JP2012072763A5 - - Google Patents

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Publication number
JP2012072763A5
JP2012072763A5 JP2011208361A JP2011208361A JP2012072763A5 JP 2012072763 A5 JP2012072763 A5 JP 2012072763A5 JP 2011208361 A JP2011208361 A JP 2011208361A JP 2011208361 A JP2011208361 A JP 2011208361A JP 2012072763 A5 JP2012072763 A5 JP 2012072763A5
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JP
Japan
Prior art keywords
synchronization ring
variable stator
bearings
mounting studs
lever arms
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP2011208361A
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English (en)
Japanese (ja)
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JP5941259B2 (ja
JP2012072763A (ja
Filing date
Publication date
Priority claimed from US12/892,269 external-priority patent/US8714916B2/en
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Publication of JP2012072763A publication Critical patent/JP2012072763A/ja
Publication of JP2012072763A5 publication Critical patent/JP2012072763A5/ja
Application granted granted Critical
Publication of JP5941259B2 publication Critical patent/JP5941259B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2011208361A 2010-09-28 2011-09-26 タービン圧縮機用の可変静翼集成体 Active JP5941259B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/892,269 2010-09-28
US12/892,269 US8714916B2 (en) 2010-09-28 2010-09-28 Variable vane assembly for a turbine compressor

Publications (3)

Publication Number Publication Date
JP2012072763A JP2012072763A (ja) 2012-04-12
JP2012072763A5 true JP2012072763A5 (https=) 2014-11-13
JP5941259B2 JP5941259B2 (ja) 2016-06-29

Family

ID=45804819

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2011208361A Active JP5941259B2 (ja) 2010-09-28 2011-09-26 タービン圧縮機用の可変静翼集成体

Country Status (5)

Country Link
US (1) US8714916B2 (https=)
JP (1) JP5941259B2 (https=)
CN (1) CN102418712B (https=)
CH (1) CH703871B1 (https=)
DE (1) DE102011053433A1 (https=)

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US11215117B2 (en) * 2019-11-08 2022-01-04 Raytheon Technologies Corporation Gas turbine engine having electric motor applying power to the high pressure spool shaft and method for operating same
US20210254557A1 (en) * 2020-02-13 2021-08-19 Honeywell International Inc. Variable vane system for turbomachine with linkage having tapered receiving aperture for unison ring pin
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CN112065743B (zh) * 2020-08-21 2025-01-28 山东钢铁股份有限公司 高炉轴流鼓风机可调式信号反馈连杆的使用方法
CN112360815B (zh) * 2020-11-10 2022-05-24 沈观清 用于多级涵道风扇的可调节定片机构及该机构的控制系统
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DE102021128979A1 (de) * 2021-11-08 2023-05-11 MTU Aero Engines AG Verstellhebel für eine strömungsmaschine
CN117287420A (zh) * 2022-06-16 2023-12-26 中国航发商用航空发动机有限责任公司 静叶调节机构及航空发动机
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