Inventor
RIVERS JONATHAN M
US22 patents
⚠️ This page may combine multiple inventors who share the name “RIVERS JONATHAN M”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
ROLLS ROYCE NAM TECH INC
12 patentsUS12286930B1Apr 29, 2025
Turbine engine fan case with bleed air for tip injection and heat exchanger cooling
ROLLS ROYCE NAM TECH INC2 citations74
US11965528B1Apr 23, 2024
Adjustable air flow plenum with circumferential movable closure for a fan of a gas turbine engine
ROLLS ROYCE NAM TECH INC3 citations74
US12085021B1Sep 10, 2024
Adjustable air flow plenum with movable closure for a fan of a gas turbine engine
ROLLS ROYCE NAM TECH INC2 citations72
US12078070B1Sep 3, 2024
Adjustable air flow plenum with sliding doors for a fan of a gas turbine engine
ROLLS ROYCE NAM TECH INC2 citations72
US12286936B1Apr 29, 2025
Adjustable fan track liner with groove array active fan tip treatment for distortion tolerance
ROLLS ROYCE NAM TECH INC0 citations51
US12258870B1Mar 25, 2025
Adjustable fan track liner with slotted array active fan tip treatment for distortion tolerance
ROLLS ROYCE NAM TECH INC0 citations51
US12215712B1Feb 4, 2025
Adjustable fan track liner with dual grooved array active fan tip treatment for distortion tolerance
ROLLS ROYCE NAM TECH INC0 citations51
US12209541B1Jan 28, 2025
Adjustable fan track liner with dual slotted array active fan tip treatment for distortion tolerance
ROLLS ROYCE NAM TECH INC0 citations51
US12209502B1Jan 28, 2025
Active fan tip treatment using rotating drum array with axial channels in fan track liner for distortion tolerance
ROLLS ROYCE NAM TECH INC0 citations51
US12168983B1Dec 17, 2024
Active fan tip treatment using rotating drum array in fan track liner with axial and circumferential channels for distortion tolerance
ROLLS ROYCE NAM TECH INC0 citations51
US11970985B1Apr 30, 2024
Adjustable air flow plenum with pivoting vanes for a fan of a gas turbine engine
ROLLS ROYCE NAM TECH INC0 citations51
US12331660B1Jun 17, 2025
Vane assemblies with overlapping band couplings in gas turbine engines
ROLLS ROYCE NAM TECH INC0 citations45
ROLLS ROYCE CORP
8 patentsUS9932840B2Apr 3, 2018
Rotor for a gas turbine engine
ROLLS ROYCE CORP10 citations82
US9470097B2Oct 18, 2016
Airfoil with leading edge reinforcement
ROLLS ROYCE CORP4 citations71
US9739158B2Aug 22, 2017
Attachment feature of a gas turbine engine blade having a curved profile
ROLLS ROYCE CORP3 citations63
US11060527B2Jul 13, 2021
Thrust ring and rotor fan system with passive leading edge slats
ROLLS ROYCE CORP0 citations61
US10605257B2Mar 31, 2020
Thrust-ring and rotor fan system
ROLLS ROYCE CORP0 citations40
US10156244B2Dec 18, 2018
Fan assembly
ROLLS ROYCE CORP0 citations40
US9759095B2Sep 12, 2017
Gas turbine engine access panel
ROLLS ROYCE CORP0 citations40
US9568009B2Feb 14, 2017
Gas turbine engine flow path geometry
ROLLS ROYCE CORP0 citations40