Inventor

Brandon Wayne Miller

Inventor
US

Overview

112→
Patents
2021–2026
Patent span
Mechanical engineering
Primary field (CPC F)

Patents· 112 as inventor

Public. Assignee & technology derived from the patent record. Each patent links to its LexDana page.

F02Cprimary
F02CGas-turbine plants20%
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants19%
Y02TClimate change mitigation technologies related to transportation11%
F01DNon-positive displacement machines or engines, e.g. steam turbines11%
F02KJet-propulsion plants11%
B64DEquipment for fitting in or to aircraft7%
F04DNon-positive-displacement pumps5%
B01DSeparation3%
B64CAeroplanes2%
F02MSupplying combustion engines in general with combustible mixtures or constituents thereof1%
PatentTitleYear
12,595,066Blended wing aircraft202612,584,445Gas turbine engine and fuel cell assembly202612,584,455Airflow mixer assembly for a gas turbine engine202612,577,925Gas turbine engine with third stream202612,571,327Liquid fluid systems including phase detection sensors for turbine engines202612,571,358Gas turbine engine with third stream202612,565,855Gas turbine engine202612,560,132Gas turbine engine with third stream202612,560,125Gas turbine engine with acoustic spacing of the fan blades and outlet guide vanes202612,523,188Gas turbine engine with third stream202612,516,647Gas turbine engine with third stream202612,510,021Fuel oxygen reduction unit for prescribed operating conditions202512,510,104Gas turbine engine with acoustic spacing of the fan blades and outlet guide vanes202512,497,904Gas turbine engine202512,497,934Gas turbine engine with acoustic spacing of the fan blades and outlet guide vanes202512,497,923Gas turbine engine with acoustic spacing of the fan blades and outlet guide vanes202512,486,817Gas turbine engine with third stream202512,467,408Ice reduction mechanism for turbofan engine202512,448,925System and method for detecting and reducing torque in a turbine engine202512,448,134Blended wing aircraft202512,428,962Gas turbine engine with acoustic spacing of the fan blades and outlet guide vanes202512,429,067Gas turbine engine with acoustic spacing of the fan blades and outlet guide vanes202512,421,854Gas turbine engine with acoustic spacing of the fan blades and outlet guide vanes202512,421,896Gas turbine engine having a heat exchanger located in an annular duct202512,416,261Gas turbine engine202512,410,752System and method of detecting an airflow fault condition202512,410,763Gas turbine engine with third stream202512,385,430Gas turbine engine with forward swept outlet guide vanes202512,372,029Gas turbine engine having cooling systems202512,372,030Turbine engine having a fire box202512,338,837Turbofan engine having angled inlet pre-swirl vanes202512,313,022Gas turbine engine having a heat exchanger located in an annular duct202512,313,021Outer nacelle with inlet guide vanes and acoustic treatment202512,292,017Gas turbine engine with acoustic spacing of the fan blades and outlet guide vanes202512,286,927Vehicle with energy conversion system202512,270,340Gas turbine engine and fuel cell assembly202512,270,342Thermal management system for an engine202512,264,588Liquid fluid systems including phase detection sensors for turbine engines202512,261,334Gas turbine engine and fuel cell assembly202512,228,037Guide vane assembly with fixed and variable pitch inlet guide vanes202512,221,980Gas turbine engine with variable pitch inlet pre-swirl features202512,209,557Gas turbine engine with forward swept outlet guide vanes202512,173,658Accessory gearbox for a turbine engine202412,168,956Ice reduction mechanism for turbofan engine202412,139,270Aircraft thermal transport system and method202412,134,971Trunnion retention for a turbine engine202412,116,929Bleed flow assembly for a gas turbine engine202412,104,499System and method of regulating thermal transport bus pressure202412,103,702Removeable fuselage shield for an aircraft202412,085,019Object direction mechanism for turbofan engine202412,085,024High fan tip speed engine202412,071,897Gas turbine fluid manifold assembly having an adjustable length bypass conduit to attenuate dynamics202412,044,194Propulsion system architecture202412,044,182Shaft power transfer for a multi spool gas turbine engine202412,031,504Gas turbine engine with third stream202412,017,751Inlet for unducted propulsion system202412,018,594Pericritical fluid systems for turbine engines202412,012,898Gas turbine engine with acoustic spacing of the fan blades and outlet guide vanes202411,994,066Thermal management system202411,982,497Heat exchanger and leak detection system202411,976,562System for controlling blade clearances within a gas turbine engine202411,965,424Electronic overspeed protection system and method202411,946,415Waste heat recovery system202411,945,600Fuel delivery system having a fuel oxygen reduction unit202411,898,518Aircraft and direct drive engine under wing installation202411,866,182Fuel delivery system having a fuel oxygen reduction unit202411,851,204Fuel oxygen conversion unit with a dual separator pump202311,814,174Layered fuselage shield202311,815,024Thermal management system202311,808,281Gas turbine engine with variable pitch inlet pre-swirl features202311,788,470Gas turbine engine thermal management202311,788,465Bleed flow assembly for a gas turbine engine202311,773,776Fuel oxygen reduction unit for prescribed operating conditions202311,767,790Object direction mechanism for turbofan engine202311,761,344Thermal management system202311,739,689Ice reduction mechanism for turbofan engine202311,725,526Turbofan engine having nacelle with non-annular inlet202311,724,814Embedded electric machine202311,725,584Heat engine with heat exchanger202311,702,958System and method of regulating thermal transport bus pressure202311,702,985Thermal management system202311,685,542Propulsion engine for an aircraft202311,655,768High fan up speed engine202311,591,965Thermal management system for transferring heat between fluids202311,585,354Engine having variable pitch outlet guide vanes202311,577,852Fuel oxygen conversion unit202311,572,838Accessory gearbox for a turbine engine202311,560,239Regenerative thermal management system202311,506,131Thermal management system202211,506,125Fluid manifold assembly for gas turbine engine202211,480,063Gas turbine engine with inlet pre-swirl features202211,447,263Fuel oxygen reduction unit control system202211,448,127Translating inlet for adjusting airflow distortion in gas turbine engine202211,421,627Aircraft and direct drive engine under wing installation202211,420,763Fuel delivery system having a fuel oxygen reduction unit202211,391,298Engine having variable pitch outlet guide vanes202211,391,211Waste heat recovery system202211,352,960Fuel oxygen reduction unit202211,319,085Fuel oxygen conversion unit with valve control202211,300,365Heat exchanger and leak detection system202211,286,853Cooling system202211,261,792Thermal management system with thermal bus for a gas turbine engine or aircraft202211,247,779Embedded electric machine202211,225,914Multi-directional gearbox deflection limiter for a gas turbine engine202211,225,975Gas turbine engine fan202211,193,671Fuel oxygen conversion unit with a fuel gas separator202111,186,382Fuel oxygen conversion unit202111,187,156Thermal management system202111,161,622Fuel oxygen reduction unit202111,156,128Embedded electric machine202111,148,824Fuel delivery system having a fuel oxygen reduction unit202111,143,104Thermal management system2021

Career & activity timeline

Assembled from patent assignee/location history and declaration credentials.

2021–2026Patents assigned to GEN ELECTRIC (111)· patent assignee history
2021–2026Based in US· patent location history
2025Patents assigned to GE AVIO SRL (1)· patent assignee history
2025Patents assigned to GENERAL ELECTRIC COMPANY POLSKA SP ZOO (1)· patent assignee history
2026Patents assigned to GENERAL ELECTRIC COMPANY (1)· patent assignee history
2026Patents assigned to GENERAL ELECTRIC DEUTSCHLAND HOLDING GMBH (1)· patent assignee history

Inventor activity

Assignee and location history derived from the patent record.

Assignees
AssigneePatentsSpan
GEN ELECTRIC1112021–2026
GE AVIO SRL12025
GENERAL ELECTRIC COMPANY12026
GENERAL ELECTRIC COMPANY POLSKA SP ZOO12025
GENERAL ELECTRIC DEUTSCHLAND HOLDING GMBH12026
Locations
LocationPatentsSpan
US1122021–2026