[[Category:F02C3/10]]
[[Category:F01D15/10]]
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2 KB (235 words) - 06:40, 31 March 2025
[[Category:F02C3/107]]
[[Category:F02C3/10]]
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3 KB (496 words) - 09:52, 1 February 2024
[[Category:F01D15/10]]
[[Category:F02C3/113]]
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1 KB (211 words) - 07:26, 19 December 2024
[[Category:B64D27/10]]
[[Category:F02C3/14]]
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2 KB (233 words) - 12:01, 18 April 2025
[[Category:B64D27/10]]
[[Category:F02C3/14]]
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2 KB (233 words) - 09:32, 22 April 2025
...airflow ratio between 3.5 and 100 and a core bypass ratio between 0.1 and 10. the thrust to power airflow ratio is a ratio of airflow through a bypass p
[[Category:F02C3/06]]
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2 KB (330 words) - 12:01, 18 April 2025
...airflow ratio between 3.5 and 100 and a core bypass ratio between 0.1 and 10. The thrust to power airflow ratio is a ratio of airflow through a bypass p
[[Category:F02C3/06]]
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2 KB (330 words) - 09:32, 22 April 2025
...airflow ratio between 3.5 and 100 and a core bypass ratio between 0.1 and 10, wherein the thrust to power airflow ratio is a ratio of an airflow through
[[Category:F02C3/06]]
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2 KB (311 words) - 08:52, 18 February 2025
* Reduction of particles/kg of nvPM in the exhaust by 10-70%
...method comprises operating the gas turbine engine such that a reduction of 10-70% in an average of particles/kg of nvPM in the exhaust of the gas turbine
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3 KB (506 words) - 06:57, 28 June 2024
...0]] (2), [[:Category:B28B7/00|B28B7/00]] (1), [[:Category:F01K23/10|F01K23/10]] (1)
IPC Code(s): B64D27/24, F01D15/10
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23 KB (3,562 words) - 04:05, 19 September 2024
[[Category:F02C3/067]]
[[Category:F02C3/10]]
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5 KB (786 words) - 03:52, 16 April 2024
...s Corporation has applied for patents in the areas of [[:Category:F02C3/30|F02C3/30]] (6), [[:Category:F01D5/18|F01D5/18]] (2), [[:Category:C04B35/628|C04B3
[[:Category:CPC_F02C3/30|F02C3/30]] (5), [[:Category:CPC_C04B35/80|C04B35/80]] (2), [[:Category:CPC_F01D5/
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27 KB (4,042 words) - 09:18, 19 September 2024
...airflow ratio between 3.5 and 100 and a core bypass ratio between 0.1 and 10.
...airflow ratio between 3.5 and 100 and a core bypass ratio between 0.1 and 10, wherein the thrust to power airflow ratio is a ratio of an airflow through
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4 KB (615 words) - 05:01, 1 October 2024
...airflow ratio between 3.5 and 100 and a core bypass ratio between 0.1 and 10.
...airflow ratio between 3.5 and 100 and a core bypass ratio between 0.1 and 10, wherein the thrust to power airflow ratio is a ratio of an airflow through
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4 KB (665 words) - 03:18, 9 February 2024
== Top 10 Technology Areas ==
* [[:Category:CPC_F02C3/04|F02C3/04]] (GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLIN
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8 KB (1,087 words) - 01:11, 21 July 2024
* [[:Category:CPC_B60L2200/10|B60L2200/10]] (No explanation available)
** [[:Category:CPC_F02C3/20|F02C3/20]] (No explanation available): 1 patents
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12 KB (1,405 words) - 02:37, 17 July 2024
...01B3/04]] (3), [[:Category:F01D21/00|F01D21/00]] (2), [[:Category:F02C3/30|F02C3/30]] (2), [[:Category:F01D9/04|F01D9/04]] (2), [[:Category:F01D5/18|F01D5/1
[[:Category:CPC_C01B3/042|C01B3/042]] (2), [[:Category:CPC_F02C3/30|F02C3/30]] (2), [[:Category:CPC_B01J6/008|B01J6/008]] (1), [[:Category:CPC_B22F10
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21 KB (3,304 words) - 01:12, 13 December 2024
* The engine also has a core bypass ratio between 0.1 and 10.
...airflow ratio between 3.5 and 100 and a core bypass ratio between 0.1 and 10, wherein the thrust to power airflow ratio is a ratio of an airflow through
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4 KB (672 words) - 08:57, 27 September 2024
[[Category:F02C3/30]]
[[Category:F23R3/10]]
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3 KB (498 words) - 09:17, 19 September 2024
...airflow ratio between 3.5 and 100 and a core bypass ratio between 0.1 and 10.
...airflow ratio between 3.5 and 100 and a core bypass ratio between 0.1 and 10, wherein the thrust to power airflow ratio is a ratio of an airflow through
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5 KB (718 words) - 04:25, 1 October 2024
