共找到 73 条与 传感元件 相关的标准,共 5 页
Strain gauge force sensor parameter series
Characteristics and test specifications of strain gauge pressure sensors
Specifies the design requirements and tests for the conductors of these cables for installation in temperature indicator and control systems. Methods for determining the thermo-e. m. f. of conductor wires against platinum are given in the annex.
Aircraft; Nickel-chromium and nickel-aluminium thermocouple extension cables; Part 1 : Conductors; General requirements and tests
This British Standard specifies the general design and performance requirements for platinum resistance temp-erature sensors designed for the measurement of the temperature of gases or fluids in small diameter ducts. The sensors are designed for satisfactory operation for the measurement of fluid temperature whilst under high pressure. The temperature-resistance relationship is based on a sensor having a resistance of 100 Ω at 0 ℃.
Specification for general purpose platinum temperature sensors for aircraft
Transmetteurs tachymétriques triphasés bipolaires
This specification covers one type of hydraulically operated, hypodermic, jet injection apparatus for rapidly injecting, a t high pressure and velocity, through a jet orifice, metered quantities of Immunizing agents in such a manner that the immunizing agent (vaccine) makes tts own opening into the skin and penetrates to a suitable depth for imunization.
HYPODERMIC INJECTION APPARATUS, JET, FOOT OPERATED
This amendment forms a parotf Military Specification MIL-C-l4806A, dated 12 June 1969 and is approved for use bayl l Departments and Agencies of the Department of Defense
COATING, REFLECTION REDUCTING, FOR INSTRUMENT COVER GLASSES AND LIGHTING WEDGES
This specification covers requirements and quality assurance provisions for obturating band, plastic, split(molded) for use on the Cartridge, 81mm; Illuminating, M853; Smoke, RP, M819 and Practice, M879
COATING, REFLECTION REDUCTING, FOR INSTRUMENT COVER GLASSES AND LIGHTING WEDGES
Aircraft temperature sensors.
This specification defines the requirements for a grooved clamp coupling and flanges suitable for joining intermediate pressure and temperature ducting in aircraft air systems. The rigid coupling joint assembly, hereafter referred to as the joint, shall operate within the temperature range of -65 degrees Fahrenheit to +800 degrees Fahrenheit.
Thermo-Sensitive Element (Iron - Constantan)
THERMO-SENSITIVE ELEMENT (RESISTANCE BULB TYPE)
THERMO-SENSITIVE ELEMENT (RESISTANCE BULB TYPE)
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