Title:
連続的に湾曲したライナセグメントを有する一体型燃焼器ノズル
Document Type and Number:
Japanese Patent JP7362287
Kind Code:
B2
Abstract:
An integrated combustor nozzle includes an inner liner segment; an outer liner segment; and a panel extending radially between the inner and outer liner segments. The panel includes a forward end, an aft end, and a side walls extending axially from the forward end to the aft end. The aft end defines a turbine nozzle having a trailing edge circumferentially offset from the forward end. The inner liner segment has a pair of sealing surfaces, each of which defines a first continuous curve in the circumferential direction. The outer liner segment has a pair of sealing surfaces, each of which defines a second continuous curve in the circumferential direction. In some instances, the curves are monotonic in the circumferential direction. A segmented annular combustor including an array of such integrated combustor nozzles is also provided.
Inventors:
Jonathan Dwight Berry
Michael John Hughes
Russell Pearson Deforest
Kevin Weston McMahan
Victor John Morgan
Ibrahim Sezel
Nielesh Nandkumar Sarawate
Deepak Trivedy
Michael John Hughes
Russell Pearson Deforest
Kevin Weston McMahan
Victor John Morgan
Ibrahim Sezel
Nielesh Nandkumar Sarawate
Deepak Trivedy
Application Number:
JP2019074515A
Publication Date:
October 17, 2023
Filing Date:
April 10, 2019
Export Citation:
Assignee:
GENERAL ELECTRIC COMPANY
International Classes:
F23R3/42; F23R3/28
Domestic Patent References:
| JP2004211705A | ||||
| JP2015031289A |
Foreign References:
| WO2017165611A1 | ||||
| US20170307221 |
Attorney, Agent or Firm:
Hiroshi Ogura
Toshihisa Kurokawa
Takuto Tanaka
Toshihisa Kurokawa
Takuto Tanaka