Patents by Inventor Jonathan M. BOND

Jonathan M. BOND 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).

  • Laboratory experiment data exploration and visualization
    Patent number: 11955207
    Abstract: The disclosure provides systems and methods for data analysis of experimental data. The analysis can include reference data that are not directly generated from the present experiment, which reference data may be values of the experimental parameters that were either provided by a user, computed by the system with input from a user, or computed by the system without using any input from a user. Another example of such reference data may be information about the instrument, such as the calibration method of the instrument.
    Type: Grant
    Filed: June 30, 2016
    Date of Patent: April 9, 2024
    Assignee: Emerald Cloud Lab, Inc.
    Inventors: Alex M. Yoshikawa, Anand V. Sastry, Asuka Ota, Ben C. Kline, Bradley M. Bond, Brian M. Frezza, Cameron R. Lamoureux, Catherine L. Hofler, Cheri Y. Li, Courtney E. Webster, Daniel J. Kleinbaum, George N. Stanley, George W. Fraser, Guillaume Robichaud, Hayley E. Buchman, James R. McKernan, Jonathan K. Leung, Paul R. Zurek, Robert M. Teed, Ruben E. Valas, Sean M. Fitzgerald, Sergio I. Villarreal, Shayna L. Hilburg, Shivani S. Baisiwala, Srikant Vaithilingam, Wyatt J. Woodson, Yang Choo, Yidan Y. Cong
  • AIRCRAFT GAS TURBINE ENGINE NACELLE
    Publication number: 20180045140
    Abstract: An aircraft gas turbine engine nacelle comprising a thrust reversal arrangement. The thrust reversal arrangement comprises at least one thrust reverser cascade box comprising a fixed structure and a plurality of thrust reverser vanes configured to direct bypass air forwardly. At least a subset of the thrust reverser vanes are pivotable and/or translatable relative to the fixed structure between a deployed position, in which the vanes define a first volume, and a stowed position, in which the pivotable vanes define a second, smaller volume.
    Type: Application
    Filed: July 25, 2017
    Publication date: February 15, 2018
    Applicant: ROLLS-ROYCE plc
    Inventor: Jonathan M. BOND
  • AIRCRAFT PNEUMATIC SYSTEM
    Publication number: 20170113808
    Abstract: An aircraft pneumatic system comprises a gas turbine engine (10) comprising a compressor (14), a fan (12) and a core turbine (12) coupled to one of the compressor (14) and the fan (12), an auxiliary turbine (50) having an inlet in fluid communication with the core turbine (20), the auxiliary turbine (50) being configured to power an auxiliary compressor (40), an inlet of the auxiliary compressor (40) being in fluid communication with an outlet of the fan (12), and an outlet of the auxiliary compressor (40) being in fluid communication with an aircraft environmental control system (48).
    Type: Application
    Filed: October 7, 2016
    Publication date: April 27, 2017
    Applicant: ROLLS-ROYCE plc
    Inventor: Jonathan M. BOND