结构健康监测的飞机结构MSG-3分析","volume":"45","year":"2015"},{"abstractinfo":"腐蚀损伤是最常见的飞机结构损伤形式之一,会降低结构的剩余强度和耐久性.针对在役民用典型机型飞机易腐蚀结构,首先将腐蚀状态划分为5个等级;其次拟合遭受腐蚀的飞机结构剩余厚度递减函数,给出腐蚀状态转移概率矩阵,建立马尔可夫状态预测模型.最后收集某型飞机后货舱隔框腐蚀数据作为算例,预测了隔框结构在潜伏期之后的腐蚀状态.结果发现使用26个月之后,沿海地区飞机隔框结构腐蚀已达到三级状态.预测结果与工程实践相符,说明马尔可夫模型适用于飞机结构腐蚀状态预测.","authors":[{"authorName":"王志平","id":"66d17602-abc7-4039-aa1c-eae93b1ec150","originalAuthorName":"王志平"},{"authorName":"马旻昱","id":"a4b36f47-23e0-4acf-a7ce-a57e04190216","originalAuthorName":"马旻昱"},{"authorName":"张春晓","id":"ffeb6bd3-719c-476c-aa9a-67c1f8fdd3f9","originalAuthorName":"张春晓"},{"authorName":"苏景新","id":"9c224315-b5a8-46c8-8ffd-9a51760e6d18","originalAuthorName":"苏景新"}],"doi":"10.11973/fsyfh-201510009","fpage":"942","id":"37203aeb-27fa-41d8-8e47-4c48389bf735","issue":"10","journal":{"abbrevTitle":"FSYFH","coverImgSrc":"journal/img/cover/FSYFH.jpg","id":"25","issnPpub":"1005-748X","publisherId":"FSYFH","title":"腐蚀与防护"},"keywords":[{"id":"bedcb042-0ea5-4d49-bde1-cd75d835c1fc","keyword":"飞机结构","originalKeyword":"飞机结构"},{"id":"79c3ae84-5305-4c0b-90b9-c344929a628c","keyword":"腐蚀","originalKeyword":"腐蚀"},{"id":"24d9c3f1-12b4-4f1a-bd83-7c390569538b","keyword":"马尔可夫模型","originalKeyword":"马尔可夫模型"},{"id":"682d4934-b319-4fa1-a953-e6c888d2fac8","keyword":"状态预测","originalKeyword":"状态预测"}],"language":"zh","publisherId":"fsyfh201510009","title":"基于马尔可夫链的飞机结构腐蚀状态预测","volume":"36","year":"2015"},{"abstractinfo":"飞机设计人员在飞机总体方案论证阶段对主要结构件进行选材时,需要对复合材料飞机结构的技术成熟度进行评估,以确定是否选用复合材料.借鉴技术完备等级(TRL)标准,提出了一个复合材料飞机结构技术成熟度定量评价方法(TEMCAS).TEMCAS方法将复合材料飞机结构的技术成熟度分为8个等级,涵盖了复合材料结构技术从设计需求到结构应用的整个过程,通过对波音公司复合材料机身结构技术的技术成熟度评价实例证明了其有效性.在飞机总体方案论证阶段可以利用TEMCAS方法,对复合材料飞机结构技术的成熟度进行定量分析,为初步选材复合材料结构应用的决策和风险评估提供依据.","authors":[{"authorName":"蓝元沛","id":"e1401ece-dfab-434c-9169-a16080a58a7c","originalAuthorName":"蓝元沛"},{"authorName":"关志东","id":"76366ebb-4d76-4911-a55a-1a6f11e4c892","originalAuthorName":"关志东"},{"authorName":"孟庆春","id":"63f7f79a-1c12-43a3-a11e-a6000f83afb6","originalAuthorName":"孟庆春"}],"doi":"","fpage":"150","id":"02531578-e48f-429a-acb1-5c7010174846","issue":"3","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":"accbbe98-fa23-4c13-971c-0d04ea880565","keyword":"先进复合材料","originalKeyword":"先进复合材料"},{"id":"3186d0e3-d8c0-4bb5-8c08-f5a38fc68598","keyword":"飞机结构","originalKeyword":"飞机结构"},{"id":"769e1558-a08b-4b32-beb5-5cb97393bd17","keyword":"技术成熟度","originalKeyword":"技术成熟度"},{"id":"0c550406-1876-495d-b2d2-b5ecf3ca6ff9","keyword":"技术完备等级","originalKeyword":"技术完备等级"},{"id":"4cb51c8c-5118-492c-a922-44458d99e5f3","keyword":"评价方法","originalKeyword":"评价方法"}],"language":"zh","publisherId":"fhclxb201003025","title":"复合材料飞机结构技术成熟度评价方法","volume":"27","year":"2010"},{"abstractinfo":"综合作者多年的飞机结构修理工作,分析、归纳了沿海机场飞机典型腐蚀损伤,得出飞机结构腐蚀主要是环形间隙中未加保护的铝合金表面和间隙中的积水而形成的电化学腐蚀.提出缝隙密封等减少结构腐蚀的制造和使用维护过程中的防腐工艺措施.","authors":[{"authorName":"胡芳友","id":"3169046b-e002-461b-9f72-b087dde289db","originalAuthorName":"胡芳友"},{"authorName":"王茂才","id":"344cecb9-4e2b-4279-92e4-3466583be3fc","originalAuthorName":"王茂才"},{"authorName":"温景林","id":"084faa3d-e766-476a-a003-bbfd4482dc77","originalAuthorName":"温景林"}],"doi":"10.3969/j.issn.1002-6495.2003.02.010","fpage":"97","id":"737844a3-7e3b-483c-8a4b-9ce5504cafbd","issue":"2","journal":{"abbrevTitle":"FSXB","coverImgSrc":"journal/img/cover/腐蚀学报封面.jpg","id":"24","issnPpub":"2667-2669","publisherId":"FSXB","title":"腐蚀学报（英文）"},"keywords":[{"id":"d6c45ccc-f727-42da-b679-cd2284c20638","keyword":"铝合金","originalKeyword":"铝合金"},{"id":"37403d6b-8fbf-4ebe-a9ee-da899b45541e","keyword":"飞机结构","originalKeyword":"飞机结构"},{"id":"1d661fd9-65a4-4ff1-ac06-fa041903d456","keyword":"腐蚀","originalKeyword":"腐蚀"},{"id":"e06951e5-c59f-4ccf-9caa-abd58458c919","keyword":"对策","originalKeyword":"对策"}],"language":"zh","publisherId":"fskxyfhjs200302010","title":"沿海飞机铝合金结构件腐蚀与防护","volume":"15","year":"2003"},{"abstractinfo":"本文从飞机结构完整性要求出发提出了对聚合物基复合材料性能的具体要求,特别是在湿热和抗冲击性能方面的要求.为了降低全尺寸结构静强度验证中对湿热环境影响考虑的技术难度,建议提高对湿态玻璃化转变温度的要求;为了满足含冲击损伤(通常用一定深度的凹坑来描述)结构的剩余强度要求,适用于飞机主结构的复合材料体系应当是用静压痕试验得到易于产生表面凹坑同时损伤面积较小的材料体系.","authors":[{"authorName":"沈真","id":"439c2016-61dc-45ab-b4a6-ff71b4d11d6c","originalAuthorName":"沈真"},{"authorName":"杨胜春","id":"02dce3c7-ff5c-48b4-a250-cb26fdd71e32","originalAuthorName":"杨胜春"}],"doi":"10.3969/j.issn.1001-4381.2007.z1.056","fpage":"248","id":"4dc20153-5ba8-424d-8e82-5e8559ec4a9d","issue":"z1","journal":{"abbrevTitle":"CLGC","coverImgSrc":"journal/img/cover/CLGC.jpg","id":"9","issnPpub":"1001-4381","publisherId":"CLGC","title":"材料工程"},"keywords":[{"id":"753d7e07-1499-486c-a368-a7ac1e57c412","keyword":"飞机结构","originalKeyword":"飞机结构"},{"id":"729e863c-aa42-4333-8830-75c8bd0492da","keyword":"结构完整性","originalKeyword":"结构完整性"},{"id":"9f956625-1d23-4bb9-9633-22bf0600d75f","keyword":"复合材料","originalKeyword":"复合材料"},{"id":"bfef8376-5b5d-4a0c-8bc8-e6d209deec78","keyword":"湿热性能","originalKeyword":"湿热性能"},{"id":"86cd1b66-58f5-4272-8d2d-c97da73e51f1","keyword":"损伤容限","originalKeyword":"损伤容限"},{"id":"8d4d767f-dc9a-40a0-806c-a4ea59efc3ff","keyword":"损伤阻抗","originalKeyword":"损伤阻抗"}],"language":"zh","publisherId":"clgc2007z1056","title":"飞机结构用复合材料的力学性能要求","volume":"","year":"2007"},{"abstractinfo":"提出估算日历寿命的一种新方法-线性累积破坏率准则法,其物理意义明确,简单明了.飞机机体的损伤模式描述为疲劳损伤和预腐蚀疲劳损伤,并将飞机结构的日历寿命定义为地面停放日历寿命和飞行日历寿命之和.选取破坏率为损伤参量,在环境腐蚀当量关系加速预腐蚀疲劳试验的基础上,通过疲劳寿命分布形式和概率密度函数求出破坏率来估算预腐蚀环境下的日历寿命.利用一组预腐蚀与疲劳试验数据对该方法进行了验证.","authors":[{"authorName":"赵海军","id":"4aa347f5-a844-4162-8505-553d51aea50b","originalAuthorName":"赵海军"},{"authorName":"郭泉","id":"cff62e25-8f2d-4c24-81cb-8b3268abf086","originalAuthorName":"郭泉"},{"authorName":"金平","id":"49b0861a-1efe-4dea-b3b2-7393f049f328","originalAuthorName":"金平"}],"doi":"10.3969/j.issn.1002-6495.2007.03.021","fpage":"229","id":"292a3101-49c5-48ea-9816-567a4b450f8c","issue":"3","journal":{"abbrevTitle":"FSXB","coverImgSrc":"journal/img/cover/腐蚀学报封面.jpg","id":"24","issnPpub":"2667-2669","publisherId":"FSXB","title":"腐蚀学报（英文）"},"keywords":[{"id":"73082428-d23a-45c2-9d0b-588529ef48b3","keyword":"飞机结构","originalKeyword":"飞机结构"},{"id":"2c6805ea-dfc6-4df9-9c66-4e92f3ffe49b","keyword":"日历寿命","originalKeyword":"日历寿命"},{"id":"b6443c21-07d7-4292-b4eb-91592076c862","keyword":"累积破坏率准则","originalKeyword":"累积破坏率准则"},{"id":"3f2334dc-2ad8-4d25-8c29-d3f1c789da5a","keyword":"预腐蚀","originalKeyword":"预腐蚀"},{"id":"b5bf45af-c13c-4f9d-904a-26bce2661284","keyword":"疲劳","originalKeyword":"疲劳"}],"language":"zh","publisherId":"fskxyfhjs200703021","title":"加速预腐蚀与疲劳试验估算飞机结构日历寿命的新方法","volume":"19","year":"2007"},{"abstractinfo":"分析国内外复合材料飞机结构材料许用值、设计许用值的确定原则和方法,研究给出了复合材料结构材料许用值的表征和应用、试验以反试验数据的统计分析方法,以及静强度、疲劳强度、损伤容限和修理设计许用值的确定方法.","authors":[{"authorName":"冯振宇","id":"bd3a1ead-4a3e-4f28-bd43-8b23eecd4c0f","originalAuthorName":"冯振宇"},{"authorName":"邹田春","id":"1287f44e-acba-4d3e-aa64-0ca3b6f9a647","originalAuthorName":"邹田春"},{"authorName":"郝鹏","id":"2089ccb7-1fcd-4bb3-8497-7f1d21137efc","originalAuthorName":"郝鹏"},{"authorName":"杜洪增","id":"dc45df42-9f87-427e-b2ba-bbdd1933b2ca","originalAuthorName":"杜洪增"},{"authorName":"田秀云","id":"60750894-d72f-45d8-9abe-51d38e5aea4f","originalAuthorName":"田秀云"}],"doi":"10.3969/j.issn.1007-2330.2011.05.004","fpage":"15","id":"129b24d3-1afc-443b-93f5-a850f0d2e6d3","issue":"5","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":"d0030691-d336-436f-9ca9-df85ae53642b","keyword":"飞机结构","originalKeyword":"飞机结构"},{"id":"653dc435-cda2-43e1-b1ff-16cdd4290481","keyword":"复合材料","originalKeyword":"复合材料"},{"id":"16f9abda-03da-4cc2-96e9-07844c40c549","keyword":"材料许用值","originalKeyword":"材料许用值"},{"id":"68baf9d6-f1c4-44ed-bbb4-5736f6f67fc7","keyword":"设计许用值","originalKeyword":"设计许用值"}],"language":"zh","publisherId":"yhclgy201105004","title":"复合材料飞机结构材料和设计许用值的确定方法","volume":"41","year":"2011"},{"abstractinfo":"利用热波成像技术,对加速腐蚀试样和实际飞机结构腐蚀件进行了隐蔽腐蚀检测的实验研究.结果表明:这一技术可以很好地检测出隐蔽腐蚀,不受腐蚀产物残留与否以及表面漆层的影响,对于剥层腐蚀特别有效；该方法获得的腐蚀坑的图像细节丰富、直观易懂；同时,该技术能够检测胶结缝内部的缺胶和脱胶.","authors":[{"authorName":"赵志昌","id":"df9f5fa6-863e-45a8-b117-63dabb4617d5","originalAuthorName":"赵志昌"},{"authorName":"姚红宇","id":"046b5188-2326-433b-98fc-83f1ae0828f5","originalAuthorName":"姚红宇"},{"authorName":"曹大树","id":"f67d3857-4b0a-44cd-a27e-f8ab6b44afc9","originalAuthorName":"曹大树"},{"authorName":"孙延春","id":"9cc42eff-62b3-4792-9747-b933da6ac552","originalAuthorName":"孙延春"}],"doi":"10.3969/j.issn.1001-4381.2012.04.015","fpage":"72","id":"0a9f6402-6ef9-4b99-8b73-f61a20c2d24e","issue":"4","journal":{"abbrevTitle":"CLGC","coverImgSrc":"journal/img/cover/CLGC.jpg","id":"9","issnPpub":"1001-4381","publisherId":"CLGC","title":"材料工程"},"keywords":[{"id":"ccf2259e-05e5-49fb-bac2-333240b64c9e","keyword":"无损检测","originalKeyword":"无损检测"},{"id":"bbdaabed-bcf3-4707-ac99-4175fb439854","keyword":"热波成像","originalKeyword":"热波成像"},{"id":"19dbc0d3-9b26-486c-8657-94bee4b8f46e","keyword":"腐蚀","originalKeyword":"腐蚀"},{"id":"a85b4ef5-2892-49fc-9e13-b432b9a38270","keyword":"飞机结构","originalKeyword":"飞机结构"}],"language":"zh","publisherId":"clgc201204015","title":"应用热波成像技术检测飞机结构隐蔽腐蚀的实验研究","volume":"","year":"2012"}],"totalpage":5948,"totalrecord":59473}