VARIABLE GEOMETRY THRUSTER

TURBOMACHINE EXHAUST CASE

VARIABLE GEOMETRY THRUSTER

Variable geometry thruster

System for controlling speed transition and thrust vectorisation in a multiple-shaped nozzle by secondary injection

Generation of a Pulsed Jet by Jet Vectoring Through a Nozzle with Multiple Outlets

Combustion-powered flow control actuator with heated walls

STRUCTURAL FRAME INTEGRATED WITH VARIABLE-VECTORING FLOW CONTROL FOR USE IN TURBINE SYSTEMS

MAGNETIC GAS ENGINE AND METHOD OF EXTRACTING WORK

Variable geometry thruster

Coanda device for a round exhaust nozzle

Exhaust plume cooling using periodic interruption of exhaust gas flow to form ambient air entraining vortices

Methods of creating fluidic barriers in turbine engines

Jet noise suppressor

Structural frame integrated with variable-vectoring flow control for use in turbine systems

Magnetic Gas Engine and Method of Extracting Work

Nozzle for an aircraft turboprop engine with an unducted fan

Method and apparatus for variable exhaust nozzle exit area

Generation of a pulsed jet by jet vectoring through a nozzle with multiple outlets

System of support thrust from wasted exhaust

Method and thermal reactor for single-valve propulsion with multiple injections and combustions per rotation cycle

Flow control device for a three stream turbofan engine

System, apparatus, and method for a virtual blocker

Primary cowl of a turbofan comprising a rotating ring having micro-jets

Rocket Propulsion Systems, and Related Methods

System and method for improving the efficiency of a jet engine

Method and apparatus for nozzle thrust vectoring

TURBOFAN ENGINE WITH CONVERGENT - DIVERGENT EXHAUST NOZZLE

Reflex annular vent nozzle

Exhaust nozzle of a gas turbine engine

Gas turbine engine exhaust nozzle cooling valve

Synthetic jet apparatus

Apparatus for controlling a boundary layer in a diffusing flow path of a power generating machine

Synthetic Jet Ejector With Sealed Motor

Flight vehicle, propulsion system and thrust vectoring system

Systems and Methodologies for Preventing Dust and Particle Contamination of Synthetic Jet Ejectors

SYSTEM AND METHOD FOR A GAS TURBINE EXHAUST DIFFUSER

Systems And Methodologies For Preventing Dust and Particle Contamination of Synthetic Jet Ejectors

Method and device to increase thrust and efficiency of jet engine

Arrangement for controlling fluid jets injected into a fluid stream of a bleed air discharge nozzle

Thrust vectoring apparatus for a jet engine, corresponding jet engine, thrust vectoring method and upgrading method for a jet engine

Gas turbine engine system providing simulated boundary layer thickness increase

Arrangement for controlling fluid jets injected into a fluid stream

Generation of a pulsed jet by jet vectoring through a nozzle with multiple outlets

System and apparatus for vectoring nozzle exhaust plume from a nozzle

Magnetic gas engine and method of extracting work

Jet engine nacelle for an aircraft and aircraft comprising such a nacelle

Pulse detonation/deflagration apparatus and related methods for enhancing DDT wave production

Device for enhancing efficiency of an energy extraction system

Nacelle with a displacement device for aircraft jet engine and aircraft including such nacelle

PROCESS FOR REVERSING THE THRUST PRODUCED BY A PROPULSION UNIT OF AN AIRCRAFT, DEVICE FOR ITS IMPLEMENTATION, NACELLE EQUIPPED WITH SAID DEVICE

Nozzle assembly with flow conduits

Arrangement for controlling fluid jets injected into a fluid stream

Thrust vectoring system and method

Air reinjection compressor

Flow distribution system for inlet flow control

Fluidic vectoring for exhaust nozzle

Arrangement for controlling fluid jets injected into a fluid stream

Method and device to increase thrust and efficiency of jet engine

System, method, and apparatus for control input prediction and state verification of fluidic vectoring exhaust in high performance aircraft

Turbofan gas turbine engine and nacelle arrangement

Gas turbine engine providing simulated boundary layer thickness increase

Device for Controlling a Gas Flow, a Jet Engine Comprising the Device and an Aircraft Comprising the Device

Combustion nozzle fluidic injection assembly

Turbocharger for a vehicle with a coanda device

Outlet nozzle for a jet engine, an aircraft comprising the outlet nozzle and a method for controlling a gas flow from the jet engine

Exhaust assembly forming a horizontal propulsion gas elbow in an aircraft

Method and system for flow control with arrays of dual bimorph synthetic jet fluidic actuators

Thrust orienting nozzle

Arrangement for controlling fluid jets injected into a fluid stream

Mixing-enhancement inserts for pulse detonation chambers

Magnetic gas engine and method of extracting work

Exhaust nozzle for an engine of a flying craft

Deflection system for a gas stream in a nozzle

Fluid vectoring nozzle

Yaw vectoring for exhaust nozzle

Rotary adjustable exhaust nozzle