High voltage ignition cable for capacitive ignition systems of gas-turbine aircraft engines, comprising a discharge current conductor surrounded by insulation, enclosed in the internal volume of a shielding metal braid
	IBRAEV T R; BELYAEV A A; VALIEV R SH; MURYSEV A N
	2024-08-12
专利权人	UFA AGGREGATE PRODN ASSOC STOCK CO (UFAA-Non-standard)
申请日期	2024-08-12
专利号	RU2836862-C1
成果简介	NOVELTY - Invention relates to wires of gas turbine engine ignition systems. Ignition wire containing discharge current conductor, insulation and screening metal braiding includes the first cylindrical stepped fitting, to which braiding and nut are connected, as well as the first contact device soldered to the conductor. Wire includes a metal elbow in the form of an L-shaped cylindrical branch pipe connected to the braiding on one side and connected by soldering to the second cylindrical stepped fitting on the other side. Soldered seam is localized on the inner surface of the second cylindrical stepped fitting with a smaller diameter. Wire includes a second contact device soldered to the conductor, a stepped ceramic insulator, a spring and a nut fixed on the second stepped fitting. Spring is placed between the end of the second stepped fitting and the outer surface of the ceramic insulator. Second contact device is placed in the inner volume of the ceramic insulator. USE - Mechanical engineering. ADVANTAGE - Reduction of ignition wire dimensions. 1 cl, 2 dwg
IPC 分类号	F02C-007/266 ; H01B-007/04 ; H01T-013/04
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/15484
专题	中国科学院新疆生态与地理研究所
作者单位	UFA AGGREGATE PRODN ASSOC STOCK CO (UFAA-Non-standard)
推荐引用方式 GB/T 7714	IBRAEV T R,BELYAEV A A,VALIEV R SH,et al. High voltage ignition cable for capacitive ignition systems of gas-turbine aircraft engines, comprising a discharge current conductor surrounded by insulation, enclosed in the internal volume of a shielding metal braid. RU2836862-C1[P]. 2024.

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