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公开(公告)号：US20160069570A1
公开(公告)日：2016-03-10
申请号：US14479010
申请日：2014-09-05
Applicant: Solar Turbines Incorporated
Inventor： Christopher Zdzislaw Twardochleb , Stephen Paul Burke , Bharat Damodar Raghunathan , Robert James Fanella
CPC classification number: F23R3/10 , F01D9/04 , F05D2230/232 , F05D2230/60 , F05D2240/127 , F05D2250/132 , F05D2250/283 , F05D2260/30 , F05D2260/607 , F23R3/16 , F23R2900/00017
Abstract: A diffuser for a gas-turbine engine is provided. The diffuser has an outer housing, an inner housing, and a diffusion plate. The outer housing has a first wall. The inner housing has a second wall and is disposed within the outer housing. A flow passage is formed between the first wall and the second wall and has a forward end and an aft end. The diffusion plate has a plurality of openings and extends across the flow passage from the first wall to the second wall in an aft direction.
Abstract translation: 提供了一种用于燃气涡轮发动机的扩散器。 扩散器具有外壳体，内壳体和扩散板。 外壳具有第一壁。 内壳体具有第二壁，并且设置在外壳体内。 在第一壁和第二壁之间形成有流动通道，并具有前端和后端。 扩散板具有多个开口并且在向后的方向上延伸穿过从第一壁到第二壁的流动通道。
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公开(公告)号：US20160175921A1
公开(公告)日：2016-06-23
申请号：US15058141
申请日：2016-03-01
Applicant: Solar Turbines Incorporated
Abstract: A method for manufacturing a stem for a fuel injector of gas turbine engine includes forging a material into a unitary workpiece, which includes forging a top disk having a cylindrical shape, forging a body extending from a base of the top disk, and forging a lower disk connected to the body, distal to the top disk, the lower disk having a cylindrical shape oriented transverse to the top disk. The method further including machining the lower disk to form a gas gallery having a ring shape, and to define a gallery opening through the gas gallery, and machining a first fluid passage through the top disk, the body, and a portion of the gas gallery to the gallery opening, wherein the first fluid passage is in fluid communication with the gallery opening.
Abstract translation: 一种用于制造燃气涡轮发动机的燃料喷射器的杆的方法，包括将材料锻造成一体的工件，其包括锻造具有圆柱形状的顶盘，锻造从顶盘的基部延伸的主体，并锻造下部 盘连接到身体，远离顶盘，下盘具有横向于顶盘的圆柱形形状。 该方法还包括加工下盘以形成具有环形的气体库，并且限定通过气体通道的通道，并且加工通过顶部盘，主体和气体库的一部分的第一流体通道 到所述画廊的开口，其中所述第一流体通道与所述画廊开口流体连通。
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公开(公告)号：US10208959B2
公开(公告)日：2019-02-19
申请号：US15058141
申请日：2016-03-01
Applicant: Solar Turbines Incorporated
Abstract: A method for manufacturing a stem for a fuel injector of gas turbine engine includes forging a material into a unitary workpiece, which includes forging a top disk having a cylindrical shape, forging a body extending from a base of the top disk, and forging a lower disk connected to the body, distal to the top disk, the lower disk having a cylindrical shape oriented transverse to the top disk. The method further including machining the lower disk to form a gas gallery having a ring shape, and to define a gallery opening through the gas gallery, and machining a first fluid passage through the top disk, the body, and a portion of the gas gallery to the gallery opening, wherein the first fluid passage is in fluid communication with the gallery opening.
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