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Method and apparatus for suppressing the noise of a fan-jet engine

阅读:254发布:2022-10-29

专利汇可以提供Method and apparatus for suppressing the noise of a fan-jet engine专利检索,专利查询,专利分析的服务。并且A tubular housing is disposed in spaced relation around the casing of a fan-jet engine and extends rearwardly therefrom. A convoluted ring is joined at its circular forward edge to the aft edge of the engine casing and is formed with lobes which extend axially thereof and increase in radial dimension in the downstream direction, so that the aft ends of the lobes project both radially inwardly from said engine casing and radially outwardly to the wall of said housing at the aft end of the latter. The forward edge of a nozzle is joined to the aft edge of the housing, and fan air of the engine flows through the space between the engine casing and the housing, through the spaces between the lobes, and into the nozzle. Exhaust gas of the engine flows from the engine into the passages bounded by the inner surfaces of the lobes and thence into the nozzle.,下面是Method and apparatus for suppressing the noise of a fan-jet engine专利的具体信息内容。

1. In a jet propulsion plane having a fan-jet engine, the combination comprising: a tubular housing disposed in spaced relation around the aft portion of the casing of said engine and projecting beyond the aft edge thereof, fan air of said engine flowing through the space between said housing and said casing; a convoluted ring the forward edge of which is fixedly joined to the aft edge of said casing, said ring being formed with lobes which extend axially thereof and gradually increase the radial dimension in the downstream direction so that their aft ends project both radially inwardly and radially outwardly from the aft edge of said casing, said lobes abutting the wall of said housing at the aft end of the latter; and a thrust nozzle the forward edge of which is fixedly joined to the aft edge of said housing, fan air of said engine flowing from the space between said housing and said casing into the spaces between the lobes of said ring and thence dividing therein for flow into said nozzle, the aft ends of the lobes of said ring being fixedly joined together so that exhaust gas of said engine flowing through the radially projecting passages bounded by the inner surfaces of said lobes and thence dividing therein for flow into said nozzle, whereby alternately disposed streams of fan air and exhaust gas enter the forward end of said nozzle.
2. The combination defined in claim 1 including: a tube fixedly connected to the aft bearing housing of the drive shaft of said engine and extending rearwardly therefrom in coaxial relation with said housing, the aft ends of the lobes of said ring being fixedly joined to the aft end of said tube; and a cone the base edge of which is fixedly joined to the aft edge of said tube.
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