中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

25 records (took 0.016 seconds)

    MATERIAL DISPENSING SYSTEMS
    2.
    发明申请
    MATERIAL DISPENSING SYSTEMS 审中-公开

    公开(公告)号：US20200016847A1

    公开(公告)日：2020-01-16

    申请号：US16031452

    申请日：2018-07-10

    Applicant: Bell Helicopter Textron Inc.

    Inventor： David G. Carlson ,  Paul K. Oldroyd ,  George R. Decker ,  Doug K. Wolfe

    IPC: B29C70/38 ,  B29C70/34 ,  B64F5/10 ,  B65H16/00 ,  B65H16/02

    Abstract: A material dispensing system including a first frame and a first application head. The first application head supported by the first frame including a first bias ply assembly comprising a bias ply roll supported on a bias ply dispenser unit, the first bias ply assembly configured to pass bias ply material along a bias path; and a first non-bias ply assembly comprising a non-bias ply roll supported by a non-bias ply dispenser unit, the non-bias ply assembly configured to pass non-bias ply material along a non-bias path; wherein the bias path and the non-bias path are substantially parallel. Another aspect provides a material dispensing system including a first frame and a first application head supported thereby; and a second frame and a second application head supported thereby; wherein the first frame and the second frame move in an X direction during operation. Another aspect includes preparing a composite article.

    Fixed engine and rotating proprotor arrangement for a tiltrotor aircraft
    3.
    发明授权
    Fixed engine and rotating proprotor arrangement for a tiltrotor aircraft 有权
    用于倾斜旋翼飞机的固定发动机和旋转推进器装置

    公开(公告)号：US09174731B2

    公开(公告)日：2015-11-03

    申请号：US13966678

    申请日：2013-08-14

    Applicant: Bell Helicopter Textron Inc.

    Inventor： Brent C. Ross ,  David R. Bockmiller ,  John R. McCullough ,  David G. Carlson

    IPC: B64C29/00

    CPC classification number: B64C29/0033

    Abstract: A tiltrotor aircraft includes a fuselage; a wing member having a first rib, a second rib, a first spar, second spar; and an upper wing skin; an engine disposed at a fixed location relative to the wing member; and a proprotor having a spindle gearbox, rotor mast, and a plurality of rotor blades drivable in rotation about the rotor mast, the spindle gearbox being rotatable about a conversion axis. The spindle gearbox is located above the upper wing skin of the wing member.

    Abstract translation: 一架俯仰式飞机包括机身; 翼构件，具有第一肋，第二肋，第一翼梁，第二翼梁; 和上翼皮; 设置在相对于翼构件的固定位置的发动机; 以及具有主轴齿轮箱，转子桅杆和可围绕转子桅杆旋转驱动的多个转子叶片的推进器，所述主轴齿轮箱可围绕转换轴线旋转。 主轴齿轮箱位于机翼构件的上翼面上方。

    ASSEMBLY FIXTURE WITH ANISOTROPIC THERMAL PROPERTIES
    9.
    发明申请
    ASSEMBLY FIXTURE WITH ANISOTROPIC THERMAL PROPERTIES 审中-公开

    公开(公告)号：US20200346382A1

    公开(公告)日：2020-11-05

    申请号：US16814622

    申请日：2020-03-10

    Applicant: Bell Helicopter Textron Inc.

    Inventor： David G. Carlson ,  Douglas K. Wolfe ,  James A. Cordell

    IPC: B29C48/05 ,  B29C63/00 ,  B64C11/16 ,  B32B27/02 ,  B64C3/00 ,  B29C70/52 ,  B29C64/118 ,  B29C33/38

    Abstract: In one embodiment, an assembly fixture may include a base structure including a plurality of strands of a fiber-reinforced thermoplastic material comprising a thermoplastic embedded with a plurality of reinforcement fibers, wherein the plurality of reinforcement fibers is aligned within each strand of the plurality of strands, and wherein the base structure further comprises an anisotropic thermal expansion property based on an orientation of the plurality of reinforcement fibers within the base structure, The assembly fixture may further include a plurality of fastening structures coupled to the base structure, wherein the plurality of fastening structures is configured to fasten a plurality of components of a composite structure for assembly using a heated bonding process.

Patent Agency Ranking