• The composite article as recited in claim 1 further characterized by the upper and lower surfaces being contoured to a blade aerodynamic profile.

    综合文章作为背诵权利要求1进一步特点是表面等高刀片气动的个人资料。

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  • The composite article recited in claim 8 further characterized by the upper and lower surfaces being contoured to a blade aerodynamic profile.

    综合文章背诵索赔8进一步特点是表面等高刀片气动的个人资料。

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  • The composite article as recited in claim 13 contoured to a blade aerodynamic profile.

    综合文章作为背诵索赔13等高刀片气动个人资料

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  • This paper has solved problem of machining for the profile of the blade pump stator to improve trapezium accelerated motion regulation.

    本文研究叶片定子改进梯形加速度运动规律轮廓线型面靠模加工问题

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  • The isothermal adjustment method was adopted to relieve distortion of titanium alloy blade profile.

    采用等温热校形的方法减小钛合金叶片型面翘曲变形

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  • A diffuser cascade of a centrifugal compressor was chosen to be designed with the proposed approach, with its two operating points specified, and its blade profile to be optimized.

    离心压缩机扩压器叶栅为例,在两个给定设计工况下采用所提出方法求解其最佳叶片型线

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  • It is important to study the mechanism between the cascade blade profile parameters and the thrust reverser effectiveness.

    航空发动机叶反推器叶参数反推效率、流量系数之间的规律对于反推装置的设计具有重要意义

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  • Arc crown profile, blade cutter setting.

    弧形冠部设计,翼式分布。

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  • Why use computer-controlled cutting equipment vibrating blade profile?

    为何要使用电脑控制振动仿切割设备?。

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  • It is shown from the results that the security and efficiency for LP last stage blade of air-cooling units can be obtained through adopting special profile, controlling reaction and incidences.

    分析结果表明采用专用强化型、控制反动度、控制角等方法可以有效保证机组变工况安全高效运行。

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  • It is proved that the profile loss can be decreased with the use of advanced blade through the comparison of loss coefficient of blade surface overall pressure.

    通过叶片表面损失系数证实先进叶型在流动可以降低叶型损失。

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  • The measuring method is expatiated and how to get the part drawings and blade profile drawings are described in details by the author.

    详细介绍测量方法如何得到各叶轮零件图。

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  • The great thing about this katana is the new large geometry blade profile. It has a profile that is larger than most blades which allows for the inexperienced cutter to cut successfully.

    的亮点在于设计宽大的符合几何学刀身造型这样豪壮的设计为了能够确保缺乏练习的使用者能够成功进行斩

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  • It is not only useful in the selection of machining method, design of tools, gauges and special machine tools; but also is very useful in machining and inspection of blade profile with NC method.

    不仅叶片型面加工方法选择,工、夹、量具专用机床设计而且特别是对这类叶片型面的数控加工和测量都具有重要意义

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  • The results so far obtained indicate that the method can provide a valuable insight on the relative and absolute flow patterns within the impeller passages and the effect of blade profile.

    研究结果表明所采用方法获得叶轮内部刘道内相对绝对流动模式以及叶片形状的影响

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  • In this paper, a mathematic model of the straight axis rotate blade is introduced by analysing the forming principle of the blade profile and applying the theory of 3d geometry transformation.

    本文通过旋转叶片型面成形规律分析运用几何变换理论推导出了直轴旋转叶片型面的数学模型

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  • The corner-crimping blade can be adjusted according to the requirement of different profile.

    角刀前后左右调整方便,适应不同型材需要

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  • The contrast of new designed blade with the original one is made in the design of free vortex flow combining with aft-loading profile.

    自由后加载型相结合设计设计设计进行了对比

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  • Results show that incidence affects evidently not only the pressure profile, but also the flows behavior close to the blade profile, especially in the rear part of the cascade passage.

    结果表明冲角不仅叶片表面压力分布而且对叶片附近流动状态特别是叶栅流道半部,有很大的影响

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  • Thus, the aerodynamic performance of stage is im-proved obviously, the profile loss decreases through using the "after loading" blade.

    优化后部加载明显提高气动性能降低了叶型能量损失

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  • The idea of the design method throws off the reliance on the engineering experience, avoids complicated special transformation, and has the blade profile and impeller optimized.

    本文设计思想减少了对工程经验依赖避免了复杂空间转换,可使叶轮得到优化。

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  • It is shown from the results that the security and efficiency for LP last stage blade of air-cooling units can be obtained through adopting special profile, co...

    分析结果表明采用专用强化叶型、控制反动度、控制攻角等方法可以有效保证空冷机组变工况安全高效运行。

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  • Their loss performance, exit flow angle, exit flow velocity as well as the flow velocity distribution on the blade-profile surfaces obtained in both cases are analyzed comparatively.

    本文对试验的损失特性、出气特性、速度特性、叶型表面速度分布特性等作了对比分析

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  • Effect of impeller of different blade profile on the highest pressure point, optimum operating point, shape of pressure curve and efficiency of the fan were analyzed.

    分析不同叶片型线叶轮风机最高压力最佳工况点、压力曲线形状效率影响,同时探讨风机不同叶片型线的工程实用价值。

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  • Their loss performance, exit flow Angle, exit flow velocity as well as the flow velocity distribution on the blade-profile surfaces obtained in both cases are analyzed comparatively. It is proven t...

    本文对试验的损失特性、出气特性、速度特性、叶型表面速度分布特性等作了对比分析

    youdao

  • Their loss performance, exit flow Angle, exit flow velocity as well as the flow velocity distribution on the blade-profile surfaces obtained in both cases are analyzed comparatively. It is proven t...

    本文对试验的损失特性、出气特性、速度特性、叶型表面速度分布特性等作了对比分析

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