公开(公告)号：US20190176274A1

公开(公告)日：2019-06-13

申请号：US16324059

申请日：2017-08-08

Applicant: Impcross Ltd

Inventor： Terry MAGRANE

IPC: B23P15/00 ,  B23P13/02 ,  G01B5/12 ,  G01B5/06

Abstract: A method of manufacturing a tubular component including rough machining the exterior surface of a solid billet 1 to reduce the size thereof and form two flanges. An axial blind bore 6 is then machined in the billet 1, after which a probing operation is carried out on the interior surface of the bore 6 in order to check the concentricity. A straightening operation is then performed on the billet in order to reverse any curvature along the longitudinal axis. A further machining operation is then performed on the outside to reduce the wall thickness of the bore before measuring the wall thickness of the bore 6 around the circumference of the billet 1 at least at two different axial positions. The billet 1 is then checked again and a final machining operation is then performed in order to form any ports and upstands which are required.

公开(公告)号：US10953500B2

公开(公告)日：2021-03-23

申请号：US16324059

申请日：2017-08-08

Applicant: Impcross Ltd

Inventor： Terry Magrane

IPC: B23P15/00 ,  B23P13/02 ,  G01B5/12 ,  G01B5/06 ,  F16J10/02 ,  F15B15/14

Abstract: A method of manufacturing a tubular component including rough machining the exterior surface of a solid billet 1 to reduce the size thereof and form two flanges. An axial blind bore 6 is then machined in the billet 1, after which a probing operation is carried out on the interior surface of the bore 6 in order to check the concentricity. A straightening operation is then performed on the billet in order to reverse any curvature along the longitudinal axis. A further machining operation is then performed on the outside to reduce the wall thickness of the bore before measuring the wall thickness of the bore 6 around the circumference of the billet 1 at least at two different axial positions. The billet 1 is then checked again and a final machining operation is then performed in order to form any ports and upstands which are required.

公开(公告)号：US12065263B2

公开(公告)日：2024-08-20

申请号：US17267680

申请日：2019-07-16

Applicant: IMPCROSS LTD

Inventor： Martin Phelps

IPC: B64D45/02 ,  H01R13/648 ,  H01R13/74 ,  H02G13/00

CPC classification number: B64D45/02 ,  H01R13/6485 ,  H01R13/746 ,  H02G13/80 ,  H01R2201/26

Abstract: A charge dissipation plate for aircraft electronic systems having a metal plate with machined through openings. A collar is integrally formed with each through opening. The collar extends upwardly from the plane of the plate and includes a threaded outer surface for receiving an electronic connector.

公开(公告)号：US20210323693A1

公开(公告)日：2021-10-21

申请号：US17267680

申请日：2019-07-16

Applicant: IMPCROSS LTD

Inventor： Martin PHELPS

IPC: B64D45/02 ,  H01R13/648 ,  H01R13/74 ,  H02G13/00

Abstract: A charge dissipation plate for aircraft electronic systems comprises a machined metal plate 1 have at least one through opening 2a, 2b, 2c machined therein and an integrally formed collar 3a, 3b, 3c associated with and extending around the or each opening 2a, 2b, 2c. The or each collar 3a, 3b, 3c upstands from the plane of the plate 1 and has a threaded outer surface 4a, 4b, 4c. The or each collar 3a, 3b, 3c forms a housing for receiving an electronic connector therein, the threaded outer surface 4a, 4b, 4c, in use, being engagable by a mating threaded connector for connecting with the electronic connector mounted in the collar.