首页> 外国专利> THRUST VECTORING APPARATUS FOR A JET ENGINE, CORRESPONDING JET ENGINE, THRUST VECTORING METHOD AND UPGRADING METHOD FOR A JET ENGINE

THRUST VECTORING APPARATUS FOR A JET ENGINE, CORRESPONDING JET ENGINE, THRUST VECTORING METHOD AND UPGRADING METHOD FOR A JET ENGINE

机译:喷气发动机的推力矢量装置,相应的喷气发动机,喷气发动机的推力矢量方法和升级方法

摘要

The thrust vectoring apparatus comprises: a housing defining a primary outletfor emitting the primary jet; Coandasurfaces extending from opposing regions of said housing, and radially spacedfrom the primary outlet such that a step is definedbetween each Coanda surface and the primary outlet; ducts leading from a fluidsource to secondary outlets; and flow controlmeans operable to control the mass flow through the secondary outlets. Whenthe jet engine operates to exhaust a primary jetthrough the primary outlet, low pressure regions are formed in the vicinity ofthe steps. Each secondary outlet is located adjacentone of the Coanda surfaces so as to emit a secondary flow into a low pressureregion. On activation of the secondary flow by theflow control means, the primary jet is entrained by the Coanda surfaceopposing the Coanda surface adjacent said the secondaryoutlet from which the secondary flow has been emitted. Method of vectoring thethrust or of upgrading existing jet engines withthe thrust vectoring apparatus and jet engines comprising the thrust vectoringapparatus are disclosed
机译:推力矢量设备包括:外壳,该外壳定义了主出口用于发射初级射流;康达从所述壳体的相对区域延伸并径向间隔开的表面从主要出口处定义一个步骤在每个柯恩达表面和主要出口之间;流体引出的导管来源到二级网点;和流量控制用于控制通过次级出口的质量流量的装置。什么时候喷气发动机运转以排出主喷气通过主出口,在附近形成低压区域步骤。每个辅助出口都位于附近柯恩达表面之一,以便向低压排放二次流地区。在通过流量控制装置,主射流被柯恩达表面夹带相对于柯恩达表面,相邻的是次要的二次流已从其排出的出口。向量化的方法推力或升级现有的喷气发动机推力矢量装置和包括推力矢量的喷气发动机装置被公开

著录项

  • 公开/公告号CA2729685C

    专利类型

  • 公开/公告日2013-01-29

    原文格式PDF

  • 申请/专利权人 BAE SYSTEMS PLC;

    申请/专利号CA20092729685

  • 发明设计人 WARSOP CLYDE;

    申请日2009-06-23

  • 分类号F02K1;B64C39/02;F02K1/28;F02K1/36;F02K3/077;

  • 国家 CA

  • 入库时间 2022-08-21 16:38:10

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