公开(公告)号：US20140271227A1

公开(公告)日：2014-09-18

申请号：US14158014

申请日：2014-01-17

Applicant: ROLLS-ROYCE PLC

Inventor： Steven Aleksy RADOMSKI ,  Clive GRAFTON-REED ,  Ian CROWSTON ,  Andrea Lelio MAURIZIO

IPC: F01D5/18

CPC classification number: F01D5/18 ,  B23P15/04 ,  F01D5/147 ,  Y02T50/672 ,  Y10T29/49339

Abstract: A method of manufacturing a hollow aerofoil component for a gas turbine engine includes using a capping panel to cover a pocket in a pocketed aerofoil body. During manufacture, the outer surface of the capping panel is located relative to the pocketed aerofoil body. This ensures that the outer surface of the capping panel is located as accurately as possible. This means that the capping panel can be made to be as thin as possible, which in turn reduces weight and material wastage. Once the capping panel has been located in position, it may be welded to the aerofoil body in order to produce the hollow aerofoil component.

Abstract translation: 一种用于燃气涡轮发动机的空心翼型零件的制造方法包括使用盖板覆盖袋装机翼中的口袋。 在制造过程中，封盖板的外表面相对于袋装机翼本体定位。 这确保了封盖板的外表面尽可能准确地定位。 这意味着封盖板可以制成尽可能薄，这又减轻了重量和材料浪费。 一旦盖板已经定位就位，它可以被焊接到机翼主体上，以便产生中空翼型部件。

公开(公告)号：US20140076864A1

公开(公告)日：2014-03-20

申请号：US13967750

申请日：2013-08-15

Applicant: ROLLS-ROYCE PLC

Inventor： James KELL ,  Clive GRAFTON-REED ,  Dragos AXINTE

IPC: B23K26/03 ,  B23K26/20 ,  B23K26/34 ,  G02B23/24

CPC classification number: B23K26/342 ,  B08B7/0042 ,  B23K26/0006 ,  B23K26/0096 ,  B23K26/064 ,  B23K26/08 ,  B23K26/211 ,  B23K26/32 ,  B23K26/352 ,  B23K35/0244 ,  B23K35/3033 ,  B23K35/3046 ,  B23K35/3053 ,  B23K35/365 ,  B23K2101/001 ,  B23K2101/34 ,  B23K2103/02 ,  B23K2103/08 ,  B23K2103/26 ,  B23P6/002 ,  G02B23/2423 ,  G02B26/101

Abstract: A boroscope includes a working head having first and second ends. A first optical fibre extends through the boroscope to a position between the first and second ends. A second optical fibre extends through the boroscope to the second end of the working head. A laser optical fibre extends through the boroscope. At least one lens is arranged between the first end and the second end of the working head and a mirror is gimballed to the second end of the working head. The laser optical fibre directs laser light transmitted through the laser optical fibre onto the lens and then onto the mirror. A first LED is arranged at a position between the first end and the second end of the working head and a second LED is arranged at the second end of the working head and an actuator devices adjust the position of the mirror.

Abstract translation: 透视镜包括具有第一端和第二端的工作头。 第一光纤延伸穿过硼砂镜到第一和第二端之间的位置。 第二根光纤延伸穿过工具头的第二端。 激光光纤延伸穿过硼砂镜。 在工作头的第一端和第二端之间布置至少一个透镜，并且镜子被球形到工作头的第二端。 激光光纤将通过激光光纤传输的激光引导到透镜上，然后将其引导到反射镜上。 第一LED布置在工作头的第一端和第二端之间的位置，并且第二LED布置在工作头的第二端，并且致动器装置调节镜的位置。