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Category:F01D5/30
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Pages in category "F01D5/30"
The following 20 pages are in this category, out of 20 total.
1
- 17769617. ASSEMBLY FOR A TURBOMACHINE BLADE, COMPRISING A FASTENER, DEFINING A POCKET, AND A SHIM ADAPTED TO BE RECEIVED IN THE POCKET AT THE SAME TIME AS A ROOT OF THE BLADE simplified abstract (SAFRAN AIRCRAFT ENGINES)
- 18071060. MACHINABLE COATING FOR CMC AND METAL INTERFACE IN A TURBINE SECTION simplified abstract (Raytheon Technologies Corporation)
- 18081844. ROTOR ASSEMBLY FOR A GAS TURBINE ENGINE simplified abstract (General Electric Company)
- 18088957. COMPOSITE AIRFOIL ASSEMBLY HAVING A DOVETAIL PORTION simplified abstract (GENERAL ELECTRIC COMPANY)
- 18088990. COMPOSITE AIRFOIL ASSEMBLY HAVING A DOVETAIL PORTION simplified abstract (GENERAL ELECTRIC COMPANY)
- 18171836. TURBINE ENGINE WITH A BLADE ASSEMBLY HAVING A DOVETAIL simplified abstract (General Electric Company)
- 18210347. METHODS AND APPARATUSES FOR BLADE LOCKING (General Electric Company)
- 18295408. TURBINE BLADE AND ASSEMBLY WITH DOVETAIL ARRANGEMENT FOR ENLARGED ROTOR GROOVE simplified abstract (General Electric Company)
- 18575954. FOIL, ROTOR BLADE, ASSEMBLY FOR A TURBOMACHINE ROTOR AND ROTOR simplified abstract (SAFRAN AIRCRAFT ENGINES)
- 18662043. METHOD FOR TURBINE BLADE AND ASSEMBLY WITH DOVETAIL ARRANGEMENT FOR ENLARGED ROTOR GROOVE simplified abstract (GE Infrastructure Technology LLC)
- 18817394. GAS TURBINE ENGINE WITH CLUTCH ASSEMBLY (General Electric Company)