Difference between revisions of "Pratt & Whitney Canada Corp. patent applications published on October 10th, 2024"
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+ | '''Summary of the patent applications from Pratt & Whitney Canada Corp. on October 10th, 2024''' | ||
+ | |||
+ | **Summary:** | ||
+ | The recent patents filed by the organization describe innovative technologies for gas turbine engines, including a system for removing fuel from a manifold during low-power mode, a method for adjusting the modulation characteristic of a bleed-off valve, and a rotary engine side housing with integrated coolant chamber. These patents aim to improve fuel efficiency, engine performance, and cooling capabilities in various applications such as power generation, aviation, and industrial machinery. | ||
+ | |||
+ | **Key Points of Patents:** | ||
+ | - System for removing fuel from a manifold during low-power mode. | ||
+ | - Dual manifold fuel supply system for efficient fuel management. | ||
+ | - Purging of fuel from the second manifold using combustor pressure. | ||
+ | - Method for adjusting modulation characteristic of a bleed-off valve. | ||
+ | - Utilizes setpoint configurations and adjustment factors based on operating conditions. | ||
+ | - Allows for precise control and optimization of the valve's performance. | ||
+ | - Rotary engine side housing with integrated coolant chamber. | ||
+ | - Plurality of posts for structural integrity and durability. | ||
+ | |||
+ | **Notable Applications:** | ||
+ | - Power generation plants | ||
+ | - Aircraft engines | ||
+ | - Industrial gas turbine applications | ||
+ | - Automotive industry for rotary engines | ||
+ | - Aerospace industry for aircraft engines | ||
+ | - Industrial machinery for high-performance engines | ||
+ | |||
+ | |||
+ | |||
+ | |||
==Patent applications for Pratt & Whitney Canada Corp. on October 10th, 2024== | ==Patent applications for Pratt & Whitney Canada Corp. on October 10th, 2024== | ||
Latest revision as of 05:46, 18 October 2024
Summary of the patent applications from Pratt & Whitney Canada Corp. on October 10th, 2024
- Summary:**
The recent patents filed by the organization describe innovative technologies for gas turbine engines, including a system for removing fuel from a manifold during low-power mode, a method for adjusting the modulation characteristic of a bleed-off valve, and a rotary engine side housing with integrated coolant chamber. These patents aim to improve fuel efficiency, engine performance, and cooling capabilities in various applications such as power generation, aviation, and industrial machinery.
- Key Points of Patents:**
- System for removing fuel from a manifold during low-power mode. - Dual manifold fuel supply system for efficient fuel management. - Purging of fuel from the second manifold using combustor pressure. - Method for adjusting modulation characteristic of a bleed-off valve. - Utilizes setpoint configurations and adjustment factors based on operating conditions. - Allows for precise control and optimization of the valve's performance. - Rotary engine side housing with integrated coolant chamber. - Plurality of posts for structural integrity and durability.
- Notable Applications:**
- Power generation plants - Aircraft engines - Industrial gas turbine applications - Automotive industry for rotary engines - Aerospace industry for aircraft engines - Industrial machinery for high-performance engines
Contents
- 1 Patent applications for Pratt & Whitney Canada Corp. on October 10th, 2024
- 1.1 ROTOR ASSEMBLY WITH COOLING CHANNELS SEPARATED BY RIBS FOR A ROTARY ENGINE (18132167)
- 1.2 AIRCRAFT ENGINE FLUID SYSTEM WITH BYPASS VALVE (18130643)
- 1.3 ROTOR ENGINE SIDE HOUSING AND METHOD FOR PRODUCING THE SAME (18132187)
- 1.4 SYSTEMS AND METHODS FOR ADJUSTING A MODULATION CHARACTERISTIC OF A BLEED-OFF VALVE OF A GAS TURBINE ENGINE (18130514)
- 1.5 METHOD OF OPERATING A GAS TURBINE ENGINE AT A LOW POWER CONDITION (18750320)
Patent applications for Pratt & Whitney Canada Corp. on October 10th, 2024
ROTOR ASSEMBLY WITH COOLING CHANNELS SEPARATED BY RIBS FOR A ROTARY ENGINE (18132167)
Main Inventor
Jérémie Barberger
AIRCRAFT ENGINE FLUID SYSTEM WITH BYPASS VALVE (18130643)
Main Inventor
Kashif MOHAMMED
ROTOR ENGINE SIDE HOUSING AND METHOD FOR PRODUCING THE SAME (18132187)
Main Inventor
Jérémie Barberger
SYSTEMS AND METHODS FOR ADJUSTING A MODULATION CHARACTERISTIC OF A BLEED-OFF VALVE OF A GAS TURBINE ENGINE (18130514)
Main Inventor
Louis DURANLEAU-HENDRICKX
METHOD OF OPERATING A GAS TURBINE ENGINE AT A LOW POWER CONDITION (18750320)
Main Inventor
Stephen TARLING