-
公开(公告)号：US11014857B2
公开(公告)日：2021-05-25
申请号：US15709835
申请日：2017-09-20
IPC分类号： C04B35/80 , B32B18/00 , C04B35/571 , C04B35/628 , C04B35/645 , F01D5/28 , F01D5/30
摘要： Composite components having structurally reinforced contact interfaces are provided. In one example, the component can include an inner laminate formed of one or more inner plies having reinforcement fibers oriented along a reference direction within a matrix material. The component can also include an interface laminated positioned on the inner laminate along at least a portion of a contact surface of the component. The interface laminate is formed of one or more interface plies having reinforcement fibers oriented along a direction offset from the reference direction within a matrix material. Methods for fabricating such components are also provided.
-
公开(公告)号：US11014205B2
公开(公告)日：2021-05-25
申请号：US15730961
申请日：2017-10-12
摘要： Embodiments of the present disclosure relate to the installation or removal of turbine blades at a turbine blade base thereof. An apparatus according to the present disclosure can include: an operative head configured to engage an axial sidewall of a turbine blade base; and a mount removably coupled to a portion of a turbomachine assembly by a coupler, wherein the operative head is slidably coupled to the mount such that the operative selectively engages the axial sidewall of the turbine blade base, and wherein the operative head is shaped to impart an axial and a circumferential force against the turbine blade base.
-
公开(公告)号：US20210138568A1
公开(公告)日：2021-05-13
申请号：US16965428
申请日：2019-01-25
申请人： MTU Aero Engines AG
摘要： The invention relates to a work station for electrochemically machining a workpiece, having a number of recesses, including a base structure; a module which is fastened to the base structure and is configured to electrochemically machine the workpiece. A workpiece holder is fastened to the base structure. The workpiece holder is movable relative to the base structure along a feed axis which is parallel to the axis of rotation of the module. The module includes an electrode carrier arrangement, which is coupled to the module base body so the electrode carrier arrangement can be rotated together with the module base body about the axis of rotation of the module. The electrode carrier arrangement has a carrier frame and an electrode frame, where at least one electrode is detachably fastened to the electrode frame.
-
公开(公告)号：US11000929B2
公开(公告)日：2021-05-11
申请号：US16330150
申请日：2017-08-08
发明人： Rick Giesel
摘要： Provided is a machining device for machining a rotor arranged in a turbine housing which includes two parts, thereby forming a joint, in situ while the upper housing half is removed. The machining device includes a main part that releasably secures the main part to the lower housing half in the region of the joint, at least one tool holder for receiving at least one machining tool which is secured on the main part directly or indirectly so as to be alignable relative to the main part, multiple telescopic stabilizing elements which can be locked into different longitudinal settings preferably in a continuous manner.
-
公开(公告)号：US10989112B2
公开(公告)日：2021-04-27
申请号：US16411341
申请日：2019-05-14
申请人： ROLLS-ROYCE plc
摘要： A highly efficient gas turbine engine is provided. The fan of the gas turbine engine is driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.
-
公开(公告)号：US10968745B2
公开(公告)日：2021-04-06
申请号：US16506991
申请日：2019-07-09
发明人： Victor Shemyatovskiy
摘要： A turbine, a gas turbine, and a method of disassembling turbine blades, capable of ensuring stable sealing performance as well as facilitating disassembly of turbine blades are provided. The turbine may include a rotor disk including a plurality of slots formed therein, a plurality of turbine blades spaced apart from each other by a predetermined distance in a circumferential direction of the rotor disk on an outer peripheral surface, each of the turbine blades being inserted into an associated one of the slots, and a retainer sealing a cooling passage defined between the rotor disk and the turbine blade, wherein the turbine blade includes an airfoil-shaped blade part, a root part inserted into the rotor disk, and a platform part located between the blade part and the root part, and the root part includes a blade hook protruding therefrom to support the retainer.
-
公开(公告)号：US10954795B2
公开(公告)日：2021-03-23
申请号：US16324010
申请日：2017-07-21
发明人： Benoît Guillaume Silet , Youki Olivier Ito-Lardeau , Gilles Marcel Jeannin , Baptiste Marie Aubin Pierre Jouy , Bertrand Guillaume Robin Pellaton , Josselin Luc Florent Sicard
摘要： A turbo engine rotor disc that has a rotation axis and includes, at the periphery thereof, a plurality of slots regularly distributed around the rotation axis, wherein at least one slot of the plurality of slots has a base that has a plurality of plates arranged in staggered rows and protruding from the base, each plate extending mainly along a direction perpendicular to a radial direction.
-
公开(公告)号：US10953526B2
公开(公告)日：2021-03-23
申请号：US15746971
申请日：2016-06-30
发明人： Kai Mielich
摘要： A method is provided having the following steps: a) providing a drive-out device which has a drive-out punch that is actuated via a hydraulic cylinder; b) positioning the drive-out device between two adjacent wheel discs of the rotor such that a longitudinal axis of the drive-out punch is flush with the receiving groove of the blade to be driven out; c) adjusting a maximum pressure which can be applied to the hydraulic cylinder; d) extending the drive-out punch such that the drive-out punch presses against the blade root of the blade to be driven out with increasing pressure; e) reducing the pressure as soon as the pressure has reached the maximum pressure; and f) cyclically repeating the steps d) and e) until the blade has been removed from the receiving groove. A drive-out device is further provided.
-
公开(公告)号：US10941665B2
公开(公告)日：2021-03-09
申请号：US15971249
申请日：2018-05-04
发明人： Matthew Mark Weaver
摘要： Rotor assemblies and methods for manufacturing airfoils for rotor assemblies are provided. For example, a rotor assembly comprises a rotary structure extending circumferentially about an axial centerline of a gas turbine engine and an airfoil having a root and a tip. The root is coupled to the rotary structure and has a bulbous shape. The airfoil is formed from a plurality of composite plies, a portion of which defines at the root first and second end surfaces, which are in contact with the rotary structure and together define a chisel-shaped end of the root. In another embodiment, a rotor assembly comprises an outer rotor extending circumferentially about an axial centerline of a gas turbine engine and a composite outer rotor blade having a root and a tip. The blade root is coupled to the outer rotor and extends inward along a radial direction toward the axial centerline.
-
公开(公告)号：US20210062661A1
公开(公告)日：2021-03-04
申请号：US17004592
申请日：2020-08-27
发明人： Eric Stephen Loos
摘要： A structure and a method of constructing a root joint and blade retention mechanism of a composite airfoil of a propulsor blade is presented. The retention assembly includes an inner sleeve configured to retain a root area of the composite propulsor blade. The inner sleeve is fixedly attached to an inner surface of the root area by a resin transfer molding process. An outer sleeve is bonded to an outer surface of the composite propulsor blade after the completion of the resin transfer molding process. At least one bearing assembly is disposed within an annular groove of the outer sleeve. The bearing assembly rotatably couples the propulsor blade and the retention assembly to a hub assembly.
-
-
-
-
-
-
-
-
-
搜索结果
3880 条记录 (耗时 0.035 秒)
