公开(公告)号：WO2014028078A3

公开(公告)日：2014-04-10

申请号：PCT/US2013037686

申请日：2013-04-23

Applicant: UNITED TECHNOLOGIES CORP

Inventor： GILSON JONATHAN ,  MAY MOLLY M ,  WELCH DAVID A ,  SAWYERS-ABBOTT NIGEL DAVID

IPC: F02C7/045 ,  F02K1/34

CPC classification number: F02C3/04 ,  F02C3/107 ,  F02C7/045 ,  F02K3/06 ,  F04D29/545 ,  F04D29/644 ,  F04D29/664

Abstract: A nacelle structure for a gas turbine engine assembly includes a fan case, and inlet, and a noise attenuation device. The fan case is configured to be disposed about a fan section of the gas turbine engine, which fan section has a diameter D. The inlet is attached to the fan case and extends axially forward of the fan case. A hilite of the inlet is spaced a distance L from a region in which the fan section is configured to be disposed. A ratio L/D is less than about 0.6. The noise attenuation structure covers a portion of an inner surface of the fan case and the inlet.

Abstract translation: 用于燃气涡轮发动机组件的机舱结构包括风扇壳体和入口以及噪声衰减装置。 风扇外壳被配置为围绕燃气涡轮发动机的风扇部分设置，该风扇部分具有直径D.入口连接到风扇外壳并且在风扇外壳的轴向前方延伸。 入口的hilite与配置有风扇部分的区域间隔距离L. 比值L / D小于约0.6。 噪声衰减结构覆盖风扇外壳的内表面和入口的一部分。

公开(公告)号：WO2014197053A3

公开(公告)日：2015-02-19

申请号：PCT/US2014024618

申请日：2014-03-12

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ROBERTSON JR THOMAS J ,  COSTA MARK W ,  WELCH DAVID A

IPC: F02C7/045 ,  F01D25/08 ,  F02C7/24

CPC classification number: F02C7/045 ,  B64D33/02 ,  B64D2033/0206 ,  B64D2033/0286 ,  F01D11/125 ,  F05D2250/283 ,  F05D2300/173 ,  F05D2300/433 ,  F05D2300/44 ,  F05D2300/5021 ,  Y02T50/671

Abstract: A cartridge for a fan case of a gas turbine engine includes an inlet acoustic liner section integrated with a thermally conforming liner section.

Abstract translation: 用于燃气涡轮发动机的风扇壳体的盒包括与热适应衬套部分一体化的入口声学衬垫部分。