Patents by Inventor Chandra Sudhakar GUDIMETLA

Chandra Sudhakar GUDIMETLA 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: 11913586
    Abstract: A flow limiter component including a monocoque body having first, second, and third sections along a longitudinal axis. The first section includes a first end defining a first edge of the monocoque body and a bordering second end, and a first inner diameter defining a first chamber inside the first section. The second section includes a solid wall, with an orifice disposed therein, in fluid communication with the first chamber, the orifice defined by a second inner diameter. The third section includes a third end bordering the second section and a fourth end defining a second edge of the body, and a third inner diameter, the third inner diameter defining a second chamber in the third section. The second chamber is in fluid communication with the orifice. The first inner diameter is greater than the third inner diameter, and the third inner diameter is greater than the second inner diameter.
    Type: Grant
    Filed: June 25, 2021
    Date of Patent: February 27, 2024
    Assignee: The Boeing Company
    Inventor: Chandra Sudhakar Gudimetla
  • Patent number: 11879558
    Abstract: In an example, a pressure relief valve is described. The pressure relief valve comprises a housing configured to allow fluid flow therethrough. The pressure relief valve also comprises an adapter having interior threads, where the adapter is attached to the housing such that the adapter is positioned at least partially within the housing. The pressure relief valve also comprises an orifice plate having an orifice formed therein to allow fluid flow therethrough, where the orifice plate comprises exterior threads that engage with the interior threads of the adapter to couple the orifice plate to the adapter. The pressure relief valve also comprises a spring disposed within the housing. The orifice plate translates via engagement of the exterior threads with the interior threads to calibrate a spring force of the spring.
    Type: Grant
    Filed: January 27, 2022
    Date of Patent: January 23, 2024
    Assignee: The Boeing Company
    Inventor: Chandra Sudhakar Gudimetla
  • Publication number: 20220252172
    Abstract: In an example, a pressure relief valve is described. The pressure relief valve comprises a housing configured to allow fluid flow therethrough. The pressure relief valve also comprises an adapter having interior threads, where the adapter is attached to the housing such that the adapter is positioned at least partially within the housing. The pressure relief valve also comprises an orifice plate having an orifice formed therein to allow fluid flow therethrough, where the orifice plate comprises exterior threads that engage with the interior threads of the adapter to couple the orifice plate to the adapter. The pressure relief valve also comprises a spring disposed within the housing. The orifice plate translates via engagement of the exterior threads with the interior threads to calibrate a spring force of the spring.
    Type: Application
    Filed: January 27, 2022
    Publication date: August 11, 2022
    Inventor: Chandra Sudhakar Gudimetla
  • Publication number: 20220213966
    Abstract: A device including a sleeve having a first end, a second end opposite the first end, and a hole disposed through an outer diameter of the sleeve between the first end and the second end. The device includes a spool having a third end and a fourth end opposite the third end, the spool disposed at least partially inside the sleeve and configured to slide along a longitudinal axis of the sleeve. The device includes a spring having a fifth end and a sixth end opposite the fifth end, the spring disposed in a slot disposed in the spool, the spring and the slot oriented at least partially in a radial direction relative to the longitudinal axis. The device also includes a retaining bit disposed at the fifth end of the spring. The spring, in a partially compressed state, urges the retaining bit against an inner wall of the sleeve.
    Type: Application
    Filed: November 11, 2021
    Publication date: July 7, 2022
    Applicant: The Boeing Company
    Inventor: Chandra Sudhakar Gudimetla
  • Publication number: 20220049722
    Abstract: A flow limiter component including a monocoque body having first, second, and third sections along a longitudinal axis. The first section includes a first end defining a first edge of the monocoque body and a bordering second end, and a first inner diameter defining a first chamber inside the first section. The second section includes a solid wall, with an orifice disposed therein, in fluid communication with the first chamber, the orifice defined by a second inner diameter. The third section includes a third end bordering the second section and a fourth end defining a second edge of the body, and a third inner diameter, the third inner diameter defining a second chamber in the third section. The second chamber is in fluid communication with the orifice. The first inner diameter is greater than the third inner diameter, and the third inner diameter is greater than the second inner diameter.
    Type: Application
    Filed: June 25, 2021
    Publication date: February 17, 2022
    Applicant: The Boeing Company
    Inventor: Chandra Sudhakar Gudimetla
  • Patent number: 11174917
    Abstract: Example systems, apparatuses and methods are disclosed for gear reduction. An example system comprises a second gear configured to be disposed in mesh with a first gear coupled to an input shaft. The system further comprises a carrier housing configured to be fixably disposed within the second gear. The system further comprises a third gear configured to be disposed within the carrier housing; a fourth gear configured to be disposed in mesh with the third gear, wherein the third gear is further configured to rotate about the fourth gear; an anti-backlash gear coupled to the fourth gear and configured to be disposed in mesh with the third gear; and a fifth gear configured to be disposed in mesh with the third gear. The second gear, the fourth gear, the anti-backlash gear, and the fifth gear are configured to be disposed along a common axis of rotation.
    Type: Grant
    Filed: March 2, 2020
    Date of Patent: November 16, 2021
    Assignee: Honeywell International Inc.
    Inventors: Keith D. Larson, John Jerred, Stephen William Tillotson, Chandra Sudhakar Gudimetla, Mahesh Basavantappa Hallikeri, Joe Walling
  • Publication number: 20200278010
    Abstract: Example systems, apparatuses and methods are disclosed for gear reduction. An example system comprises a second gear configured to be disposed in mesh with a first gear coupled to an input shaft. The system further comprises a carrier housing configured to be fixably disposed within the second gear. The system further comprises a third gear configured to be disposed within the carrier housing; a fourth gear configured to be disposed in mesh with the third gear, wherein the third gear is further configured to rotate about the fourth gear; an anti-backlash gear coupled to the fourth gear and configured to be disposed in mesh with the third gear; and a fifth gear configured to be disposed in mesh with the third gear. The second gear, the fourth gear, the anti-backlash gear, and the fifth gear are configured to be disposed along a common axis of rotation.
    Type: Application
    Filed: March 2, 2020
    Publication date: September 3, 2020
    Inventors: Keith D. LARSON, John JERRED, Stephen William TILLOTSON, Chandra Sudhakar GUDIMETLA, Mahesh Basavantappa HALLIKERI, Joe WALLING