Patents by Inventor Chris T. Jasklowski

Chris T. Jasklowski 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).

  • Flexible band electrical component mounts and methods
    Patent number: 10822995
    Abstract: Systems and methods are provided for a flexible band electrical component mount that includes a flexible band configured to receive one or more electrical components. The flexible band may be configured to couple to and/or wrap around at least a portion of an aircraft propulsor. The electrical components may be configured to output data from the aircraft propulsor and/or data related to operation of the aircraft propulsor. Such flexible bands may be configured to receive a plurality of electrical components and may be configured to wrap around the portion of the aircraft propulsor a plurality of times.
    Type: Grant
    Filed: January 17, 2017
    Date of Patent: November 3, 2020
    Assignee: The Boeing Company
    Inventor: Chris T. Jasklowski
  • Engine turning motor via pneumatic or hydraulic motor
    Patent number: 10753225
    Abstract: Pressurized fluid is stored while a jet engine is running. After engine shutdown, the fluid is used to drive a pneumatic or hydraulic turning motor that rotates the engine's High Pressure (HP) rotor. The rotation encourages even heat distribution across the HP rotor and thus prevents bowing of the HP rotor.
    Type: Grant
    Filed: March 31, 2017
    Date of Patent: August 25, 2020
    Assignee: THE BOEING COMPANY
    Inventors: Kent E. Karnofski, Chris T. Jasklowski, Jason J. Jackowski
  • Telescoping electrical cable
    Patent number: 10422301
    Abstract: An aircraft includes a jet engine and a telescopic tube assembly positioned on the jet engine. The telescopic tube assembly includes one end portion of the telescopic tube assembly which is associated with a thrust reverser translating sleeve of the jet engine and an opposing end portion of the telescopic tube assembly which is associated with a fixed portion of the of the jet engine. A jet engine includes a telescopic tube assembly positioned on the jet engine. The telescopic tube assembly includes one end portion of the telescopic tube assembly which is associated with a thrust reverser translating sleeve of a jet engine and an opposing end portion of the telescopic tube assembly which is associated with a fixed portion of the of the jet engine.
    Type: Grant
    Filed: July 13, 2015
    Date of Patent: September 24, 2019
    Assignee: THE BOEING COMPANY
    Inventors: Kent Edmund Karnofski, Chris T. Jasklowski, Michael Jay Burghdoff
  • ENGINE TURNING MOTOR VIA PNEUMATIC OR HYDRAULIC MOTOR
    Publication number: 20180283199
    Abstract: Pressurized fluid is stored while a jet engine is running. After engine shutdown, the fluid is used to drive a pneumatic or hydraulic turning motor that rotates the engine's High Pressure (HP) rotor. The rotation encourages even heat distribution across the HP rotor and thus prevents bowing of the HP rotor.
    Type: Application
    Filed: March 31, 2017
    Publication date: October 4, 2018
    Applicant: The Boeing Company
    Inventors: Kent E. Karnofski, Chris T. Jasklowski, Jason J. Jackowski
  • FLEXIBLE BAND ELECTRICAL COMPONENT MOUNTS AND METHODS
    Publication number: 20180202313
    Abstract: Systems and methods are provided for a flexible band electrical component mount that includes a flexible band configured to receive one or more electrical components. The flexible band may be configured to couple to and/or wrap around at least a portion of an aircraft propulsor. The electrical components may be configured to output data from the aircraft propulsor and/or data related to operation of the aircraft propulsor. Such flexible bands may be configured to receive a plurality of electrical components and may be configured to wrap around the portion of the aircraft propulsor a plurality of times.
    Type: Application
    Filed: January 17, 2017
    Publication date: July 19, 2018
    Inventor: Chris T. Jasklowski
  • TELESCOPING ELECTRICAL CABLE
    Publication number: 20170016413
    Abstract: An aircraft includes a jet engine and a telescopic tube assembly positioned on the jet engine. The telescopic tube assembly includes one end portion of the telescopic tube assembly which is associated with a thrust reverser translating sleeve of the jet engine and an opposing end portion of the telescopic tube assembly which is associated with a fixed portion of the of the jet engine. A jet engine includes a telescopic tube assembly positioned on the jet engine. The telescopic tube assembly includes one end portion of the telescopic tube assembly which is associated with a thrust reverser translating sleeve of a jet engine and an opposing end portion of the telescopic tube assembly which is associated with a fixed portion of the of the jet engine.
    Type: Application
    Filed: July 13, 2015
    Publication date: January 19, 2017
    Inventors: Kent Edmund Karnofski, Chris T. Jasklowski, Michael Jay Burghdoff