Small Aircraft Autopilot
2024-06-20
专利权人IND AUTOMATIC BUREAU STOCK (INAU-Non-standard)
申请日期2024-06-20
专利号RU2832351-C1
成果简介NOVELTY - Proposed autopilot comprises housing accommodating flight control computer, actuators in the form of servo drives, which are electromechanical servo drives of rotary type with built-in mechanical overload clutch and electromagnetic engine clutch/disengagement clutch. Console-computer contains six structural-functional modules, one of which is a display module containing a liquid crystal indicator, information input and processing means and five functional modules based on functional boards (FB1-FB5), first of which (FB1) is central, containing two processors, one of which is main, and the other is controlling, and made with possibility of connection with servo drives to corresponding control channel, second (FB2) provides communication with onboard information systems, including attitude and heading reference system, air signal and navigation systems, FB-3 and FB-4 modules provide analogue-to-digital conversion of DC and AC signals and digital-to-analogue conversion of DC signals, as well as exchange with onboard systems via ARINC-429 lines, PF-5 module contains four independent power sources. USE - Aviation. ADVANTAGE - Increasing the autopilot's fail-safety, improving the aircraft's stability and controllability characteristics, and increasing flight safety. 1 cl, 3 dwg
IPC 分类号B64C-013/18 ; G05D-001/00
国家俄罗斯
专业领域信息技术
语种英语
成果类型专利
文献类型科技成果
条目标识符http://119.78.100.226:8889/handle/3KE4DYBR/16167
专题中国科学院新疆生态与地理研究所
作者单位
IND AUTOMATIC BUREAU STOCK (INAU-Non-standard)
推荐引用方式
GB/T 7714
KNIGA V S,BISENOV O V,EGOROV V A,et al. Small Aircraft Autopilot. RU2832351-C1[P]. 2024.
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