| 摘要 |
System for registration of parameters of power unit of aircraft relates to systems for registration of parameters of different objects, in particular systems that collect information on technical condition of parameter of gas-turbine engines for power unit of aircraft. To the system that has two blocks of formers, two blocks of normalizers, two blocks for control of single signals, two blocks for transformation of signals and control of indicators and two blocks for registration of information additionally are included two operation blocks, two blocks for reception-transfer of code, two blocks of galvanic uncoupling, two switches of information code and two time blocks. Technical result is in increase of operation characteristics of gas-turbine engines of power unit, provision of reliable information for synchronized in time parameters of gas-turbine units in each block of registration of information, increase of functional abilities of the system, provision of reliable operation of has-turbine engines of power unit of aircraft by technical condition. |
