Raytheon Technologies Corporation patent applications published on May 30th, 2024
Summary of the patent applications from Raytheon Technologies Corporation on May 30th, 2024
Raytheon Technologies Corporation has recently filed patents for innovative technologies related to aircraft landing control systems, gas turbine engine components, and turbine stator vanes.
Summary: - The first patent application describes a system for controlling thrust reversers and brakes during aircraft landings, enhancing safety and efficiency. - The second patent application focuses on gas turbine engine components made of ceramic matrix composites, improving performance and durability. - The third patent application introduces a system for re-staggering and aligning static stator vanes in turbine systems, solving alignment issues. - The fourth patent application presents a composite seal material for gas turbine engines, offering enhanced wear resistance and longevity.
Notable Applications:
- Automated control system for aircraft landings
- Gas turbine engine components with ceramic matrix composites
- Turbine stator vanes with sacrificial material for alignment adjustments
- Composite seal material for gas turbine engines.
Contents
- 1 Patent applications for Raytheon Technologies Corporation on May 30th, 2024
- 1.1 SLOT WITH COATING AND METHOD OF COATING A SLOT (18071055)
- 1.2 FIXTURE WITH GROOVES FOR PROCESSING CMC ARTICLE (18070962)
- 1.3 EDGE-SEALED FIXTURE FOR PROCESSING CMC (18071078)
- 1.4 MACHINABLE COATING FOR CMC AND METAL INTERFACE IN A TURBINE SECTION (18071060)
- 1.5 SEAL SLOT WITH COATING (18071070)
- 1.6 GAS TURBINE ENGINE WITH CARBON/CARBON COMPOSITE PISTON SEAL (17994182)
- 1.7 GAS TURBINE ENGINE WITH CARBON/CARBON COMPOSITE PISTON SEAL (17994188)
- 1.8 REMOVABLE LAYER TO ADJUST MOUNT STRUCTURE OF A TURBINE VANE FOR RE-STAGGER (18070978)
- 1.9 GAS TURBINE ENGINE COMPONENT HAVING AN AIRFOIL WITH INTERNAL CROSS-RIBS (18071121)
- 1.10 INTEGRATED THRUST REVERSER AND BRAKE CONTROL FOR AN AIRCRAFT (18071141)
Patent applications for Raytheon Technologies Corporation on May 30th, 2024
SLOT WITH COATING AND METHOD OF COATING A SLOT (18071055)
Main Inventor
Brian T. Hazel
FIXTURE WITH GROOVES FOR PROCESSING CMC ARTICLE (18070962)
Main Inventor
Raymond Surace
EDGE-SEALED FIXTURE FOR PROCESSING CMC (18071078)
Main Inventor
Evan B. Callaway
MACHINABLE COATING FOR CMC AND METAL INTERFACE IN A TURBINE SECTION (18071060)
Main Inventor
Daniel S. Rogers
SEAL SLOT WITH COATING (18071070)
Main Inventor
Raymond Surace
GAS TURBINE ENGINE WITH CARBON/CARBON COMPOSITE PISTON SEAL (17994182)
Main Inventor
Calvin Jay Winder
GAS TURBINE ENGINE WITH CARBON/CARBON COMPOSITE PISTON SEAL (17994188)
Main Inventor
Calvin Jay Winder
REMOVABLE LAYER TO ADJUST MOUNT STRUCTURE OF A TURBINE VANE FOR RE-STAGGER (18070978)
Main Inventor
Robert A. White, III
GAS TURBINE ENGINE COMPONENT HAVING AN AIRFOIL WITH INTERNAL CROSS-RIBS (18071121)
Main Inventor
James T. Roach
INTEGRATED THRUST REVERSER AND BRAKE CONTROL FOR AN AIRCRAFT (18071141)
Main Inventor
David Wasselin
