发明名称 |
TURBOMACHINE COMPOSITE MATERIAL BLADE |
摘要 |
FIELD: engines and pumps. ^ SUBSTANCE: turbomachine composite material blade comprises vane made up of alternating and oriented layers of composite material interjointed by a binder material and V-shape cross section metal strips arranged on the blade vane rear and front edges. The part of inner space of the front edge metal strip adjoining point of its profile bend incorporates composite material arranged in layers across the blade vane furnished with reinforcing fibres located between adjacent layers and directed along the blade vane profile centerline. ^ EFFECT: higher impact strength of front and rear edges, uniform distribution of deformation resulted from every impact on edges, which allows using smaller-thickness edges. ^ 7 cl, 5 dwg |
申请公布号 |
RU2350757(C1) |
申请公布日期 |
2009.03.27 |
申请号 |
RU20070134993 |
申请日期 |
2007.09.21 |
申请人 |
FEDERAL'NOE GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "TSENTRAL'NYJ INSTITUT AVIATSIONNOGO MOTOROSTROENIJA IMENI P.I. BARANOVA" |
发明人 |
KARIMBAEV TEL'MAN DZHAMALDINOVICH;LUPPOV ALEKSEJ ANATOL'EVICH;PETROV JURIJ ALEKSEEVICH;EZHOV ALEKSEJ JUR'EVICH;AFANAS'EV DMITRIJ VIKTOROVICH |
分类号 |
F01D5/28 |
主分类号 |
F01D5/28 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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