Inventor
RODRIGUEZ JOSE L
US23 patents
⚠️ This page may combine multiple inventors who share the name “RODRIGUEZ JOSE L”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
SIEMENS ENERGY GLOBAL GMBH & CO KG
7 patentsUS12018591B2Jun 25, 2024
Ring segment assembly in gas turbine engine
SIEMENS ENERGY GLOBAL GMBH & CO KG0 citations55
US11873733B2Jan 16, 2024
Turbine blade in gas turbine engine
SIEMENS ENERGY GLOBAL GMBH & CO KG0 citations51
US11992875B2May 28, 2024
Investment casting core with cooling feature alignment guide and related methods
SIEMENS ENERGY GLOBAL GMBH & CO KG0 citations50
US11759850B2Sep 19, 2023
Manufacturing aligned cooling features in a core for casting
SIEMENS ENERGY GLOBAL GMBH & CO KG0 citations49
US11371361B2Jun 28, 2022
Turbine blade and corresponding servicing method
SIEMENS ENERGY GLOBAL GMBH & CO KG0 citations46
US12241400B2Mar 4, 2025
Waste heat recovery system
SIEMENS ENERGY GLOBAL GMBH & CO KG0 citations40
US11319818B2May 3, 2022
Airfoil for a turbine engine incorporating pins
SIEMENS ENERGY GLOBAL GMBH & CO KG0 citations40
RODRIGUEZ JOSE L
6 patentsUS9217369B2Dec 22, 2015
Compressor inlet manifold for a gas turbine engine
RODRIGUEZ JOSE L8 citations82
US9091171B2Jul 28, 2015
Temperature control within a cavity of a turbine engine
RODRIGUEZ JOSE L12 citations82
US8894361B2Nov 25, 2014
Gas turbine compressor inlet with reduced flow distortion
RODRIGUEZ JOSE L9 citations77
US10012098B2Jul 3, 2018
Mid-section of a can-annular gas turbine engine to introduce a radial velocity component into an air flow discharged from a compressor of the mid-section
RODRIGUEZ JOSE L2 citations71
US9279339B2Mar 8, 2016
Turbine engine temperature control system with heating element for a gas turbine engine
RODRIGUEZ JOSE L0 citations40
US9134029B2Sep 15, 2015
Radial midframe baffle for can-annular combustor arrangement having tangentially oriented combustor cans
RODRIGUEZ JOSE L0 citations40
SIEMENS ENERGY INC
3 patentsUS10047636B2Aug 14, 2018
Gas turbine diffuser outer diameter and inner diameter wall strips for turbine exhaust manifold pressure oscillation reduction
SIEMENS ENERGY INC3 citations70
US9982893B2May 29, 2018
Combustor arrangement including flow control vanes
SIEMENS ENERGY INC2 citations69
US9810099B2Nov 7, 2017
Turbine exhaust cylinder strut strip for shock induced oscillation control
SIEMENS ENERGY INC0 citations38