中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

53 records (took 0.07 seconds)

    Assembly and method of forming gas turbine engine components
    21.
    发明授权
    Assembly and method of forming gas turbine engine components 有权

    公开(公告)号：US11370016B2

    公开(公告)日：2022-06-28

    申请号：US16420291

    申请日：2019-05-23

    Applicant: United Technologies Corporation

    Inventor： Daniel A. Bales

    IPC: B21D53/78 ,  B23P15/02 ,  F01D5/14 ,  B21J15/02 ,  B21J13/02

    Abstract: A mounting plate for forming a gas turbine engine component according to an example of the present disclosure includes, among other things, a plate body defining an abutment dimensioned to mate with a forming die. The plate body defines at least one internal cooling circuit. The at least one internal cooling circuit includes a passageway having an intermediate portion interconnecting inlet and outlet portions. The intermediate portion is dimensioned to follow a perimeter of the abutment. The intermediate portion includes a plurality of fins extending partially from a first sidewall towards a second sidewall opposed to the first sidewall. A method of forming a gas turbine engine component is also disclosed.

    By-product removal device for laser welding
    29.
    发明授权
    By-product removal device for laser welding 有权

    公开(公告)号：US11267075B2

    公开(公告)日：2022-03-08

    申请号：US16414442

    申请日：2019-05-16

    Applicant: United Technologies Corporation

    Inventor： Daniel A. Bales

    IPC: B23K26/142 ,  B23K26/28 ,  B23K101/00 ,  B23K103/14

    Abstract: A laser welding by-product removal device comprises a housing that includes distal and proximate ends separated along a central axis by a peripheral sidewall. A first plenum circumscribes the peripheral sidewall at the proximate housing end and includes a gas inlet and a first plenum base surface that includes a plurality of gas outlet holes. A second plenum circumscribes the peripheral sidewall between the first plenum and the distal housing end, where the second plenum includes a second plenum base surface, radially inner and outer sidewalls that extend axially distal from the second plenum base surface. The second plenum includes a top surface extending between the radially inner and outer sidewalls, and a by-product outlet in the top surface, where at least one of the second plenum base surface and the radially outer sidewall includes a plurality of by-product inlet holes.

    METHOD OF FORMING GAS TURBINE ENGINE COMPONENTS
    30.
    发明申请
    METHOD OF FORMING GAS TURBINE ENGINE COMPONENTS 有权

    公开(公告)号：US20210060692A1

    公开(公告)日：2021-03-04

    申请号：US16555223

    申请日：2019-08-29

    Applicant: United Technologies Corporation

    Inventor： Daniel A. Bales ,  Thomas DeMichael ,  Robert C. Dolan ,  Francis B. Parisi

    IPC: B23K20/02 ,  B21D11/14 ,  F01D5/18 ,  F01D5/14

    Abstract: A method of forming a gas turbine engine component according to an example of the present disclosure includes, among other things, attaching a cover skin to an airfoil body, the airfoil body and the cover skin cooperating to establish pressure and suction sides of an airfoil, positioning the airfoil between first and second dies of a deforming station, heating the airfoil body to a first predefined temperature threshold between the first and second dies, and moving the first die relative to the second die to hold the airfoil between the first and second dies subsequent to the heating step, and then deforming the airfoil between the first and second dies.

Patent Agency Ranking