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公开(公告)号:US20240200491A1
公开(公告)日:2024-06-20
申请号:US18407648
申请日:2024-01-09
Applicant: RTX CORPORATION
Inventor: Edward Thomas Rocco , Danbing Seto , Coy Bruce Wood , Liang Tang
CPC classification number: F02C3/30 , F02C3/22 , F02C7/185 , F05D2220/323 , F05D2260/211 , F05D2260/213 , F05D2260/2322 , F05D2260/607 , F05D2260/80 , F05D2270/3015
Abstract: A propulsion system for an aircraft includes a hydrogen fuel system, a water recovery system and a water pressure and quantity monitoring system. The water recovery system uses a condenser to extract water from an exhaust gas flow. The water pressure and quantity monitoring system measures water pressures and quantities at various locations in the water recovery system to assess the health and efficiency of the water recovery/supply system and the propulsion system.
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公开(公告)号:US11860124B2
公开(公告)日:2024-01-02
申请号:US17666009
申请日:2022-02-07
Applicant: RTX Corporation
Inventor: Edward Thomas Rocco , Danbing Seto
CPC classification number: G01N27/74 , G01N33/2888
Abstract: A method to effectively utilize an oil debris monitor to provide advanced warning to mechanical system failures in a high noise system by adapting detection and annunciation algorithms to the background noise in a system that includes collecting I and Q channel data from a sensor; processing the I and Q channel data to both calculate a noise based (RMS adjusted) detection threshold and to identify a ferrous and nonferrous signal; processing the ferrous and nonferrous signals to determine signal peaks above the RMS adjusted detection threshold; adjusting a detection threshold if more signal peaks observed than allowable particles in a given time window; transmitting the detection threshold previously determined to particle detection, rate limit adjustment, detectability algorithms, and estimated mass loss accumulation.
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公开(公告)号:US20250067625A1
公开(公告)日:2025-02-27
申请号:US18238051
申请日:2023-08-25
Applicant: RTX Corporation
Inventor: Jeremiah C. Lee , William K. Donat , Scott Goyette , Danbing Seto
Abstract: An in-situ system for a gas turbine engine blade inspection including a sensor system configured to capture images of a forward surface of at least one gas turbine engine blade; a processor coupled to the sensor system, the processor configured to determine damage to the at least one gas turbine engine blade based on image analytics; and a tangible, non-transitory memory configured to communicate with the processor, the tangible, non-transitory memory having instructions stored therein that, in response to execution by the processor, cause the processor to perform operations comprising receiving, by the processor, data for the forward surface of at least one gas turbine engine blade from the sensor system; and determining, by the processor, surface damage responsive to the light source.
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公开(公告)号:US20250067194A1
公开(公告)日:2025-02-27
申请号:US18238065
申请日:2023-08-25
Applicant: RTX Corporation
Inventor: Jeremiah C. Lee , David L. Lincoln , Scott Goyette , Zaffir A. Chaudhry , Danbing Seto
IPC: F01D21/00
Abstract: An in-situ system for a gas turbine engine blade inspection including a sensor system configured to capture images of a forward surface of at least one gas turbine engine blade; a processor coupled to the sensor system, the processor configured to determine damage to the at least one gas turbine engine blade based on video analytics; and a tangible, non-transitory memory configured to communicate with the processor, the tangible, non-transitory memory having instructions stored therein that, in response to execution by the processor, cause the processor to perform operations comprising receiving, by the processor, data for the forward surface of at least one gas turbine engine blade from the sensor system; determining, by the processor, a rotational speed of a fan; and determining, by the processor, a fan synchronization.
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公开(公告)号:US11840966B1
公开(公告)日:2023-12-12
申请号:US17990487
申请日:2022-11-18
Applicant: RTX Corporation
Inventor: Joshua Adams , Danbing Seto , Ramesh Rajagopalan
IPC: F02C9/00
CPC classification number: F02C9/00 , F05D2270/11 , F05D2270/20 , F05D2270/44 , F05D2270/71
Abstract: An engine parameter estimation tuning system includes an engine parameter estimator unit and a gas path analysis (GPA) unit. The engine parameter estimator unit includes an onboard model (OBM) configured to output estimated parameters based on operation of a gas turbine engine. The gas path analysis (GPA) unit includes a performance health monitor unit configured to adjust a long-term deterioration parameter independently from adjustment of a short-term tuning parameter to tune one or more targeted estimation parameters included in the estimated engine parameter. In this manner, the engine parameter estimation tuning system can realize the different time scales associated with uncertainties in an engine and accommodate them separately so that the estimated engine parameters become much more accurate.
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