公开(公告)号：US5483793A

公开(公告)日：1996-01-16

申请号：US078334

申请日：1970-09-02

Applicant: Barry Weinstein ,  John M. Koshoffer ,  Roy E. Moyer

Inventor： Barry Weinstein ,  John M. Koshoffer ,  Roy E. Moyer

IPC: F02K1/38 ,  F02K1/82 ,  F02K3/10 ,  F02K3/06

CPC classification number: F02K1/386 ,  F02K1/825

Abstract: A gas turbine engine of the type generating a hot gas stream and a fan stream includes a mixer having upstream and downstream portions which define first and second chutes for efficiently mixing the streams prior to discharge through an engine nozzle. Means are provided to selectively communicate the downstream chutes with alternate ones of the upstream chutes to cool the downstream mixer portion and reduce the infrared radiation emissions from the nozzle,

Abstract translation: 产生热气流和风扇流的类型的燃气涡轮发动机包括具有上游和下游部分的混合器，所述上游和下游部分限定第一和第二滑槽，用于在通过发动机喷嘴排出之前有效地混合流。 提供装置以选择性地将下游斜槽与替代的上游滑槽通信，以冷却下游混合器部分并减少来自喷嘴的红外辐射发射，

公开(公告)号：US4685942A

公开(公告)日：1987-08-11

申请号：US453011

申请日：1982-12-27

Applicant: David D. Klassen ,  Roy E. Moyer ,  Frank A. Lastrina ,  Robert P. Tameo

Inventor： David D. Klassen ,  Roy E. Moyer ,  Frank A. Lastrina ,  Robert P. Tameo

IPC: F02C7/052 ,  B01D45/04

CPC classification number: F02C7/052 ,  Y10T137/0536

Abstract: The invention is an improved inlet particle separator for removing extraneous matter from a stream of air directed into the engine's core section. The improved separator utilizes two stages of separation. The first stage is an axial flow separator for initially separating engine inlet air into a first flow of relatively contaminated air and a second flow of relatively clean air. This first stage of separation is accomplished by sharply turning the air flow radially inwardly so that the relatively dense extraneous matter continues in its original direction into a scavenge system. A second stage of separation is accomplished in the scavenge system and comprises a centrifugal separator that separates the first flow of air into third and fourth flows of relatively contaminated air for the purpose of protecting a blower that powers the flow through the scavenge system and which is in flow communication with only the relatively less contaminated fourth flow of air.

Abstract translation: 本发明是一种改进的入口颗粒分离器，用于从引导到发动机的核心部分的空气流中除去外来物质。 改进的分离器利用两个阶段的分离。 第一级是用于将发动机入口空气初始分离成相对污染的空气的第一流和相对干净的空气的第二流的轴流分离器。 这种分离的第一阶段是通过使空气流径向向内旋转而实现的，使得相对致密的外来物质沿其原始方向继续进入扫气系统。 分离的第二阶段在清扫系统中完成，并且包括离心分离器，其将第一空气流分离成第三和第四相对污染的空气流，以保护对通过扫气系统的流动提供动力的鼓风机， 与只有相对较少受污染的第四个空气流的流动通信。

公开(公告)号：US5682739A

公开(公告)日：1997-11-04

申请号：US473392

申请日：1995-06-07

Applicant: Barry Weinstein ,  John M. Koshoffer ,  Roy E. Moyer

Inventor： Barry Weinstein ,  John M. Koshoffer ,  Roy E. Moyer

IPC: F02K1/38 ,  F02K1/82 ,  F02K3/10 ,  F02K3/06

CPC classification number: F02K1/386 ,  F02K1/825

Abstract: A gas turbine engine of the type generating a hot gas stream and a fan stream includes a mixer having upstream and downstream portions which define first and second chutes for efficiently mixing the streams prior to discharge through an engine nozzle. Means are provided to selectively communicate the downstream chutes with alternate ones of the upstream chutes to cool the downstream mixer portion and reduce the infrared radiation emissions from the nozzle.

Abstract translation: 产生热气流和风扇流的类型的燃气涡轮发动机包括具有上游和下游部分的混合器，所述上游和下游部分限定第一和第二滑槽，用于在通过发动机喷嘴排出之前有效地混合流。 提供装置以选择性地将下游滑槽与替代的上游滑槽通信，以冷却下游混合器部分并减少来自喷嘴的红外辐射。

公开(公告)号：US4989406A

公开(公告)日：1991-02-05

申请号：US291840

申请日：1988-12-29

Applicant: John W. Vdoviak ,  Roy E. Moyer ,  Dennis C. Evans

Inventor： John W. Vdoviak ,  Roy E. Moyer ,  Dennis C. Evans

IPC: F02C7/00 ,  F01D25/16

CPC classification number: F01D25/162 ,  Y02T50/672

Abstract: A turbine assembly includes an annular fairing and strut subassembly which provides mechanical strength to the turbine assembly and support for the rotor aft bearing. A readily demountable annular outlet guide vane assembly is mounted to the aft of the fairing and strut assembly for deswirling the exhaust gasses which exit the turbine assembly. The aft mounting of the outlet guide vanes allows for an axially shorter and lighter turbine engine design which removes greater inlet swirl than prior designs, with equal or less pressure loss.

Abstract translation: 涡轮组件包括环形整流罩和支柱子组件，其向涡轮机组件提供机械强度并为转子后轴承提供支撑。 容易拆卸的环形出口导向叶片组件安装在整流罩和支柱组件的后部，用于旋转离开涡轮组件的废气。 出口导向叶片的后部安装允许轴向更短和更轻的涡轮发动机设计，其消除了比现有设计更大的入口涡流，具有相等或更小的压力损失。

公开(公告)号：US4928480A

公开(公告)日：1990-05-29

申请号：US164371

申请日：1988-03-04

Applicant: Wayne R. Oliver ,  Roy E. Moyer ,  Dennis R. Girardin

Inventor： Wayne R. Oliver ,  Roy E. Moyer ,  Dennis R. Girardin

IPC: F02M35/08 ,  B64D33/02 ,  F02C7/052

CPC classification number: B64D33/02 ,  F02C7/052 ,  B64D2033/0246 ,  B64D2033/0286 ,  Y02T50/671

Abstract: A gas turbine engine utilizes a main and at least one auxiliary particle separator for enhancing the separation of foreign particles from a stream of air entering the engine. The engine includes interior walls which collectively define an engine intake passageway and a compressor inlet passageway in flow communication with the intake passageway so as to provide a primary flowpath for air traveling through the engine to the engine compressor. The main and auxiliary particle separators each include a passageway associated with a corresponding interior wall of the engine. Each separator passageway has an inlet opening to one side of the main flowpath and directed generally upstream of the primary flowpath so as not to appreciably effect the pressure loss through the engine. Furthermore, each separator passageway includes a section adjacent its inlet which is arranged relative to the primary flow path extending thereacross so as to facilitate the acceptance of an amount of air flowing along and adjacent the corresponding wall by the separators and thereby facilitate the acceptance of foreign particles entrained within the amount of air.