GB202004387D0 - High pressure ratio gas turbine engine - Google Patents

High pressure ratio gas turbine engine

Info

Publication number
GB202004387D0
GB202004387D0 GBGB2004387.3A GB202004387A GB202004387D0 GB 202004387 D0 GB202004387 D0 GB 202004387D0 GB 202004387 A GB202004387 A GB 202004387A GB 202004387 D0 GB202004387 D0 GB 202004387D0
Authority
GB
United Kingdom
Prior art keywords
high pressure
gas turbine
turbine engine
pressure ratio
ratio gas
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.)
Ceased
Application number
GBGB2004387.3A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GBGB2004387.3A priority Critical patent/GB202004387D0/en
Publication of GB202004387D0 publication Critical patent/GB202004387D0/en
Priority to US17/196,460 priority patent/US20210301764A1/en
Priority to US17/196,382 priority patent/US11519363B2/en
Priority to US17/196,546 priority patent/US11629668B2/en
Priority to US17/196,345 priority patent/US20210348555A1/en
Priority to US17/196,393 priority patent/US20210301763A1/en
Priority to EP21161763.4A priority patent/EP3885554A1/en
Priority to EP21161766.7A priority patent/EP3885556A1/en
Priority to EP21161757.6A priority patent/EP3885552A1/en
Priority to EP21161765.9A priority patent/EP3885555A1/en
Priority to EP21161761.8A priority patent/EP3885553A1/en
Priority to CN202110326065.5A priority patent/CN113446117A/en
Priority to CN202110325824.6A priority patent/CN113446114A/en
Priority to CN202110325980.2A priority patent/CN113446115A/en
Priority to CN202110326079.7A priority patent/CN113446118A/en
Priority to CN202110326007.2A priority patent/CN113446116A/en
Ceased legal-status Critical Current

Links

GBGB2004387.3A 2020-03-26 2020-03-26 High pressure ratio gas turbine engine Ceased GB202004387D0 (en)

Priority Applications (16)

Application Number Priority Date Filing Date Title
GBGB2004387.3A GB202004387D0 (en) 2020-03-26 2020-03-26 High pressure ratio gas turbine engine
US17/196,460 US20210301764A1 (en) 2020-03-26 2021-03-09 Gas turbine engine
US17/196,382 US11519363B2 (en) 2020-03-26 2021-03-09 High pressure ratio gas turbine engine
US17/196,546 US11629668B2 (en) 2020-03-26 2021-03-09 High pressure ratio gas turbine engine
US17/196,345 US20210348555A1 (en) 2020-03-26 2021-03-09 High pressure ratio gas turbine engine
US17/196,393 US20210301763A1 (en) 2020-03-26 2021-03-09 Gas turbine engine
EP21161761.8A EP3885553A1 (en) 2020-03-26 2021-03-10 High pressure ratio gas turbine engine
EP21161763.4A EP3885554A1 (en) 2020-03-26 2021-03-10 High pressure ratio gas turbine engine
EP21161766.7A EP3885556A1 (en) 2020-03-26 2021-03-10 High pressure ratio gas turbine engine
EP21161757.6A EP3885552A1 (en) 2020-03-26 2021-03-10 Gas turbine engine
EP21161765.9A EP3885555A1 (en) 2020-03-26 2021-03-10 Gas turbine engine
CN202110326065.5A CN113446117A (en) 2020-03-26 2021-03-26 High pressure ratio gas turbine engine
CN202110325824.6A CN113446114A (en) 2020-03-26 2021-03-26 High pressure ratio gas turbine engine
CN202110325980.2A CN113446115A (en) 2020-03-26 2021-03-26 Gas turbine engine
CN202110326079.7A CN113446118A (en) 2020-03-26 2021-03-26 Gas turbine engine
CN202110326007.2A CN113446116A (en) 2020-03-26 2021-03-26 High pressure ratio gas turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB2004387.3A GB202004387D0 (en) 2020-03-26 2020-03-26 High pressure ratio gas turbine engine

Publications (1)

Publication Number Publication Date
GB202004387D0 true GB202004387D0 (en) 2020-05-13

Family

ID=70553473

Family Applications (1)

Application Number Title Priority Date Filing Date
GBGB2004387.3A Ceased GB202004387D0 (en) 2020-03-26 2020-03-26 High pressure ratio gas turbine engine

Country Status (1)

Country Link
GB (1) GB202004387D0 (en)

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Legal Events

Date Code Title Description
AT Applications terminated before publication under section 16(1)