Inventor

CHANDLER JESSE M

US115 patents

⚠️ This page may combine multiple inventors who share the name “CHANDLER JESSE M”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

CHANDLER JESSE M

UNITED TECHNOLOGIES CORP

Reverse core engine with thrust reverser

Idler gear connection for multi-stage variable vane actuation

Direct drive aft fan engine

Exhaust duct for turbine forward of fan

Intercooled cooling air tapped from plural locations

Engine with nose cone heat exchanger and radially outer discharge

Stabilizer sacrificial surfaces

Offset core engine architecture

Dual filtration particle separator

Tandem thrust reverser with sliding rails

Bypass duct heat exchanger with controlled fan

Nose cone assembly and method of circulating air in a gas turbine engine

Stabilizer with structural box and sacrificial surfaces

Intercooled cooling air with dual pass heat exchanger

Thermal management system and method of circulating air in a gas turbine engine

Tandem thrust reverser with multi-point actuation

Wide fuselage aircraft with increased boundary layer ingestion

Integrated nozzle and plug

Box wing with angled gas turbine engine cores

Gas turbine engine having fan rotor driven by turbine exhaust and with a bypass

Cable drive system for variable vane operation

Harmonic drive for shaft driving multiple stages of vanes via gears

Gas turbine engine with distributed fans

Full ring sliding nacelle with thrust reverser

Aft counter-rotating boundary layer ingestion engine

Boundary layer excitation aft fan gas turbine engine

Aft fan counter-rotating turbine engine

Turbine engine with guide vanes forward of its fan blades

Hybrid electric turbine engine

Active clearance control for gas turbine engine

Dedicated fans for boundary layer ingestion

Firewall mount hub

Electrical and mechanical connections through firewall

Engine bleed air system with waste gate valve for compressor surge management

Intercooled cooling air with plural heat exchangers

Gas turbine nacelle ventilation manifold having a circumferential varying cross-sectional area

Twin shafts driving adjacent fans for aircraft propulsion

Double propulsor imbedded in aircraft tail with single core engine

Pusher fan engine with in wing configuration

Electric actuation for variable vanes

Active clearance control for gas turbine engine

Gas turbine engine with paired distributed fan sets

Off-axis electric actuation for variable vanes

Direct drive aft fan engine

Gas turbine engine with plural accessory air paths

RAYTHEON TECH CORP

Harmonic drive for shaft driving multiple stages of vanes via gears

Engine with intercooler

Heat exchanger(s) for recovering water and/or heat energy from turbine engine combustion products

RTX CORP

Thrust reverser in condenser exit duct

Circumferential flow condenser arrangement for an aircraft propulsion system