Inventor
SHARMA OM P
US23 patents
⚠️ This page may combine multiple inventors who share the name “SHARMA OM P”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
15 patentsUS5486091AJan 23, 1996
Gas turbine airfoil clocking
UNITED TECHNOLOGIES CORP81 citations95
US5525038AJun 11, 1996
Rotor airfoils to control tip leakage flows
UNITED TECHNOLOGIES CORP128 citations94
US7984607B2Jul 26, 2011
Gas turbine engine systems and related methods involving vane-blade count ratios greater than unity
UNITED TECHNOLOGIES CORP21 citations92
US7942632B2May 17, 2011
Variable-shape variable-stagger inlet guide vane flap
UNITED TECHNOLOGIES CORP20 citations92
US7413406B2Aug 19, 2008
Turbine blade with radial cooling channels
UNITED TECHNOLOGIES CORP20 citations89
US10619483B2Apr 14, 2020
Partially shrouded gas turbine engine fan
UNITED TECHNOLOGIES CORP5 citations73
US11519289B2Dec 6, 2022
Systems and methods for hybrid electric turbine engines
UNITED TECHNOLOGIES CORP2 citations72
US11199136B2Dec 14, 2021
Additively manufactured thermally insulating structure
UNITED TECHNOLOGIES CORP2 citations72
US11162416B2Nov 2, 2021
Attritable engine integrated with vehicle
UNITED TECHNOLOGIES CORP3 citations72
US11156156B2Oct 26, 2021
Gas turbine engine with a unitary structure and method for manufacturing the same
UNITED TECHNOLOGIES CORP3 citations72
US10808545B2Oct 20, 2020
Gas turbine engine fan blade, design, and fabrication
UNITED TECHNOLOGIES CORP2 citations72
US11242769B2Feb 8, 2022
Additively controlled surface roughness for designed performance
UNITED TECHNOLOGIES CORP0 citations62
US10907544B2Feb 2, 2021
Gas turbine engine inlet wall design
UNITED TECHNOLOGIES CORP0 citations62
US11136895B2Oct 5, 2021
Spiraling grooves as a hub treatment for cantilevered stators in compressors
UNITED TECHNOLOGIES CORP0 citations58
US10330010B2Jun 25, 2019
Compressor core inner diameter cooling
UNITED TECHNOLOGIES CORP0 citations52
RAYTHEON TECH CORP
4 patentsUS11655778B2May 23, 2023
Morphing structures for fan inlet variable vanes
RAYTHEON TECH CORP3 citations71
US11988140B2May 21, 2024
Gas turbine engine inlet wall design
RAYTHEON TECH CORP0 citations62
US11904405B2Feb 20, 2024
Additively controlled surface roughness for designed performance
RAYTHEON TECH CORP0 citations62
US12247529B2Mar 11, 2025
Morphing structures for fan inlet variable vanes
RAYTHEON TECH CORP0 citations61
SHARMA OM P
3 patentsUS8973374B2Mar 10, 2015
Blades in a turbine section of a gas turbine engine
SHARMA OM P7 citations82
US8468797B2Jun 25, 2013
Gas turbine engine systems and related methods involving vane-blade count ratios greater than unity
SHARMA OM P4 citations60
US8516793B2Aug 27, 2013
Gas turbine engine systems and related methods involving vane-blade count ratios greater than unity
SHARMA OM P0 citations50