JP2011231767A5 - - Google Patents

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Publication number
JP2011231767A5
JP2011231767A5 JP2011101128A JP2011101128A JP2011231767A5 JP 2011231767 A5 JP2011231767 A5 JP 2011231767A5 JP 2011101128 A JP2011101128 A JP 2011101128A JP 2011101128 A JP2011101128 A JP 2011101128A JP 2011231767 A5 JP2011231767 A5 JP 2011231767A5
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JP
Japan
Prior art keywords
engine
flow path
engine according
valve
exhaust
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
JP2011101128A
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English (en)
Japanese (ja)
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JP2011231767A (ja
JP5714405B2 (ja
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Publication date
Priority claimed from GBGB1007063.9A external-priority patent/GB201007063D0/en
Application filed filed Critical
Publication of JP2011231767A publication Critical patent/JP2011231767A/ja
Publication of JP2011231767A5 publication Critical patent/JP2011231767A5/ja
Application granted granted Critical
Publication of JP5714405B2 publication Critical patent/JP5714405B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2011101128A 2010-04-28 2011-04-28 ガスタービンエンジン Expired - Fee Related JP5714405B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB1007063.9A GB201007063D0 (en) 2010-04-28 2010-04-28 A gas turbine engine
GB1007063.9 2010-04-28

Publications (3)

Publication Number Publication Date
JP2011231767A JP2011231767A (ja) 2011-11-17
JP2011231767A5 true JP2011231767A5 (enExample) 2015-03-19
JP5714405B2 JP5714405B2 (ja) 2015-05-07

Family

ID=42270939

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2011101128A Expired - Fee Related JP5714405B2 (ja) 2010-04-28 2011-04-28 ガスタービンエンジン

Country Status (4)

Country Link
US (1) US8876465B2 (enExample)
EP (1) EP2383441B1 (enExample)
JP (1) JP5714405B2 (enExample)
GB (1) GB201007063D0 (enExample)

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US10808619B2 (en) 2018-04-19 2020-10-20 Raytheon Technologies Corporation Intercooled cooling air with advanced cooling system
US10830145B2 (en) 2018-04-19 2020-11-10 Raytheon Technologies Corporation Intercooled cooling air fleet management system
US10718233B2 (en) 2018-06-19 2020-07-21 Raytheon Technologies Corporation Intercooled cooling air with low temperature bearing compartment air
US11255268B2 (en) 2018-07-31 2022-02-22 Raytheon Technologies Corporation Intercooled cooling air with selective pressure dump
JP2020121605A (ja) * 2019-01-29 2020-08-13 京セラ株式会社 カメラ清浄装置および制御方法
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US11519368B2 (en) 2020-01-07 2022-12-06 Raytheon Technologies Corporation Heat exchanger supply plenum
BE1029507B1 (fr) * 2021-06-18 2023-01-23 Gen Electric Structure de turbomachine a trois flux
WO2022262998A1 (fr) * 2021-06-18 2022-12-22 Safran Aero Boosters Sa Structure de turbomachine a trois flux
US11639671B2 (en) 2021-07-06 2023-05-02 General Electric Company Unducted fan turbine engine with a cowl door
US11492918B1 (en) 2021-09-03 2022-11-08 General Electric Company Gas turbine engine with third stream
US11834995B2 (en) 2022-03-29 2023-12-05 General Electric Company Air-to-air heat exchanger potential in gas turbine engines
US12071896B2 (en) 2022-03-29 2024-08-27 General Electric Company Air-to-air heat exchanger potential in gas turbine engines
CN118974386A (zh) * 2022-04-04 2024-11-15 赛峰飞机发动机公司 包括冷却空气通道和可变排放阀喷射通道的无涵道螺旋桨燃气涡轮
US11834954B2 (en) 2022-04-11 2023-12-05 General Electric Company Gas turbine engine with third stream
US12065989B2 (en) 2022-04-11 2024-08-20 General Electric Company Gas turbine engine with third stream
US11680530B1 (en) 2022-04-27 2023-06-20 General Electric Company Heat exchanger capacity for one or more heat exchangers associated with a power gearbox of a turbofan engine
US11834992B2 (en) 2022-04-27 2023-12-05 General Electric Company Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine
US12060829B2 (en) 2022-04-27 2024-08-13 General Electric Company Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine
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