Patents by Inventor Su Hyeong CHO

Su Hyeong CHO 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).

  • Publication number: 20230204212
    Abstract: A combustor includes: a combustor case; a combustor liner which is arranged in the combustor case and into which fuel is injected; and an air guide unit that is hollow and is formed to protrude from an inner surface of the combustor liner to inject air into an inside of the combustor liner, wherein the air guide unit includes: a first portion forming one end of the air guide unit and coupled to the inner surface of the combustor liner; and a second portion forming another end of the air guide unit and disposed in the combustor liner, and a size of the first portion is different from a size of the second portion.
    Type: Application
    Filed: May 6, 2022
    Publication date: June 29, 2023
    Applicant: Hanwha Aerospace Co., Ltd.
    Inventors: Shaun Kim, Su Hyeong Cho, Ju Pyoung Kim
  • Patent number: 11435082
    Abstract: A fuel supply device includes: an outer tubular member; an inner tubular member inside the outer tubular member; and a flow distribution portion on an inner surface of the outer tubular member or an outer surface of the inner tubular member, wherein the flow distribution portion includes first and second distribution wall portions arranged apart from one another in an axial direction of the inner tubular member, the first distribution wall portion includes first individual wall portions spaced apart from one another along a first circumference of the inner tubular member, the second distribution wall portion includes second individual wall portions spaced apart from one another along a second circumference of the inner tubular member, at least some of the first individual wall portions are arranged to face spaces between at least some of the second individual wall portions, respectively, in the axial direction of the inner tubular member.
    Type: Grant
    Filed: May 28, 2021
    Date of Patent: September 6, 2022
    Assignee: HANWHA AEROSPACE CO., LTD.
    Inventors: Ju Pyoung Kim, Sin Hyen Kim, Seung Chai Jung, Su Hyeong Cho
  • Publication number: 20220196240
    Abstract: A fuel supply device includes: an outer tubular member; an inner tubular member inside the outer tubular member; and a flow distribution portion on an inner surface of the outer tubular member or an outer surface of the inner tubular member, wherein the flow distribution portion includes first and second distribution wall portions arranged apart from one another in an axial direction of the inner tubular member, the first distribution wall portion includes first individual wall portions spaced apart from one another along a first circumference of the inner tubular member, the second distribution wall portion includes second individual wall portions spaced apart from one another along a second circumference of the inner tubular member, at least some of the first individual wall portions are arranged to face spaces between at least some of the second individual wall portions, respectively, in the axial direction of the inner tubular member.
    Type: Application
    Filed: May 28, 2021
    Publication date: June 23, 2022
    Applicant: HANWHA AEROSPACE CO., LTD.
    Inventors: Ju Pyoung KIM, Sin Hyen KIM, Seung Chai JUNG, Su Hyeong CHO
  • Patent number: 10344980
    Abstract: Provided is a combustor assembly. The combust assembly includes: a plurality of swirlers through which a first fluid that is a part of a fluid discharged from a compressor passes; a base portion, in which the plurality of swirlers are provided, comprising a first through hole formed between one swirler and another swirler from among the plurality of swirlers so that a second fluid that is another part of the fluid discharged from the compressor and different from the first fluid passes through the first through hole; and a deflector provided in the base portion so as to face the first through hole for changing a moving direction of the second fluid.
    Type: Grant
    Filed: October 27, 2014
    Date of Patent: July 9, 2019
    Assignee: HANWHA AEROSPACE CO., LTD.
    Inventors: Hee Ho Park, Su Hyeong Cho
  • Publication number: 20170234538
    Abstract: Provided is a combustor assembly. The combust assembly includes: a plurality of swirlers through which a first fluid that is a part of a fluid discharged from a compressor passes; a base portion, in which the plurality of swirlers are provided, comprising a first through hole formed between one swirler and another swirler from among the plurality of swirlers so that a second fluid that is another part of the fluid discharged from the compressor and different from the first fluid passes through the first through hole; and a deflector provided in the base portion so as to face the first through hole for changing a moving direction of the second fluid.
    Type: Application
    Filed: October 27, 2014
    Publication date: August 17, 2017
    Applicant: Hanwha Techwin Co., Ltd.
    Inventors: Hee Ho PARK, Su Hyeong CHO