公开(公告)号：US20100047077A1

公开(公告)日：2010-02-25

申请号：US11966165

申请日：2007-12-28

Applicant: James Lloyd Daniels

Inventor： James Lloyd Daniels

IPC: F02C7/00

CPC classification number: F02K3/00 ,  B64F1/005 ,  B64F5/50 ,  F01D25/285 ,  F02C7/00 ,  F02C7/20 ,  F05D2240/55 ,  Y02T50/672

Abstract: A fairing kit for a gas turbine engine, where the engine has a core gas turbine engine, a fan rotor, and a plurality of external fan blades attached to the fan rotor and powered by the core gas turbine engine. The core gas turbine engine has an annular splitter for directing a portion of incoming airflow into the core gas turbine engine. The fairing kit comprises: a) a fairing; b) a plurality of fasteners for securing the fairing to the core gas turbine engine; and c) a conformable seal for sealing mating surfaces of the fairing and the core gas turbine engine.

Abstract translation: 一种用于燃气涡轮发动机的整流罩，其中发动机具有核心燃气涡轮发动机，风扇转子和附接到风扇转子并由核心燃气涡轮发动机供电的多个外部风扇叶片。 核心燃气涡轮发动机具有用于将一部分进入的气流引导到核心燃气涡轮发动机中的环形分配器。 整流罩包括：a）整流罩; b）用于将整流罩固定到核心燃气涡轮发动机的多个紧固件; 以及c）用于密封整流罩和核心燃气涡轮发动机的配合表面的适形密封件。

公开(公告)号：US20100043228A1

公开(公告)日：2010-02-25

申请号：US11966180

申请日：2007-12-28

Applicant: James Lloyd Daniels

Inventor： James Lloyd Daniels

IPC: B23P11/00

CPC classification number: F01D25/285 ,  B64F1/005 ,  B64F5/50 ,  F02C7/00 ,  F02C7/20 ,  F02K3/00 ,  F05D2240/55 ,  Y02T50/672 ,  Y10T29/49318

Abstract: A method for preparing a gas turbine engine for a ferry flight, where the engine has a core gas turbine engine, a spinner, and a plurality of external fan blades powered by the core gas turbine engine. The core gas turbine engine has an annular splitter for directing a portion of incoming airflow into the core gas turbine engine. The method comprises the steps of: a) removing the spinner; b) removing the fan blades; and c) securing a fairing in sealing engagement with the core gas turbine engine.

Abstract translation: 一种制备用于渡轮飞行的燃气涡轮发动机的方法，其中发动机具有核心燃气涡轮发动机，旋转器和由核心燃气涡轮发动机供电的多个外部风扇叶片。 核心燃气涡轮发动机具有用于将一部分进入的气流引导到核心燃气涡轮发动机中的环形分配器。 该方法包括以下步骤：a）去除旋转器; b）拆下风扇叶片; 以及c）确保整流罩与所述核心燃气涡轮发动机的密封接合。