航空材料学报
航空材料學報
항공재료학보
JOURNAL OF AERONAUTICAL MATERIALS
2009年
6期
77-80
,共4页
吴小梅%贺世美%李建平%何利民
吳小梅%賀世美%李建平%何利民
오소매%하세미%리건평%하이민
IC10合金%EB-PVD热障涂层%力学性能
IC10閤金%EB-PVD熱障塗層%力學性能
IC10합금%EB-PVD열장도층%역학성능
IC10 alloy%EB-PVD TBCs%mechanical properties
采用电弧离子镀技术在IC10合金基体上制备NiCrAlYSi粘结层,利用电子束物理气相沉积(EB-PVD)技术在粘结层上制备YSZ陶瓷面层.研究了YSZ热障涂层对IC10合金拉伸、持久、疲劳性能的影响.结果表明:IC10合金沉积YSZ热障涂层后,980℃/200 MPa高温持久寿命与IC10合金相当;900℃高温抗拉强度σ_b、屈服强度σ_0.2、伸长率δ和断面收缩率ψ与基体相比,基本保持不变;室温抗拉强度σ_b、屈服强度σ_0.2与基体相比稍有下降;800℃/447MPa疲劳寿命与基体合金相当.因此,IC10合金沉积TBCs涂层后,对IC10合金力学性能无明显影响,不影响合金的实际使用.
採用電弧離子鍍技術在IC10閤金基體上製備NiCrAlYSi粘結層,利用電子束物理氣相沉積(EB-PVD)技術在粘結層上製備YSZ陶瓷麵層.研究瞭YSZ熱障塗層對IC10閤金拉伸、持久、疲勞性能的影響.結果錶明:IC10閤金沉積YSZ熱障塗層後,980℃/200 MPa高溫持久壽命與IC10閤金相噹;900℃高溫抗拉彊度σ_b、屈服彊度σ_0.2、伸長率δ和斷麵收縮率ψ與基體相比,基本保持不變;室溫抗拉彊度σ_b、屈服彊度σ_0.2與基體相比稍有下降;800℃/447MPa疲勞壽命與基體閤金相噹.因此,IC10閤金沉積TBCs塗層後,對IC10閤金力學性能無明顯影響,不影響閤金的實際使用.
채용전호리자도기술재IC10합금기체상제비NiCrAlYSi점결층,이용전자속물리기상침적(EB-PVD)기술재점결층상제비YSZ도자면층.연구료YSZ열장도층대IC10합금랍신、지구、피로성능적영향.결과표명:IC10합금침적YSZ열장도층후,980℃/200 MPa고온지구수명여IC10합금상당;900℃고온항랍강도σ_b、굴복강도σ_0.2、신장솔δ화단면수축솔ψ여기체상비,기본보지불변;실온항랍강도σ_b、굴복강도σ_0.2여기체상비초유하강;800℃/447MPa피로수명여기체합금상당.인차,IC10합금침적TBCs도층후,대IC10합금역학성능무명현영향,불영향합금적실제사용.
The Y2O3 stabilized ZrO2 thermal barrier coatings with arc ion plated NiCrAlYSi bond coating were deposited by EB-PVD technique on the IC10 alloy substrate. The effect of YSZ thermal barrier coating on the tensile strength,yield strength at 900℃ and the rotating bending fatigue life were studied. Compared IC10 alloy with thermal barrier coating to IC10 alloy,the results of the stress rupture life under 980℃/200 MPa conditions, the tensile intension and yield intension at 900℃ and the rotating bending fatigue life under 800℃/447 MPa were identical. But it's room temperature tensile strength and yield strength decreases in some sort. So the EB-PVD TBCs process does not affect the mechanical properties of IC10 substrate.