CN112292791A - 用于涡轮机的电气线束 - Google Patents
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Abstract
本发明涉及电气线束(1),其包括:至少一个第一电缆股(2)、至少一个第二电缆股(3,4)和连接插套(16),至少一个第一电缆股(2)和至少一个第二电缆股(3,4)外部分别至少部分地被第一屏蔽编织层(13)和第二屏蔽编织层(14,15)包围;所述连接插套(16)从外部包围第一电缆股(17)的一端和第二电缆股(18,19)的一端,其特征在于,所述连接插套(16)包括固定部(21)和压接部(20),所述固定部(21)旨在接合在涡轮机的固定构件上,第一屏蔽编织层(13)和第二屏蔽编织层(14,15)的端部(26,27,28)从外部接合到所述压接部(20)上,至少一个压接构件(32)将端部(26,27,40)固定在所述压接部(20)上。
Description
技术领域
本发明涉及一种电气线束,特别是一种用于航空领域的电气线束,更具体地说,涉及一种旨在安装在涡轮机(例如飞机的涡轮喷气发动机或涡轮螺旋桨发动机)中的电气线束。
背景技术
为了减小涡轮机的尺寸,需要找到电气线束本身的尺寸和特性允许其安装在有限空间内的技术方案。
此外,还需要开发出既能承受高温,又小巧轻便的电气线束。
为了减少电气线束的质量,可在热应力较低且在给定温度范围内(例如低于210℃)的区域内使用以轻质、热缩合成材料为主的保护套技术。
众所周知,还使用了能够承受高温(特别是高于210℃)的编织不锈钢护套。
在线束的一个分区中可以提供不锈钢护套和合成护套之间的过渡部分,所述分区特别包括所谓的过渡段。所述过渡部分也可用于将线束固定到涡轮机的固定构件上。这种连接例如是通过将构件插入弹性夹来实现的。
此外,电气线束通常有分支点,在那里单股电线被分成若干股。这可以在带有所谓旁路构件的线束区域进行。旁路构件与过渡段分开,位于过渡段下游或上游。所述旁路构件还可以包括用于将线束连接到涡轮机的固定构件上的区域。
由于结构原因,线束连接到涡轮机固定构件的区域也可能存在形状缺陷。这些形状上的缺陷使它们更难安装在涡轮机上。
使用两个独立的衬套增加了线束的尺寸和重量,使得将这样的线束集成到一个小型涡轮机中变得困难。
电缆和电缆股外部也被电磁屏蔽护套包围。除上述限制外,还必须确保过渡和分支部分的电磁屏蔽连续性。
本发明旨在以简单和经济的方式弥补上述全部或部分缺点。
发明内容
为此,本发明涉及一种电气线束,所述电气线束包括:至少一个第一电缆股、至少一个第二电缆股和连接插套,至少一个第一电缆股和至少一个第二电缆股外部分别至少部分地被第一屏蔽编织层和第二屏蔽编织层包围;所述连接插套从外部包围第一电缆股的一端和第二电缆股的一端,其特征在于,所述连接插套包括固定部和压接部,所述固定部旨在接合在涡轮机的固定构件上,第一屏蔽编织层和第二屏蔽编织层的端部从外部接合到所述压接部上,至少一个压接构件将端部固定在压接部上。
连接插套将屏蔽编织层的固定和压接功能组合成一个一体式刚性元件。因此,压接部具有足够的刚性,以允许用压接工具压接屏蔽编织层。这样的压接保证了屏蔽的电气连续性。
此外,连接件的形状可以固定,例如圆柱形,以便于线束在涡轮机相关构件上的安装和角度定位。
屏蔽编织层可由编织材料(例如铜镍基合金)制成。
例如,连接插套可以由金属制成。
线束可以由一根第一电线股和几根第二电线股(例如两根或更多根第二电线股)组成。
另外,第一或第二屏蔽编织层的端部能插入连接插套中,并能在压接部外部反向折叠180°,因此第二或第一屏蔽编织层的端部仅在压接部外部插入。
换句话说,第二或第一屏蔽编织层的端部不穿过连接插套。
每根电缆股外部能至少部分地被第一保护编织层包围,其中第一保护编织层在重叠区域中重叠。
第一保护编织层可以是织物护套。
例如,第一保护编织层由间位芳纶制成。
第一保护编织层能在重叠区域缝合在一起。
屏蔽编织层能从外部包裹在第一保护编织层周围。
每根电缆股外部能至少部分地被第二保护套包围。
电缆股中的一根的第二保护套的端部能从外部安装在压接部上,也能从外部安装在屏蔽编织层的压接的端部上。
第二保护套的端部能通过使用压接构件从外部压接到压接部上来固定。
第二保护套能至少部分地从外部包围屏蔽编织层。
连接插套的内部空间至少部分填充有树脂,以使电缆、屏蔽编织层和/或保护套嵌入。
本发明还涉及一种涡轮机,例如用于飞机的涡轮喷气发动机或涡轮螺旋桨发动机,其特征在于,所述涡轮机包括上述类型的电气线束。
在参考附图阅读作为非限制性示例给出的以下描述时,将更好地理解本发明,并将呈现本发明的其它细节、特征和优点。
附图说明
-图1是根据本发明的一个实施例的电气线束的示意性剖视图;
-图2是连接插套的示意图;
-图3是根据本发明的另一实施例的电气线束的示意性半剖视图;
-图4是通过紧固件固定的根据本发明的线束的部分的透视图。
具体实施方式
图1示出了根据本发明的第一实施例的线束1的一部分。线束由第一电缆股2和两根第二电缆股3,4组成,电缆股用于从电源向涡轮机组件供电,或在组件之间传递电信号。每根电缆至少有一根电导线。第一电缆的每根电导线5,6被分支到由电导线7,8组成的第二电缆股3,4中。
第一电缆股2和每根第二电缆股3,4外部被第一织物保护编织层包围。第一电缆股2的第一保护编织层9和第二电缆股3,4的第一保护编织层10,11在重叠区域12中缝合在一起。重叠区域12位于第一电缆股2的外部。
例如,第一保护编织层9,10,11由间位芳纶型合成材料制成。
第一电磁屏蔽编织层13从外部包围第一电缆股2和第一保护编织层9。类似地,第二电缆股3,4中的每一根及其各自的第一保护编织层10,11外部被第二电磁屏蔽编织层14,15包围。屏蔽编织层13,14,15是由铜和镍基合金制成的编织套管。
连接插套16,如图2所示,从外部包围第一电线股2的一端17和第二电线股3,4的端部18,19。
连接插套16是刚性的,由圆柱形压接部20和直径大于压接部的圆柱形固定部21组成。
压接部20具有由第一环形凸缘22隔开的两个圆柱形区域20a,20b,并且所述压接部的端部具有第二环形凸缘23。固定部在其端部有两个环形凸缘24,25。
连接插套16可以由金属(例如不锈钢或钛)或合成材料(例如玻璃填充树脂)制成。
第一屏蔽编织层13和第二屏蔽编织层14,15的端部27,26,40从外部接合到连接件16的压接部20上。第二屏蔽编织层14,15与连接插套16接合,并在压接部20处向外折叠,翻转180°。换句话说,第二屏蔽编织层14,15穿过连接插套16并且弯曲,这使得这些屏蔽编织层的端部26,40从外部包围压接部20的外表面。第一屏蔽编织层13不穿过衬套16,并且其端部27从外部接合到压接部20上。
第一电缆股2的第二保护套28的一端31安装在压接部20的外部,以及屏蔽编织层的相应端部27,26,40的外部。连接这些端部31,26,27,40的方式是使用压接环32从外部将其压接到刚性压接部20上。压接环32安装在各分区20a和20b处。在拧紧压接工具32时,压接部20的刚性可防止其变形。
此外,紧固部21用于插入涡轮机的紧固元件例如紧固夹33(图4中可见)中。紧固部21的刚性保障了所述构件的形状,从而便于操作员在紧固件33上定位。
第二电缆股3,4的第二保护套29,30的相应端部34,35安装在固定部21内。固定部21的内部容积填充有树脂39,例如环氧树脂,以使第二电缆股3,4的第二保护套29,30嵌入。
因此,连接插套16允许从第二不锈钢保护套过渡到第二合成保护套,并将电缆股分支成多根电缆股。使用单个衬套16可减小电气线束的尺寸,从而更容易将此类线束集成到小型涡轮机中。
屏蔽编织层13,14,15的布置也确保了连接插套处电磁屏蔽的连续性。
图3示出了根据本发明的另一实施例的电气线束的一部分。在所述具体实施例中,第一电缆股2和第二电缆股3,4的第一保护编织层9,11重叠并缝合在一起的重叠区域12位于连接插套16的固定部21内。
图4显示了两个线束36,37在紧固件33上的安装。具体地说,每个线束具有多个如上所述的连接插孔16。每个连接插套16的紧固部卡入紧固件33。具体而言,如所知,每个紧固件33具有由两个可弹性变形支腿组成的夹子形状。每个紧固件33本身可连接到涡轮机的固定部。紧固件33也可以是带硅酮护套的夹子。
每个线束36,37还包括可连接到涡轮机组件的连接头38。
Claims (9)
1.用于涡轮机的电气线束(1),所述电气线束具有至少一个第一电缆股(2)、至少一个第二电缆股(3,4)和连接插套(16),至少一个第一电缆股(2)和至少一个第二电缆股(3,4)外部分别至少部分地被第一屏蔽编织层(13)和第二屏蔽编织层(14,15)包围;所述连接插套(16)从外部包围第一电缆股(17)的一端和第二电缆股(18,19)的一端,
其特征在于,所述连接插套(16)包括固定部(21)和压接部(20),所述固定部(21)旨在接合在所述涡轮机的固定构件(33)上,第一屏蔽编织层(13)和第二屏蔽编织层(14,15)的端部(26,27,40)从外部接合到所述压接部(20)上,至少一个压接构件(32)将端部(26,27,40)固定在所述压接部(20)上,第一屏蔽编织层(13)或第二屏蔽编织层(14,15)的端部(26,27,40)插入所述连接插套(16)中并在所述压接部(20)外部向后弯曲180°,第二屏蔽编织层(14,15)或第一屏蔽编织层(13)的端部(26,27,40)仅在所述压接部(20)外部插入。
2.根据权利要求1所述的电气线束(1),其特征在于,每根电缆股(2,3,4)外部至少部分地被第一保护编织层(9,10,11)包围,所述第一保护编织层(9,10,11)在重叠区域(12)中重叠。
3.根据权利要求2所述的电气线束(1),其特征在于,所述第一保护编织层(9,10,11)为织物护套。
4.根据权利要求3所述的电气线束(1),其特征在于,所述第一保护编织层(9,10,11)在所述重叠区域(12)中缝合在一起。
5.根据权利要求2至4中任一项所述的电气线束(1),其特征在于,屏蔽编织层(13,14,15)从外部包围所述第一保护编织层。
6.根据权利要求2至5中任一项所述的电气线束(1),其特征在于,每根电缆股(2,3,4)外部至少部分地被第二保护套(28,29,30)包围。
7.根据权利要求6所述的电气线束(1),其特征在于,电缆股(2,3,4)中的一根的第二保护套(28,29,30)的端部从外部安装在所述压接部(20)上,并且从外部安装在屏蔽编织层(13,14,15)的压接的端部(26,27,40)上。
8.根据权利要求6或7所述的电气线束(1),其特征在于,第二保护套(28,29,30)至少部分地从外部包围屏蔽编织层(13,14,15)。
9.根据权利要求1至8中任一项所述的电气线束(1),其特征在于,所述连接插套(16)的内部容积至少部分填充有树脂(39),以使电缆股(2,3,4)、屏蔽编织层(13,14,15)和/或保护套(9,10,11,28,29,30)嵌入。
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FR1854464A FR3081622B1 (fr) | 2018-05-25 | 2018-05-25 | Harnais electrique pour turbomachine |
FR1854464 | 2018-05-25 | ||
PCT/FR2019/051210 WO2019224502A1 (fr) | 2018-05-25 | 2019-05-24 | Harnais electrique pour turbomachine |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2022188449A1 (zh) * | 2021-03-12 | 2022-09-15 | 长春捷翼汽车零部件有限公司 | 一种线缆组件和线缆组件的制备方法 |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3113937B1 (fr) * | 2020-09-10 | 2022-07-29 | Safran Aircraft Engines | Fixation d’une gaine tressée dans une turbomachine |
US11784482B2 (en) * | 2020-10-20 | 2023-10-10 | Apple Inc. | Electrical connection monitoring using cable shielding |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20040256136A1 (en) * | 2003-01-29 | 2004-12-23 | Labinal | System for modifying the structure of an electrical harness |
US20060278423A1 (en) * | 2004-11-26 | 2006-12-14 | Yazaki Corporation | High-voltage wire harness |
CN101075708A (zh) * | 2006-05-19 | 2007-11-21 | 伊斯帕诺-絮扎公司 | 屏蔽且密封的电气配线 |
FR2937471A1 (fr) * | 2008-10-16 | 2010-04-23 | Eurocopter France | Procede pour raccorder un faisceau electrique a un connecteur et harnais mettant en oeuvre ce procede |
KR20110135031A (ko) * | 2010-06-10 | 2011-12-16 | 주식회사 넥센테크 | 나사식 케이블 단부 차폐층 마감기구 |
KR20120138215A (ko) * | 2010-04-12 | 2012-12-24 | 타이코 일렉트로닉스 유케이 리미티드 | 동축 커넥터 및 이를 어셈블링하는 방법 |
CN104282371A (zh) * | 2013-07-04 | 2015-01-14 | 住友电装株式会社 | 屏蔽导电体及其制造方法 |
JP2015076163A (ja) * | 2013-10-07 | 2015-04-20 | 株式会社七星科学研究所 | 電源ケーブルコネクタ |
CN105591210A (zh) * | 2014-11-06 | 2016-05-18 | 住友电装株式会社 | 线束的屏蔽构造 |
CN105993051A (zh) * | 2013-11-29 | 2016-10-05 | 住友电装株式会社 | 电线的屏蔽结构 |
CN106911045A (zh) * | 2015-12-22 | 2017-06-30 | 矢崎(中国)投资有限公司 | 屏蔽连接结构 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1424068A (en) * | 1973-04-10 | 1976-02-04 | Standard Telephones Cables Ltd | Jointing arrangement for a coaxial core |
US3801730A (en) * | 1973-05-23 | 1974-04-02 | Gen Electric | High voltage cable splice with provision for testing the insulation thereof and method of making same |
DE3633208A1 (de) * | 1986-09-30 | 1988-04-07 | Spinner Gmbh Elektrotech | Abgedichteter kabelverbinder |
US7799997B2 (en) * | 2007-04-27 | 2010-09-21 | Milliken & Company | Innerduct structure having increased flexibility |
JP5740146B2 (ja) * | 2010-12-10 | 2015-06-24 | 矢崎総業株式会社 | ワイヤハーネス |
US9543747B2 (en) * | 2013-10-30 | 2017-01-10 | Delphi Technologies, Inc. | Method for splicing shielded wire cables |
JP6788802B2 (ja) * | 2017-05-26 | 2020-11-25 | 住友電装株式会社 | ワイヤハーネス |
-
2018
- 2018-05-25 FR FR1854464A patent/FR3081622B1/fr active Active
-
2019
- 2019-05-24 WO PCT/FR2019/051210 patent/WO2019224502A1/fr unknown
- 2019-05-24 CN CN201980041320.2A patent/CN112292791B/zh active Active
- 2019-05-24 EP EP19744755.0A patent/EP3804059A1/fr active Pending
- 2019-05-24 US US17/058,971 patent/US11289827B2/en active Active
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20040256136A1 (en) * | 2003-01-29 | 2004-12-23 | Labinal | System for modifying the structure of an electrical harness |
US20060278423A1 (en) * | 2004-11-26 | 2006-12-14 | Yazaki Corporation | High-voltage wire harness |
CN101075708A (zh) * | 2006-05-19 | 2007-11-21 | 伊斯帕诺-絮扎公司 | 屏蔽且密封的电气配线 |
FR2937471A1 (fr) * | 2008-10-16 | 2010-04-23 | Eurocopter France | Procede pour raccorder un faisceau electrique a un connecteur et harnais mettant en oeuvre ce procede |
KR20120138215A (ko) * | 2010-04-12 | 2012-12-24 | 타이코 일렉트로닉스 유케이 리미티드 | 동축 커넥터 및 이를 어셈블링하는 방법 |
KR20110135031A (ko) * | 2010-06-10 | 2011-12-16 | 주식회사 넥센테크 | 나사식 케이블 단부 차폐층 마감기구 |
CN104282371A (zh) * | 2013-07-04 | 2015-01-14 | 住友电装株式会社 | 屏蔽导电体及其制造方法 |
JP2015076163A (ja) * | 2013-10-07 | 2015-04-20 | 株式会社七星科学研究所 | 電源ケーブルコネクタ |
CN105993051A (zh) * | 2013-11-29 | 2016-10-05 | 住友电装株式会社 | 电线的屏蔽结构 |
CN105591210A (zh) * | 2014-11-06 | 2016-05-18 | 住友电装株式会社 | 线束的屏蔽构造 |
CN106911045A (zh) * | 2015-12-22 | 2017-06-30 | 矢崎(中国)投资有限公司 | 屏蔽连接结构 |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2022188449A1 (zh) * | 2021-03-12 | 2022-09-15 | 长春捷翼汽车零部件有限公司 | 一种线缆组件和线缆组件的制备方法 |
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WO2019224502A1 (fr) | 2019-11-28 |
FR3081622B1 (fr) | 2021-04-30 |
EP3804059A1 (fr) | 2021-04-14 |
US11289827B2 (en) | 2022-03-29 |
CN112292791B (zh) | 2022-07-05 |
US20210218159A1 (en) | 2021-07-15 |
FR3081622A1 (fr) | 2019-11-29 |
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