Patents Assigned to Howmet Aerospace Inc.
  • Patent number: 11959504
    Abstract: Self-forming thread blind fasteners and methods for fastening are provided. The self-forming thread blind fastener comprises a sleeve and a pin. The sleeve comprises a first sleeve end, a second sleeve end, an elongate portion, and an inner wall defining a bore. The pin is configured to be at least partially received by the bore. The pin comprises a first pin end, a second pin end, a pin head portion, an at least partially threaded portion, a shank intermediate, and a driving portion. The at least partially threaded portion is configured to form threads on at least a portion of the inner wall of the sleeve. The driving portion is configured to receive a torque to rotate the pin within the sleeve and thereby axially compress and deform the sleeve and form the threads on the at least a portion of the inner wall of the sleeve.
    Type: Grant
    Filed: July 16, 2021
    Date of Patent: April 16, 2024
    Assignee: HOWMET AEROSPACE INC.
    Inventor: Thomas Brennetot
  • Patent number: 11885358
    Abstract: The present disclosure relates to a blind fastener and a method of installation thereof. The blind fastener comprises a sleeve and a mandrel. The sleeve comprises a first sleeve end, a second sleeve end, and a cavity extending from the first sleeve end to the second sleeve end. The mandrel is configured to be at least partially received by the cavity of the sleeve. The mandrel comprises a first mandrel end disposed adjacent to the first sleeve end and comprising an enlarged portion having a diameter greater than a diameter of the cavity, a second mandrel end comprising a pull region, and a shank region extending intermediate the first mandrel end and the second mandrel end. The pull region comprises an axial length no greater than four times a diameter of the shank region and is configured to be engaged by an installation tool.
    Type: Grant
    Filed: February 7, 2019
    Date of Patent: January 30, 2024
    Assignee: HOWMET AEROSPACE INC.
    Inventors: Robert B. Wilcox, James Thomas Smith, Troy Don Pierce
  • Patent number: 11841041
    Abstract: Fastening collars, multi-piece fastening systems, and methods of fastening are provided. The fastening collar comprises a first end, a second end, and an elongate portion intermediate the first end and the second end and defining a longitudinal axis of the fastening collar. The elongate portion comprises a first region adjacent the first end, a second region intermediate the first region and the second end, and a cavity. The first region comprises a first diameter and is configured to be received by a bore of a structure. The second region comprises a second diameter greater than the first diameter. The cavity extends through the elongate portion and is configured to receive at least a portion of a shank of the multi-piece fastening system. The elongate portion is configured to at least partially deform onto the shank responsive to forcible contact between the second region and an installation tool.
    Type: Grant
    Filed: March 23, 2020
    Date of Patent: December 12, 2023
    Assignee: HOWMET AEROSPACE INC.
    Inventors: Robert B. Wilcox, Justin Branch, Ryan J. White
  • Patent number: 11801567
    Abstract: A collet assembly including an actuator and a collet connected to the actuator. The collet assembly is adapted to be installed on a welding electrode holder having an electrode. The collet is moveable by the actuator from an advanced position, in which the collet is adapted to grip a fastener such as a welding rivet, and a retracted position, in which at least a portion of the collet is retracted into the actuator to enable the electrode to engage the fastener for welding to a work piece, and the collet is adapted to release the fastener.
    Type: Grant
    Filed: February 13, 2020
    Date of Patent: October 31, 2023
    Assignee: HOWMET AEROSPACE INC.
    Inventors: Robert Wilcox, Thomas Kingsbury, Dan Peter Vanderzwet, Simon Maurice Britton, Donald J. Spinella, Daniel Bergstrom, Eric Jean Michaud, Larry Frank Koscielski, Gino Norman Iasella
  • Patent number: 11802581
    Abstract: Methods of fastening are provided. A method comprises contacting a fastener with a first layer of an assembly at a first location. The assembly comprises the first layer, a third layer, and a second layer positioned intermediate the first layer and the third layer. The first layer, the third layer, and the fastener are electrically conductive. The second layer defines a gap and the first location is in communication with the gap. Electrical communication is formed between the assembly and the fastener. The first layer is fastened to the third layer through the gap in the second layer with the fastener. The fastening comprises resistance welding the fastener to the third layer.
    Type: Grant
    Filed: March 15, 2021
    Date of Patent: October 31, 2023
    Assignee: HOWMET AEROSPACE INC.
    Inventors: Anthony J. Fedusa, Donald J. Spinella
  • Patent number: 11767871
    Abstract: A lockbolt collar having a shank including a first end, a second end opposite the first end, a through-bore extending from the first end to the second end, an inner wall extending from the first end to the second end, and a tab extending radially and outwardly from the inner wall, the tab including a top surface having an arcuate shape, the arcuate shape of the tab being sized and shaped to mate with at least one lock groove of a threaded portion of a pin member.
    Type: Grant
    Filed: January 6, 2020
    Date of Patent: September 26, 2023
    Assignee: HOWMET AEROSPACE INC.
    Inventor: Stanley E. Wojciechowski
  • Patent number: 11738595
    Abstract: Vehicle wheels, methods of making vehicle wheels, and dual wheel assemblies are provided. The vehicle wheel includes a generally cylindrical first region and a second region extending radially inwardly from the first region. The second region includes a first surface, a second surface, an opening, and a hub surface. A distance from the first surface to the second surface defines a thickness. The opening is configured to receive at least a portion of a hub of the vehicle axle. The hub surface is adjacent to and surrounds the opening and extends from the first surface to the second surface. The hub surface includes a generally flat portion and a relief portion adjacent to at least one of the first surface and the second surface. The relief portion surrounds the opening and extends along the hub surface for a distance of at least 25% of the thickness.
    Type: Grant
    Filed: February 26, 2020
    Date of Patent: August 29, 2023
    Assignee: HOWMET AEROSPACE INC.
    Inventor: Spencer Wallace
  • Patent number: 11684992
    Abstract: Resistance spot rivet welding systems, subsystems, and methods of use thereof are provided.
    Type: Grant
    Filed: December 13, 2018
    Date of Patent: June 27, 2023
    Assignees: HOWMET AEROSPACE INC., CENTERLINE (WINDSOR) LIMITED
    Inventors: Daniel Peter Vanderzwet, Simon Maurice Britton, Larry Frank Koscielski, Eric Jean Michaud, David Mario Simone, Stuart Cameron Cosgrave, Kyle Alexander Wasyliniuk, Donald J. Spinella, Gino N. Iasella, Daniel Bergstrom, Robert B. Wilcox, Thomas R. Kingsbury, Graham Scott Musgrove
  • Patent number: 11628507
    Abstract: Fastening collar removal apparatus, methods of making fastening collar removal apparatus, and methods of removing a fastening collar secured to a fastener are provided. A fastening collar removal apparatus includes a collet including a first section including a substantially cylindrical shape and a second section operatively coupled to the first section. The second section includes a collet cavity extending therein. The collet cavity is configured to receive at least a portion of a collar. The second section includes at least two fingers formed by at least two axial channels in the second section. At least one of the at least two fingers includes a blade extending inwardly relative to a longitudinal axis of the collet. In an open configuration of the collet, each of the at least two fingers includes an outward taper relative to a longitudinal axis of the collet.
    Type: Grant
    Filed: February 28, 2019
    Date of Patent: April 18, 2023
    Assignee: HOWMET AEROSPACE INC.
    Inventor: Thomas R. Kingsbury
  • Patent number: 11608551
    Abstract: New aluminum alloys are disclosed and generally include 0.6-1.4 wt. % Si, 0.25-0.90 wt. % Mg, wherein the ratio of wt. % Si to wt. % Mg is from 1.05:1 to 5.0:1, 0.25-2.0 wt. % Cu, 0.10-3.5 wt. % Zn, 0.01-1.0 wt. % Fe, up to 0.8 wt. % Mn, up to 0.25 wt. % Cr, up to 0.20 wt. % Zr, up to 0.20 wt. % V, and up to 0.15 wt. % Ti, wherein the total of Fe+Mn+Cr+Zr+V+Ti is not greater than 2.0 wt. %, the balance being aluminum and impurities. The new aluminum alloys may include Q phase precipitates. In some embodiments, the solvus temperature of the Q phase precipitates is not greater than 950° F.
    Type: Grant
    Filed: April 14, 2020
    Date of Patent: March 21, 2023
    Assignee: Howmet Aerospace Inc.
    Inventors: Jen C. Lin, Gabriele F. Ciccola, Santosh Prasad, Wei Wen, Raymond J. Kilmer
  • Patent number: 11554443
    Abstract: The present disclosure is directed towards different embodiments of additively manufacturing and smoothing an AM preform to configure an AM preform for downstream processing (working, forging, and the like).
    Type: Grant
    Filed: January 13, 2017
    Date of Patent: January 17, 2023
    Assignee: Howmet Aerospace Inc.
    Inventors: Gen Satoh, Daniel M. Myers, Brandon H. Bodily
  • Patent number: 11541449
    Abstract: Rivet dispenser reloading systems and methods of use thereof are provided. A non-limiting embodiment of a rivet dispenser reloading system comprises a receiving member defining a channel therein, and a first gate. The rivet receiving member comprises a first port and a second port that communicate with the channel. The first port is configured to receive rivets. The second port is configured to selectively engage with a rivet dispenser and introduce rivets to the rivet dispenser. The channel extends between the first port and the second port and is configured to transport rivets from the first port to the second port in a series arrangement and in a preselected orientation. The first gate is in communication with the second port and is selectively positionable between a first configuration inhibiting movement of rivets through the second port, and a second configuration enabling movement of rivets through the second port.
    Type: Grant
    Filed: December 13, 2019
    Date of Patent: January 3, 2023
    Assignees: HOWMET AEROSPACE INC., CENTERLINE (WINDSOR) LIMITED
    Inventors: Stuart Cameron Cosgrave, Kyle Alexander Wasyliniuk, Donald J. Spinella, Daniel Bergstrom, Gino N. Iasella
  • Patent number: 11529826
    Abstract: A wheel cover assembly for a vehicle wheel may include a wheel rib that is attachable to a rim inner surface of a wheel rim of the vehicle wheel, a cover body having a cover body outer surface, a cover body inner surface, and a cover body outer edge having an outer diameter that is greater than an inner diameter of the wheel rib and less than an inner diameter of an open end flange of the wheel rim. A cover mounting mechanism operatively connected to the cover body has a cover locking position wherein the cover mounting mechanism engages the wheel rib to retain the wheel rib between the cover mounting mechanism and the cover body and secure the wheel cover assembly to the vehicle wheel when the wheel rib is attached to the rim inner surface.
    Type: Grant
    Filed: September 6, 2019
    Date of Patent: December 20, 2022
    Assignee: HOWMET AEROSPACE INC.
    Inventors: Spencer Wallace, Matt Brest
  • Patent number: 11519452
    Abstract: A fastener including a bolt having an elongated shank having a first end, a second end opposite the first end, and a threaded portion having an external bolt thread, the bolt thread including a bolt pitch. The fastener includes a nut having a first end, a second end opposite the first end of the nut, and an internal nut thread extending between the first and second ends of the nut and adapted to engage threadedly the bolt thread of the bolt. The nut thread includes a nut pitch and a hardness that changes gradationally between the first and second ends of the nut. The bolt pitch of the bolt thread of the bolt is mismatched with the nut pitch of the nut thread of the nut.
    Type: Grant
    Filed: May 9, 2019
    Date of Patent: December 6, 2022
    Assignee: HOWMET AEROSPACE INC.
    Inventors: Donald C. Busby, Richard Franklin, James L. Wollard
  • Patent number: 11473605
    Abstract: A fastener including a pin member having a shank portion, a threaded portion having a thread, a lock portion having at least one lock groove, and a pull portion located having at least one pull groove. The threaded portion is adapted to be engaged threadedly with a threaded hole of a workpiece to install the pin member therein. The fastener includes a swage collar adapted to be installed into the at least one lock groove of the lock portion to secure a plurality of workpieces. The pull portion is adapted to break off when the fastener is installed.
    Type: Grant
    Filed: January 30, 2020
    Date of Patent: October 18, 2022
    Assignee: HOWMET AEROSPACE INC.
    Inventors: Thomas Brennetot, Arnaud Brunet, Christophe Coulon
  • Patent number: 11471932
    Abstract: Rivet dispenser systems and methods of use thereof are provided. In a non-limiting embodiment, the rivet dispenser system comprises a rivet receiving member defining a channel therein, and a seat member. The channel includes a curved region. The rivet receiving member comprises a first port and a second port. The first port communicates with the channel and is configured to receive rivets. The second port communicates with the channel and is configured to dispense rivets. The channel extends between the first port and the second port and is configured to transport rivets from the first port to the second port in a series arrangement and in a preselected orientation. The seat member communicates with the second port and is configured to selectively engage with a rivet holder of a resistance spot rivet welding apparatus and introduce a single rivet to the rivet holder at one time.
    Type: Grant
    Filed: December 13, 2019
    Date of Patent: October 18, 2022
    Assignees: HOWMET AEROSPACE INC., CenterLine (Windsor) Limited
    Inventors: Daniel Peter Vanderzwet, Simon Maurice Britton, Larry Frank Koscielski, Eric Jean Michaud, David Mario Simone, Donald J. Spinella, Gino N. Iasella, Daniel Bergstrom, Robert B. Wilcox, Thomas R. Kingsbury, Graham Scott Musgrove
  • Patent number: 11421303
    Abstract: The present disclosure relates to new titanium alloys and methods for making the same. The new titanium alloys generally include 4.75-6.75 wt. % Al, 6.5-8.5 wt. % (Nb+Ta), 1.5-3.5 wt. % Sn, up to 5.0 wt. % Zr, and up to 2.5 wt. % Mo, the balance being titanium, optional incidental elements, and impurities. Due to their composition and methods of manufacture, the new titanium alloys may find use in several applications, such as aerospace and/or automotive applications.
    Type: Grant
    Filed: April 13, 2020
    Date of Patent: August 23, 2022
    Assignee: HOWMET AEROSPACE INC.
    Inventors: Fusheng Sun, Ernest M. Crist, Jr.
  • Patent number: 11345188
    Abstract: A wheel rim including a flange profile on a tire side of an open end flange of the wheel rim, the flange profile defined by the equation: y 1 = ( a ? ? Theta ? ? 1 + 1 ( 1 + Exp ? ( a ? ? Theta ? ? 3 + a ? Theta ? ? 4 · X 1 ) ) aTheta ? ? 5 ) · a ? Theta ? 2 wherein, for 0?X1?1, aTheta1 is between ?1.004 to ?0.974, aTheta2 is between ??1.049 to ?1.0182, aTheta3 is between ?3.601 to ?2.760, aTheta4 is between 18.791 to 25.965, and aTheta5 is between 0.185 to 0.277.
    Type: Grant
    Filed: February 26, 2020
    Date of Patent: May 31, 2022
    Assignee: HOWMET AEROSPACE INC.
    Inventors: Craig M. Zehnder, Gabriele F. Ciccola, Grant DeGeorge, Santosh Prasad, Henry Sklyut, Anton Rovito, Christopher J. Tan, Jay H. Goodman
  • Patent number: D1003797
    Type: Grant
    Filed: July 14, 2021
    Date of Patent: November 7, 2023
    Assignee: HOWMET AEROSPACE INC.
    Inventors: Douglas P. Mason, Spencer Wallace
  • Patent number: D1017495
    Type: Grant
    Filed: July 14, 2021
    Date of Patent: March 12, 2024
    Assignee: HOWMET AEROSPACE INC.
    Inventors: Douglas P. Mason, Spencer Wallace