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Category:F01D5/14
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Pages in category "F01D5/14"
The following 19 pages are in this category, out of 19 total.
1
- 17835091. GAS TURBINE ENGINE WITH AN AIRFOIL simplified abstract (General Electric Company)
- 18365118. GEOMETRIC APPROACH TO STRESS REDUCED INTRA-FLOW PATH SHROUDS FOR TUNING MODAL RESPONSES IN RAM AIR TURBINE ROTORS simplified abstract (HONEYWELL INTERNATIONAL INC.)
- 18476683. BLADE AND ROTOR simplified abstract (HONDA MOTOR CO., LTD.)
2
- 20240011399. BLADE WITH TIP RAIL COOLING simplified abstract (General Electric Company)
- 20240011401. TURBINE BLADE WITH MODAL RESPONSE ADAPTED TIP SHROUD simplified abstract (Power Systems Mfg., LLC)
- 20240044254. AIRFOIL ASSEMBLY WITH AN INTERNAL REINFORCEMENT STRUCTURE simplified abstract (General Electric Company)
- 20240052746. FAN BLADE OR VANE WITH IMPROVED BIRD IMPACT CAPABILITY simplified abstract (RTX Corporation)
- 20240052747. FAN BLADE OR VANE WITH IMPROVED BIRD IMPACT CAPABILITY simplified abstract (RTX Corporation)
B
- Blockchain patent applications on 22nd Mar 2024
- Blockchain patent applications on February 15th, 2024
- Blockchain patent applications on February 8th, 2024
- Blockchain patent applications on January 11th, 2024
- Blockchain patent applications on March 14th, 2024
- Blockchain patent applications on March 21st, 2024
- Blockchain patent applications on March 7th, 2024