Invention Grant
US09447974B2 Light weight swirler for gas turbine engine combustor and a method for lightening a swirler for a gas turbine engine
有权
用于燃气涡轮发动机燃烧器的轻质旋流器和用于减轻燃气涡轮发动机的旋流器的方法
- Patent Title: Light weight swirler for gas turbine engine combustor and a method for lightening a swirler for a gas turbine engine
- Patent Title (中): 用于燃气涡轮发动机燃烧器的轻质旋流器和用于减轻燃气涡轮发动机的旋流器的方法
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Application No.: US13614657Application Date: 2012-09-13
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Publication No.: US09447974B2Publication Date: 2016-09-20
- Inventor: Seth A. Max , Jonathan M. Jause
- Applicant: Seth A. Max , Jonathan M. Jause
- Applicant Address: US CT Farmington
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: O'Shea Getz P.C.
- Main IPC: F23R3/14
- IPC: F23R3/14 ; F23R3/28 ; F23R3/12 ; F23R3/04 ; F23R3/10
Abstract:
The disclosure is directed to a swirler body for a combustor of a gas turbine engine, where the swirler body includes an annular mount face which defines at least one pocket. The disclosure is directed to a swirler assembly for a combustor of a gas turbine engine, where the swirler assembly includes a swirler first body with an annular first mount face which defines at least one first pocket and a swirler second body with an annular second mount face which abuts said annular first mount face, where said second annular mount face defines at least one second pocket. The disclosure is directed to a method of lightening a swirl assembly for a combustor of a gas turbine engine, where the method includes defining at least one pocket within an annular mount face of a swirler body.
Public/Granted literature
- US20150192300A1 LIGHT WEIGHT SWIRLER FOR GAS TURBINE ENGINE COMBUSTOR AND A METHOD OF MANUFACTURING Public/Granted day:2015-07-09
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