Patents by Inventor Jayanth Hirebelaguly Shivaprakash

Jayanth Hirebelaguly Shivaprakash 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).

  • Frangible strut for gas turbine engine
    Patent number: 11313250
    Abstract: A frangible strut for a gas turbine engine includes a first end to couple to a first structure of the gas turbine engine, and a second end opposite the first end. The second end is to couple to a second structure of the gas turbine engine. The second end includes an outer portion coaxial with and spaced radially apart from an inner portion. The inner portion is to receive a fastening device to couple the second end to the second structure. The outer portion is coupled to a body of the frangible strut. The inner portion is interconnected to the outer portion by a plurality of frangible members that are spaced apart about a perimeter of the inner portion, and each of the frangible members are configured to release the inner portion from the outer portion. The frangible strut includes the body interconnecting the first end and the second end.
    Type: Grant
    Filed: July 15, 2020
    Date of Patent: April 26, 2022
    Assignee: HONEYWELL INTERNATIONAL INC.
    Inventors: Manjunath Subbarayachar, Anil Kumar Thokala, Jayanth Hirebelaguly Shivaprakash, Pavankumar Kadam, Avinash Kumar
  • Frangible strut for gas turbine engine
    Patent number: 10837320
    Abstract: A frangible strut for a gas turbine engine includes a first end to couple to a first structure of the gas turbine engine, and a second end opposite the first end. The second end is to couple to a second structure of the gas turbine engine. The second end includes an outer portion coaxial with and spaced radially apart from an inner portion. The inner portion is to receive a fastening device to couple the second end to the second structure. The outer portion is coupled to a body of the frangible strut. The inner portion is interconnected to the outer portion by a plurality of frangible members that are spaced apart about a perimeter of the inner portion, and each of the frangible members are configured to release the inner portion from the outer portion. The frangible strut includes the body interconnecting the first end and the second end.
    Type: Grant
    Filed: September 25, 2018
    Date of Patent: November 17, 2020
    Assignee: HONEYWELL INTERNATIONAL INC.
    Inventors: Manjunath Subbarayachar, Anil Kumar Thokala, Jayanth Hirebelaguly Shivaprakash, Pavankumar Kadam, Avinash Kumar
  • FRANGIBLE STRUT FOR GAS TURBINE ENGINE
    Publication number: 20200347751
    Abstract: A frangible strut for a gas turbine engine includes a first end to couple to a first structure of the gas turbine engine, and a second end opposite the first end. The second end is to couple to a second structure of the gas turbine engine. The second end includes an outer portion coaxial with and spaced radially apart from an inner portion. The inner portion is to receive a fastening device to couple the second end to the second structure. The outer portion is coupled to a body of the frangible strut. The inner portion is interconnected to the outer portion by a plurality of frangible members that are spaced apart about a perimeter of the inner portion, and each of the frangible members are configured to release the inner portion from the outer portion. The frangible strut includes the body interconnecting the first end and the second end.
    Type: Application
    Filed: July 15, 2020
    Publication date: November 5, 2020
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Manjunath Subbarayachar, Anil Kumar Thokala, Jayanth Hirebelaguly Shivaprakash, Pavankumar Kadam, Avinash Kumar
  • FRANGIBLE STRUT FOR GAS TURBINE ENGINE
    Publication number: 20200095895
    Abstract: A frangible strut for a gas turbine engine includes a first end to couple to a first structure of the gas turbine engine, and a second end opposite the first end. The second end is to couple to a second structure of the gas turbine engine. The second end includes an outer portion coaxial with and spaced radially apart from an inner portion. The inner portion is to receive a fastening device to couple the second end to the second structure. The outer portion is coupled to a body of the frangible strut. The inner portion is interconnected to the outer portion by a plurality of frangible members that are spaced apart about a perimeter of the inner portion, and each of the frangible members are configured to release the inner portion from the outer portion. The frangible strut includes the body interconnecting the first end and the second end.
    Type: Application
    Filed: September 25, 2018
    Publication date: March 26, 2020
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Manjunath Subbarayachar, Anil Kumar Thokala, Jayanth Hirebelaguly Shivaprakash, Pavankumar Kadam, Avinash Kumar