Metso Valm-818417

-响应时间:≤3ms(超导失超保护模式)。

环境适应性:

-温度范围:-269°C(液氦)至+400°C(超导冷却剂);

-磁场兼容性:耐10特斯拉以上静态磁场。

2.关键技术参数

项目典型规格(参考同类产品)

输入/输出

-输入信号:4–20mA DC(支持PROFINET IO);

-输出类型:Inconel 718阀体+金刚石涂层阀芯(热导率>1000 W/m·K);

供电要求

描述

1.产品定位与核心功能

VALM-818417推测为高温超导兼容型阀门定位器,定位能源炼化、航空航天热控及超导磁体系统,聚焦液态金属冷却、毫秒级热冲击响应与磁场环境适应性。其核心功能包括:

控制性能:

-位置精度:±0.005%(全行程范围内,抗热膨胀形变);

-响应时间:≤3ms(超导失超保护模式)。

环境适应性:

-温度范围:-269°C(液氦)至+400°C(超导冷却剂);

-磁场兼容性:耐10特斯拉以上静态磁场。

2.关键技术参数

项目典型规格(参考同类产品)

输入/输出

-输入信号:4–20mA DC(支持PROFINET IO);

-输出类型:Inconel 718阀体+金刚石涂层阀芯(热导率>1000 W/m·K);

供电要求

-电压范围:9–36V DC(宽压输入,航天级冗余电源);

-功耗:≤5W(峰值),休眠模式<0.008W;

通信接口

-数字总线:SpaceWire(航天器数据总线标准);

-无线扩展:Ultra-Wideband(超导腔体内部通信)。

3.功能特性

超导系统适配:

-热管理算法:基于液态汞/钠冷却剂的相变控制模型;

-材料体系:非磁性钛合金+BN纳米润滑层(摩擦无颗粒生成)。

极端温控设计:

-双金属片补偿结构(消除-200°C温差形变);

-集成珀尔帖效应热电偶(实时监测阀体温度梯度)。

航天级安全:

-抗辐射加固(耐质子辐照剂量>1×10⁹p/cm²);

-失超保护逻辑:磁场突变时自动切换至预设安全位。

4.典型应用场景

能源与交通:

-磁约束核聚变装置冷却阀(兼容ITER标准);

-超导电缆低温阀(液氮工况,流量精度±0.01%)。

航空航天:

-液氢涡轮泵控制阀(耐空化腐蚀,压力脉动抑制至<1%);

-导弹级联推进剂阀(耐400°C燃气瞬时冲击)。

科研与医疗:

-超导MRI磁体冷却系统隔离阀(无磁干扰设计);

-聚变实验堆第一壁保护阀(耐14MeV中子辐照)。

1.Product positioning and core functions

VALM-818417 is speculated to be a high-temperature superconducting compatible valve positioner that locates energy refining,aerospace thermal control and superconducting magnet systems,focusing on liquid metal cooling,millisecond thermal shock response and magnetic field environment adaptability.Its core functions include:

Control performance:

-Position accuracy:±0.005%(within the entire stroke range,resisting thermal expansion deformation);

-Response time:≤3ms(superconductor loss-protected mode).

Environmental adaptability:

-Temperature range:-269°C(liquid helium)to+400°C(superconducting coolant);

-Magnetic field compatibility:Resistance to static magnetic fields above 10 Tesla.

2.Key technical parameters

Project Typical specifications(refer to similar products)

Input/Output

-Input signal:4–20mA DC(supports PROFINET IO);

-Output type:Inconel 718 valve body+diamond-coated valve core(thermal conductivity>1000 W/m·K);

Power supply requirements

-Voltage range:9–36V DC(wide voltage input,aerospace-level redundant power supply);

-Power consumption:≤5W(peak),sleep mode<0.008W;

Communication interface

-Digital bus:SpaceWire(spacecraft data bus standard);

-Wireless extension:Ultra-Wideband(Superconducting cavity internal communication).

3.Functional characteristics

Superconducting system adaptation:

-Thermal management algorithm:phase change control model based on liquid mercury/sodium coolant;

-Material system:non-magnetic titanium alloy+BN nano-lubricating layer(generated without friction).

Extreme temperature control design:

-Bimetallic sheet compensation structure(eliminates temperature difference deformation of-200°C);

-Integrated Peltier effect thermocouple(real-time monitoring of valve body temperature gradient).

Aerospace-grade safety:

-Radiation-resistant reinforcement(proton radiation-resistant dose>1×10⁹p/cm²);

-Over-resolution protection logic:Automatically switch to the preset safe position when the magnetic field changes suddenly.

4.Typical application scenarios

Energy and Transportation:

-Cooling valve for magnetically constrained nuclear fusion device(compatible with ITER standard);

-Superconducting cable low temperature valve(liquid nitrogen working conditions,flow accuracy±0.01%).

Aerospace:

-Liquid hydrogen turbo pump control valve(resistant to cavitation corrosion,pressure pulsation is suppressed to<1%);

-Missile cascade propellant valve(resistant to instantaneous impact of 400°C gas).

Scientific research and medical treatment:

-Superconducting MRI magnet cooling system isolation valve(non-magnetic interference design);

-The first wall protection valve of the fusion experimental reactor(resistant to 14MeV neutron radiation).