Patents by Inventor Zoran Pasic

Zoran Pasic has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 11708150
    Abstract: An aircraft landing gear assembly includes a main fitting comprising having a main barrel and a cross beam fixedly positioned relative to the main barrel and extending radially from the main barrel. The main fitting further includes a drag arm with a first end pivotally coupled to the cross beam by a first pivotal connection and a second end pivotally coupled to the main barrel by a second pivotal connection.
    Type: Grant
    Filed: February 9, 2021
    Date of Patent: July 25, 2023
    Assignee: Safran Landing Systems Canada Inc.
    Inventors: Randy Lee, Zoran Pasic, Charles Borchert, Adam Lucci
  • Publication number: 20220250740
    Abstract: An aircraft landing gear assembly includes a main fitting comprising having a main barrel and a cross beam fixedly positioned relative to the main barrel and extending radially from the main barrel. The main fitting further includes a drag arm with a first end pivotally coupled to the cross beam by a first pivotal connection and a second end pivotally coupled to the main barrel by a second pivotal connection.
    Type: Application
    Filed: February 9, 2021
    Publication date: August 11, 2022
    Applicant: SAFRAN LANDING SYSTEMS CANADA INC.
    Inventors: Randy Lee, Zoran Pasic, Charles Borchert, Adam Lucci
  • Patent number: 11383827
    Abstract: A truck beam for an aircraft landing gear assembly is provided. The truck beam includes an elongate hub having first and second ends. The hub is rotatably mountable to a shock strut of the landing gear assembly. A first leg extends radially in a first direction from the first end of the hub. The first leg has an inner side facing the second end of the hub and is configured to have a first wheel rotatably mounted to the inner side about a first wheel axis. A second leg extends radially in a second direction from the second end of the hub and has an inner side facing the first end of the hub. The second leg is configured to have a second wheel rotatably mounted to the inner side of the second leg about a second wheel axis.
    Type: Grant
    Filed: April 23, 2020
    Date of Patent: July 12, 2022
    Assignee: SAFRAN LANDING SYSTEMS CANADA INC.
    Inventors: Adam Lucci, Randy Lee, Gregory Eggers, Zoran Pasic
  • Patent number: 11377206
    Abstract: A torque link assembly for a landing gear includes a lower torque link and an upper torque link that releasably engage first and second quick release pin assemblies. The pin assemblies each include a housing attached to one of the torque links, and a locking pin member extending through the housing. The locking pin member includes a rod portion and a pin portion, and is slidable between an engaged position and a disengaged position for hingedly connecting/disconnecting the torque links. One of the housing and the locking pin member includes a channel having a longitudinal portion and a circumferential portion, and the other has a guide pin that engages the channel. The guide pin is in the longitudinal portion of the channel when moving between the engaged and disengaged positions, and is retained in the disengaged position when the guide pin is in the circumferential portion of the channel.
    Type: Grant
    Filed: March 23, 2018
    Date of Patent: July 5, 2022
    Assignee: SAFRAN LANDING SYSTEMS CANADA INC.
    Inventors: Steven Amberg, Randy Lee, Zoran Pasic
  • Publication number: 20210331785
    Abstract: A truck beam for an aircraft landing gear assembly is provided. The truck beam includes an elongate hub having first and second ends. The hub is rotatably mountable a shock strut of the landing gear assembly. A first leg extends radially in a first direction from the first end of the hub. The first leg has an inner side facing the second end of the hub and is configured to have a first wheel rotatably mounted to the inner side about a first wheel axis. A second leg extends radially in a second direction from the second end of the hub and has an inner side facing the first end of the hub. The second leg is configured to have a second wheel rotatably mounted to the inner side of the second leg about a second wheel axis.
    Type: Application
    Filed: April 23, 2020
    Publication date: October 28, 2021
    Applicant: SAFRAN LANDING SYSTEMS CANADA INC.
    Inventors: Adam Lucci, Randy Lee, Gregory Eggers, Zoran Pasic
  • Publication number: 20190291854
    Abstract: A torque link assembly for a landing gear includes a lower torque link and an upper torque link that releasably engage first and second quick release pin assemblies. The pin assemblies each include a housing attached to one of the torque links, and a locking pin member extending through the housing. The locking pin member includes a rod portion and a pin portion, and is slidable between an engaged position and a disengaged position for hingedly connecting/disconnecting the torque links. One of the housing and the locking pin member includes a channel having a longitudinal portion and a circumferential portion, and the other has a guide pin that engages the channel. The guide pin is in the longitudinal portion of the channel when moving between the engaged and disengaged positions, and is retained in the disengaged position when the guide pin is in the circumferential portion of the channel.
    Type: Application
    Filed: March 23, 2018
    Publication date: September 26, 2019
    Applicant: Safran Landing Systems Canada Inc.
    Inventors: Steven Amberg, Randy Lee, Zoran Pasic