Inventor · disambiguated record
Catherine Pikovsky
Also filed as: PIKOVSKY CATHERINE
12 granted patents·1 pending application·25 citations·filing 2014–2020
85Inventor score
Top patents by PatentIndex Score
13 records- 0191US10364881B2Turbine engine module comprising a casing around a device with a cover for recovering lubricating oilSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Jul 30, 2019·12 cites·6 claims
- 0286US11754342B2Bypass air/fluid heat exchanger, method for manufacturing same and turbofan engine provided with such exchangerSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Sep 12, 2023·2 cites·11 claims
- 0382US11686249B2Turbine engine comprising a heat exchanger in the secondary pathSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Jun 27, 2023·3 cites·11 claims
- 0482US10174634B2Device and method for lubricating a turbomachine rolling bearingSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Jan 8, 2019·4 cites·12 claims
- 0581US11346247B2Turbine engine including a heat exchanger formed in a platformSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted May 31, 2022·2 cites·10 claims
- 0676US11639665B2Turbomachine comprising a heat exchanger in the secondary pathSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted May 2, 2023·1 cites·8 claims
- 0757US12025018B2Turbine arrangement incorporating an oil recovery circumferential troughSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Jul 2, 2024·0 cites·9 claims
- 0851US10012110B2Turbomachine assembly comprising two bodies and means for guiding a fluid flowing from one body to the otherSNECMA·Filed 2014·Granted Jul 3, 2018·1 cites·8 claims
- 0948US10738654B2Lubricating-oil collection cap for turbomachine equipmentSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Aug 11, 2020·0 cites·24 claims
- 1045US12180912B2Turbine engine comprising a heat exchanger consisting of at least one deck between vanesSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Dec 31, 2024·0 cites·7 claims
- 1145US2020240641A1Turbomachine, such as an aircraft turbojet engineSAFRAN AIRCRAFT ENGINES·Filed 2020·Application pending·0 cites
- 1244US11499439B2Double flow turbojet including an intermediate flow path dedicated to supplying with air via radial arms an exhaust casing of this turbojetSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Nov 15, 2022·0 cites·6 claims
- 1335US11326472B2Turbine engine comprising means for axially homogenising the temperature of an inner ring of a roller bearingSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted May 10, 2022·0 cites·14 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →