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EP3812548A1
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Stage of a turbomachine compressor with an optimised inner end wall
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EP3693609A1
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Measurement of total pressure and total temperature in a turbine engine
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EP3674586A1
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Valve
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EP3671091A1
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Fuel-oil heat exchanger
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EP3640480A1
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Pump assembly of a lubricating unit of an aircraft turbine engine comprising a piezoelectric generator
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EP3633154A1
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Blade of an aircraft turbomachine including at least one pressure sensor
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BE1027594A1
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Device for lifting a mechanical part
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BE1027565A1
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Tooling for holding a blade during its friction welding to a rotor element of an aircraft turbomachine
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EP3623606A1
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Multi-fluid heat exchanger matrix
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EP3623772A1
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Measuring system for a turbine engine
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EP3617518A1
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Pump of turbomachine
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BE1027483A1
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System and method of quality control of manufactured parts
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BE1027469A1
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TURBOMACHINE ARCHITECTURE WITH ACCELERATED BOOSTER
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BE1027463A1
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Micro-percussion marking tool, machine tool comprising a marking tool and micro-percussion marking method
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BE1027459A1
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Stage of a compressor of an aircraft turbomachine
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BE1027453A1
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GEAR PUMP
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BE1027431A1
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Turbomachinery test bench depolluted
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BE1027399A1
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Magnetic valve device
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EP3599453A2
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Turbomachine test bench
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EP3594503A1
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Turbine engine
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