-
公开(公告)号：US20140165574A1
公开(公告)日：2014-06-19
申请号：US14177503
申请日：2014-02-11
Applicant: AIRCELLE
Inventor： Philippe BIENVENU , Helene Malot
IPC: F02K1/04
CPC classification number: F02K1/04 , F02K1/80 , F02K1/82 , F05D2230/232 , F05D2250/283 , F05D2260/30 , Y02T50/671
Abstract: An exhaust plug for an aircraft turbojet engine is provided. The exhaust plug includes a front part being attached to a rear part, and the front and rear parts each have an outer skin. In particular, the front part and the rear part are connected by a connecting flange which is shared by the front and rear parts. The outer skins of the front and rear parts are placed side by side on the connecting flange.
Abstract translation: 提供了一种用于飞机涡轮喷气发动机的排气塞。 排气塞包括附接到后部的前部，并且前后部各自具有外皮。 特别地，前部和后部通过由前部和后部共享的连接凸缘连接。 前部和后部的外表面并排放置在连接法兰上。
-
公开(公告)号：US09789556B2
公开(公告)日：2017-10-17
申请号：US14883994
申请日：2015-10-15
Applicant: AIRCELLE
Inventor： Philippe Bienvenu , Helene Malot , Francisco Caneque
IPC: B23K31/02 , B23K3/08 , B21D26/033 , B23K1/008 , F02K1/82 , F02K1/80 , B23K1/00 , B23K101/00
CPC classification number: B23K3/087 , B21D26/033 , B23K1/0014 , B23K1/0018 , B23K1/008 , B23K2101/001 , F02K1/80 , F02K1/827 , F05D2230/23 , F05D2230/237 , F05D2250/283 , F05D2300/502
Abstract: A method for assembling a set including an inner wall, a shrouded outer wall and an intermediate element, each presenting substantially circular sections, the shrouded outer wall presenting a shape substantially complementary to a shape of outer and inner surfaces of the intermediate element, and whose inner surface covers the outer surface of the intermediate element. In particular, the method includes a step of placing a brazing sheet, whose melting temperature is lower than melting temperatures of other elements of the set, over an assembly surface in contact with another assembly surface, and a step of heating, by a furnace, a set including the outer or inner walls and the intermediate element between which is interposed a brazing sheet so as to fix the outer or inner wall by brazing on the intermediate element.
-
公开(公告)号：US09051899B2
公开(公告)日：2015-06-09
申请号：US14177494
申请日：2014-02-11
Applicant: AIRCELLE
Inventor： Helene Malot , Philippe Bienvenu
IPC: G10K11/172 , F02K1/82 , F02K1/04 , F02K1/44 , F02K1/80
CPC classification number: F02K1/827 , F02K1/04 , F02K1/44 , F02K1/80 , F05D2230/232 , F05D2250/283 , F05D2260/30 , Y02T50/671
Abstract: An exhaust cone for an aircraft turbojet engine includes a front part which has a front end and a rear end. The front end is equipped with a front connecting flange connecting to an outlet of a turbojet engine and the rear end is equipped with a rear connecting flange connecting to a rear part of the exhaust cone. In particular, the front part is further equipped with a sound attenuation structure including an outer skin, and the outer skin overlaps the front connecting flange and the rear connecting flange.
Abstract translation: 用于飞机涡轮喷气发动机的排气锥体包括具有前端和后端的前部。 前端配备有连接到涡轮喷气发动机的出口的前连接凸缘，并且后端配备有连接到排气锥的后部的后连接凸缘。 特别地，前部还配备有包括外皮的声音衰减结构，并且外表皮与前连接凸缘和后连接凸缘重叠。
-
公开(公告)号：US20140158458A1
公开(公告)日：2014-06-12
申请号：US14177494
申请日：2014-02-11
Applicant: AIRCELLE
Inventor： Helene Malot , Philippe Bienvenu
IPC: F02K1/82
CPC classification number: F02K1/827 , F02K1/04 , F02K1/44 , F02K1/80 , F05D2230/232 , F05D2250/283 , F05D2260/30 , Y02T50/671
Abstract: An exhaust cone for an aircraft turbojet engine includes a front part which has a front end and a rear end. The front end is equipped with a front connecting flange connecting to an outlet of a turbojet engine and the rear end is equipped with a rear connecting flange connecting to a rear part of the exhaust cone. In particular, the front part is further equipped with a sound attenuation structure including an outer skin, and the outer skin overlaps the front connecting flange and the rear connecting flange.
Abstract translation: 用于飞机涡轮喷气发动机的排气锥体包括具有前端和后端的前部。 前端配备有连接到涡轮喷气发动机的出口的前连接凸缘，并且后端配备有连接到排气锥的后部的后连接凸缘。 特别地，前部还配备有包括外皮的声音衰减结构，并且外表皮与前连接凸缘和后连接凸缘重叠。
-
-
-
Search Results
4
records
(took 0.008 seconds)
