Gas turbine having a high-speed low-pressure turbine and a turbine case
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United States of America Patent
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N/A
Issued Date -
Jan 10, 2019
app pub date -
Jul 5, 2018
filing date -
Jul 5, 2018
priority date (Note) -
Published
status (Latency Note)
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Abstract
A gas turbine (40) having a high-speed low-pressure turbine (24) and a turbine case (28) that bounds a flow path of a working fluid of the gas turbine (40) and an exit region (30), and extends between a rotor (32) of the high-speed low-pressure turbine (24) that is the most downstream in the through flow direction of the working fluid, and an exit opening (34) of the turbine case (28). The exit region (30) is designed to be free of exit guide vane assemblies.
First Claim
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Family

- 15 United States
- 10 France
- 8 Japan
- 7 China
- 5 Korea
- 2 Other
Patent Owner(s)
Patent Owner | Address | |
---|---|---|
MTU AERO ENGINES AG | 80995 MÜNCHEN |
International Classification(s)

- 2018 Application Filing Year
- F02K Class
- 467 Applications Filed
- 297 Patents Issued To-Date
- 63.60 % Issued To-Date
Inventor(s)
Inventor Name | Address | # of filed Patents | Total Citations |
---|---|---|---|
RAMM, Guenter | Eichenau, DE | 11 | 50 |
# of filed Patents : 11 Total Citations : 50 | |||
SCHABER, Reinhold | Ottobrunn, DE | 1 | 1 |
# of filed Patents : 1 Total Citations : 1 |
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Patent Citation Ranking
- 1 Citation Count
- F02K Class
- 26.87 % this patent is cited more than
- 6 Age
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