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Category:F01D5/18
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This category has the following 29 subcategories, out of 29 total.
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Pages in category "F01D5/18"
The following 67 pages are in this category, out of 67 total.
1
- 17835091. GAS TURBINE ENGINE WITH AN AIRFOIL simplified abstract (General Electric Company)
- 17836023. TURBINE ENGINE WITH A BLADE simplified abstract (General Electric Company)
- 17836049. TURBINE ENGINE WITH A BLADE simplified abstract (General Electric Company)
- 17958690. PLATFORM OUTSIDE DIAMETER CHANNEL FOR DUAL SUPPLY PRESSURE VANE APPLICATIONS simplified abstract (Raytheon Technologies Corporation)
- 17960230. TURBINE ENGINE WITH COMPONENT HAVING A COOLING HOLE WITH A LAYBACK SURFACE simplified abstract (General Electric Company)
- 18071121. GAS TURBINE ENGINE COMPONENT HAVING AN AIRFOIL WITH INTERNAL CROSS-RIBS simplified abstract (Raytheon Technologies Corporation)
- 18118365. AIRFOIL TIP ARRANGEMENT FOR GAS TURBINE ENGINE simplified abstract (Raytheon Technologies Corporation)
- 18118471. Airfoils with Axial Leading Edge Impingement Slots simplified abstract (Raytheon Technologies Corporation)
- 18118706. Airfoils with Mixed Skin Passageway Cooling simplified abstract (Raytheon Technologies Corporation)
- 18121049. ALTERING STRUCTURAL RESPONSE OF TWO-PIECE HOLLOW-VANE ASSEMBLY simplified abstract (Raytheon Technologies Corporation)
- 18121146. ALTERING STRUCTURAL RESPONSE OF TWO-PIECE HOLLOW-VANE ASSEMBLY BY CHANGING THE COVER COMPOSITION simplified abstract (Raytheon Technologies Corporation)
- 18295388. ENGINE COMPONENT WITH A COOLING SUPPLY CIRCUIT simplified abstract (General Electric Company)
- 18337841. AIRFOIL FOR A TURBINE ENGINE simplified abstract (General Electric Company)
- 18354774. TURBINE ENGINE WITH A BLADE simplified abstract (General Electric Company)
- 18377080. COOLING PASSAGE EXIT OPENING CROSS-SECTIONAL AREA REDUCTION FOR TURBINE SYSTEM COMPONENT simplified abstract (GENERAL ELECTRIC COMPANY)
- 18418909. TURBOMACHINE COOLING TRENCH simplified abstract (GENERAL ELECTRIC COMPANY)
- 18442719. INDUCER ASSEMBLY FOR A TURBINE ENGINE (General Electric Company)
- 18452901. CMC VANE WITH ROTATABLE BAFFLE DESIGN TO ACCOMMODATE RE-STAGGER (RTX Corporation)
- 18452912. BATHTUB SEAL INTEGRATED INTO CMC VANE LOAD PATH (RTX Corporation)
- 18453564. COMPOSITE COMPONENT HAVING AN ADDITIVELY PRINTED INNER PORTION (General Electric Company)
- 18463475. DIRT AND DUST FREE TURBINE VANE COOLING (RTX CORPORATION)
- 18480692. CMC AIRFOIL WITH CIRCUMVENTING COOLING PASSAGE (RTX Corporation)
- 18480698. CMC Airfoil with Cooling Passage Having Multi-Dimensional Plenum (RTX Corporation)
- 18486788. TURBINE BLADE WITH BOOMERANG SHAPED WALL COOLING PASSAGES (RTX Corporation)
- 18496256. CMC AIRFOIL WITH COOLING PASSAGE FORMED IN FIBER PLIES (RTX CORPORATION)
- 18496267. CMC Airfoil with Closed-Circuit Cooling Passage in Platform (RTX CORPORATION)
- 18599486. COMPONENT FOR A TURBINE ENGINE WITH A COOLING HOLE simplified abstract (General Electric Company)
- 18672309. BATHTUB SEAL FOR DAMPING CMC VANE PLATFORM (RTX Corporation)
- 18817394. GAS TURBINE ENGINE WITH CLUTCH ASSEMBLY (General Electric Company)
- 18888810. Internal Aluminization of Coated Substrates (RTX Corporation)
- 18966893. Airfoils with Lobed Cooling Cavities (RTX Corporation)
- 18973613. ALUMINUM-CHROMIUM OXIDE COATING AND METHOD THEREFOR (RTX Corporation)
2
- 20240011398. TURBINE COMPONENT HAVING PLATFORM COOLING CIRCUIT simplified abstract (Siemens Energy Global GmbH & Co. KG)
- 20240011399. BLADE WITH TIP RAIL COOLING simplified abstract (General Electric Company)
- 20240011400. AIRFOIL WITH BAFFLE HAVING FLANGE RING AFFIXED TO PLATFORM simplified abstract (Raytheon Technologies Corporation)
- 20240026795. COOLING CIRCUIT FOR A STATOR VANE BRAZE JOINT simplified abstract (General Electric Company)
- 20240035386. TURBINE BLADE SQUEALER TIP WALL WITH CHAMFERED SURFACE simplified abstract (Siemens Energy Global GmbH & Co. KG)
- 20240052745. RADIAL FAN WITH LEADING EDGE AIR INJECTION simplified abstract (Hamilton Sundstrand Corporation)
B
- Blockchain patent applications on April 11th, 2024
- Blockchain patent applications on April 18th, 2024
- Blockchain patent applications on April 4th, 2024
- Blockchain patent applications on February 15th, 2024
- Blockchain patent applications on February 1st, 2024
- Blockchain patent applications on February 22nd, 2024
- Blockchain patent applications on February 29th, 2024
- Blockchain patent applications on January 11th, 2024
- Blockchain patent applications on January 25th, 2024
- Blockchain patent applications on March 14th, 2024
- Blockchain patent applications on March 28th, 2024
- Blockchain patent applications on May 16th, 2024
G
R
- Raytheon technologies corporation (20240301796). Airfoils with Axial Leading Edge Impingement Slots simplified abstract
- Raytheon technologies corporation (20240301797). Airfoils with Mixed Skin Passageway Cooling simplified abstract
- Raytheon technologies corporation (20240301799). AIRFOIL TIP ARRANGEMENT FOR GAS TURBINE ENGINE simplified abstract
- Raytheon technologies corporation (20240309764). ALTERING STRUCTURAL RESPONSE OF TWO-PIECE HOLLOW-VANE ASSEMBLY simplified abstract
- Raytheon technologies corporation (20240309765). ALTERING STRUCTURAL RESPONSE OF TWO-PIECE HOLLOW-VANE ASSEMBLY BY CHANGING THE COVER COMPOSITION simplified abstract
- Raytheon technologies corporation (20240410283). AIRFOIL COOLING CIRCUIT
- Raytheon technologies corporation (20240410284). TURBINE VANE BAFFLE CHIMNEY
- RAYTHEON TECHNOLOGIES CORPORATION patent applications on December 12th, 2024
- Raytheon Technologies Corporation patent applications on September 12th, 2024
- Raytheon Technologies Corporation patent applications on September 19th, 2024
- Rtx corporation (20250067182). BATHTUB SEAL INTEGRATED INTO CMC VANE LOAD PATH
- Rtx corporation (20250067183). BATHTUB SEAL FOR DAMPING CMC VANE PLATFORM
- Rtx corporation (20250067185). CMC VANE WITH ROTATABLE BAFFLE DESIGN TO ACCOMMODATE RE-STAGGER
- RTX Corporation patent applications on February 27th, 2025