The Circuit Compensation Technique for Improving Temperature Drift Properties of Gas Sensors

1、

Temperature Drift Compensation for a High Pressure Eddy Current Displacement Sensor

一类耐高压电涡流位移传感器的温度补偿研究

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2、

The Methods of Reducing the Influence of the Temperature Drift

减小温度漂移影响的措施

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3、

Design of Low Temperature Drift and Low Power Consumption Bandgap Reference

一种低温漂低功耗的带隙基准源的设计

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4、

A Compensation Method of the Temperature Drift of Image Sensor

图象传感信号温度漂移的补偿方法

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5、

Temperature drift with different grid voltage is different, too.

不同的栅极电压下的温度漂移也不相同。

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6、

The dopants of Al_2O_3 greatly inhibited the increase of crystallite size and the phase transformation from tetragonal to monoclinic, also made the phase transformation temperature and crystal lattice distortion increase.

Al2O3的添加抑制了ZrO2（3Y）晶粒的增长和四方相向单斜相的结构相变，使相变温度显著提高，晶格畸变增大。

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7、

Fortunately the research method and obtained results have universality, which can be applied to analyze temperature field and thermal distortion field with axial symmetry thermal models.

研究方法和所得结论具有普适性，可以应用到其它具有轴对称性热模型产生的温度场、热形变分析工作中。

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8、

Temperature Field and Thermal Distortion Field of Nd: YVO_4 Crystal with Double-Ends Pumping

双端泵浦Nd：YVO4晶体温度场及热形变场的研究

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9、

The transient temperature distribution and thermal distortion of optical coating components under an annular high-power continuous wave laser radiation

环状连续强激光下光学薄膜的瞬温和热畸变

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10、

The measuring of temperature change and distortion in RTM moulds shows that the exothermic peak of resin in the cavity can be adjusted through catalyst contents. The cracking and softening of surface resins result in the mould failure.

RTM模腔内温度变化与形变的测试结果表明：模腔内树脂的放热峰可以通过改变固化剂的含量适当调节，模腔表面胶衣及表面层树脂应能承受120℃的热疲劳冲击；

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11、

Chapter 2 study the temperature and heat distortion, using finite element software to analysis GMA temperature field and the heat distortion.

第二章研究了GMA的温度场和热变形，使用有限元软件对GMA温度场及热变形进行了分析。

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12、

During conventional hot extrusion processes, temperature and distortion of the billets change unevenly, so the dimension, shape, organization and capability of the profile will be deterioration.

在常规的铝及铝合金热挤压过程中，金属的温度和变形是很不均匀的，这将导致产品的尺寸、形状、组织和性能等质量方面的缺陷。

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13、

The characteristics of dynamic welding angular distortions of aluminum alloy5A12 with TIG welding are investigated by self-made welding dynamic temperature and distortion measuring system.

利用温度与变形实时测量系统，对铝合金5A12薄板氩弧焊接动态角变形过程进行了试验研究，探讨通过特征值来描述角变形动态行为。

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14、

The Temperature Distortion Generator ( TDG) design specifications, design technique and the technology of its fabrication were presented. The TDG was tested and calibrated using a turbojet engine and a turbofan engine.

介绍了航空发动机温度畸变试验装置设计技术与研制方法，主要设备及设计技术指标，以及用A型涡轮喷气发动机B型涡轮风扇发动机调试和对比试验结果。

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15、

The pressure and the temperature distortion can cause the compressor to lose the stability and enter the buzz. When the engine loses steadily, it can endanger the flight safety directly.

对气流最敏感的部件是风扇和压气机，恶劣的压力和温度畸变会使得压气机丧失稳定性进入喘振，发动机的失稳会直接危及飞行安全。

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16、

The influence of the pressure and temperature distortion to the engine stability is one of important target to evaluate aircraft engine. The fan and compressor is the most sensitive part to the air current.

压力和温度畸变对发动机稳定性影响的评定是当代航空燃气涡轮发动机适用性战术指标的重要内容之一。

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17、

According to the total pressure and temperature distortion question in the aircraft engine using process, this article closely track overseas development tendency and develop one mathematics physical model to evaluate the compressor system stability.

本文根据当前航空发动机使用过程中遇到的总压和温度畸变问题，紧密跟踪国外发展趋势，发展了一种在发动机环境下评定航空燃气涡轮发动机压缩系统稳定工作边界的数学物理模型。

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18、

Sensitive coefficients of engine circumference temperature distortion were derived. A group of temperature distortion parameters with most influence on steady operation was finally determined.

得到了发动机的周向温度畸变敏感系数，最终确定了对发动机稳定工作影响最大的一组温度畸变参数。

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19、

The magnitude of pressure distortion and temperature distortion determines the severity of the combined distortion effect on the fan or compressor stability.

压力畸变和温度畸变的相对大小，决定了组合畸变对风扇或压气机稳定性影响的严重程度。

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20、

The effect of combined distortion on engine stability is not a simple addition of pressure and temperature distortion effects, but a complex nonlinear relationship.

组合畸变对发动机稳定性的影响，不是压力畸变和温度畸变单独影响的简单相加，而是一种非常复杂的非线性关系。

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