Patents by Inventor NICHOLAS R. FARRELL

NICHOLAS R. FARRELL 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: 10434624
    Abstract: A machining tool incorporates a shaft having a first end configured to fit into a machining collet. A cutting portion extends from a second end of the shaft. A residual stress inducer is located between the first and second ends and includes a torsion element joined to the shaft at a connection end. A carbide tip is present on a free end opposite the connection end and the torsion element is configured such that a selected rotational speed, altered from a normal cutting speed, causes the carbide tip of the torsion element to contact a workpiece surface.
    Type: Grant
    Filed: July 7, 2016
    Date of Patent: October 8, 2019
    Assignee: The Boeing Company
    Inventors: Nicholas R. Farrell, James D. Gamboa, Wesley E. Holleman, Gary Lipczynski
  • Patent number: 9889510
    Abstract: Within examples, systems and methods for forming a hole through at least one layer of a material are provided. An example cutting tool for forming such a hole may include a body, and a first portion of the body having a first diameter and a first radial rake angle. The cutting tool also includes a second portion of the body adjacent the first portion, the second portion having a second diameter and a second radial rake angle, wherein the second diameter is different than the first diameter, and wherein the second radial rake angle is different than the first radial rake angle.
    Type: Grant
    Filed: January 5, 2016
    Date of Patent: February 13, 2018
    Assignee: The Boeing Company
    Inventors: Nicholas R. Farrell, Gary Lipczynski
  • Patent number: 9884371
    Abstract: Apparatus and methods for performing and controlling the sequence of steps in a multi-step machining process utilizing a plurality of drilling units, where each drilling unit is configured to perform at least one step of the multi-step machining process. Air pressure sensors in each drilling unit measure air pressures at the surface of a workpiece where the cutting tool of the drilling unit is engaged, which measured air pressures indicate air flow at the surface. These air flows in turn indicate the state of the machining at the surface of the workpiece, and based on the state of the machining, a machine control system will determine whether a drilling unit can perform its particular machining operation in the proper sequence on the workpiece.
    Type: Grant
    Filed: November 16, 2015
    Date of Patent: February 6, 2018
    Assignee: The Boeing Company
    Inventors: Wesley Edward Holleman, Gary A. Lipczynski, Nicholas R. Farrell
  • Publication number: 20180009082
    Abstract: A machining tool incorporates a shaft having a first end configured to fit into a machining collet. A cutting portion extends from a second end of the shaft. A residual stress inducer is located between the first and second ends and includes a torsion element joined to the shaft at a connection end. A carbide tip is present on a free end opposite the connection end and the torsion element is configured such that a selected rotational speed, altered from a normal cutting speed, causes the carbide tip of the torsion element to contact a workpiece surface.
    Type: Application
    Filed: July 7, 2016
    Publication date: January 11, 2018
    Inventors: Nicholas R. Farrell, James D. Gamboa, Wesley E. Holleman, Gary Lipczynski
  • Patent number: 9770769
    Abstract: Described herein is an orbital drilling system that includes an orbital drilling machine and a cutter. The orbital drilling machine includes a spindle and an eccentric rotation mechanism. The spindle is rotatable about a cutter axis. The eccentric rotation mechanism is coupled to the spindle and configured to orbit the spindle about an orbital axis, offset from the cutter axis. The cutter is co-rotatably coupled to the spindle and comprises a plurality of cutting edges, collectively defining a cutting diameter of the cutter. The cutting diameter of the cutter is adjustable.
    Type: Grant
    Filed: January 22, 2016
    Date of Patent: September 26, 2017
    Assignee: The Boeing Company
    Inventors: Wesley E. Holleman, Nicholas R. Farrell
  • Publication number: 20170209946
    Abstract: Described herein is an orbital drilling system that includes an orbital drilling machine and a cutter. The orbital drilling machine includes a spindle and an eccentric rotation mechanism. The spindle is rotatable about a cutter axis. The eccentric rotation mechanism is coupled to the spindle and configured to orbit the spindle about an orbital axis, offset from the cutter axis. The cutter is co-rotatably coupled to the spindle and comprises a plurality of cutting edges, collectively defining a cutting diameter of the cutter. The cutting diameter of the cutter is adjustable.
    Type: Application
    Filed: January 22, 2016
    Publication date: July 27, 2017
    Inventors: Wesley E. Holleman, Nicholas R. Farrell
  • Publication number: 20170189973
    Abstract: Within examples, systems and methods for forming a hole through at least one layer of a material are provided. An example cutting tool for forming such a hole may include a body, and a first portion of the body having a first diameter and a first radial rake angle. The cutting tool also includes a second portion of the body adjacent the first portion, the second portion having a second diameter and a second radial rake angle, wherein the second diameter is different than the first diameter, and wherein the second radial rake angle is different than the first radial rake angle.
    Type: Application
    Filed: January 5, 2016
    Publication date: July 6, 2017
    Inventors: Nicholas R. Farrell, Gary Lipczynski
  • Publication number: 20170136554
    Abstract: Apparatus and methods for performing and controlling the sequence of steps in a multi-step machining process utilizing a plurality of drilling units, where each drilling unit is configured to perform at least one step of the multi-step machining process. Air pressure sensors in each drilling unit measure air pressures at the surface of a workpiece where the cutting tool of the drilling unit is engaged, which measured air pressures indicate air flow at the surface. These air flows in turn indicate the state of the machining at the surface of the workpiece, and based on the state of the machining, a machine control system will determine whether a drilling unit can perform its particular machining operation in the proper sequence on the workpiece.
    Type: Application
    Filed: November 16, 2015
    Publication date: May 18, 2017
    Inventors: WESLEY EDWARD HOLLEMAN, GARY A. LIPCZYNSKI, NICHOLAS R. FARRELL