Passive cooling system for control valve actuators within a negative pressure turbine enclosure using ambient cooling air

Disc axis adjusting mechanism in gas turbine

Clearance control system for a rotary machine and method of controlling a clearance

Three-dimensional printing process, swirling device and thermal management process

Systems relating to axial positioning turbine casings and blade tip clearance in gas turbine engines

Turbine casing false flange flow diverter

TIP CLEARANCE CONTROL METHOD

Shroud block segment for a gas turbine

Blade track assembly with turbine tip clearance control

CONJOINED GAS TURBINE INTERFACE SEAL

Interface device between two turbomachine elements

Piston seal ring

Dual source cooling air shroud arrangement for a gas turbine engine

Valve for gas turbine engine

Shroud arrangement for a gas turbine engine

Flow sleeve for thermal control of a double-wall turbine shell and related method

Rotor tip clearance

Turbine thermal clearance management system

TURBINE ENGINE SHUTDOWN TEMPERATURE CONTROL SYSTEM

Gas turbine engine tip clearance control

Gas turbine shroud assemblies

Blade track assembly with turbine tip clearance control

Turbine blade track assembly

Method and apparatus to improve heat transfer in turbine sections of gas turbines

Turbine shroud segment sealing

Active clearance control system with zone controls

Active turbine or compressor tip clearance control

Cooling structure for turbomachine

Variable outer air seal fluid control

TURBO-MACHINE WITH ACTIVE ELECTRICAL CLEARANCE CONTROL

Axial compressor and operation method of the same

Gas turbine casing thermal control device

Clearance control

Arrangement for connecting a duct to an air-distribution casing

Gas turbine thermal control and related method

METHODS AND SYSTEMS FOR OPERATING AN INTEGRATED ACTUATOR

Impingement plate for damping and cooling shroud assembly inter segment seals

Gas turbine engine component having platform trench

Blade outer air seal having anti-rotation feature

Flow conducting assembly for cooling the low-pressure turbine housing of a gas turbine jet engine

Turbomachine including horizontal joint heating and method of controlling tip clearance in a gas turbomachine

Active clearance control manifold system

Blade outer air seal with cooling features

Turbine casing comprising ring sector attachment means

Active clearance control for gas turbine engine

Blade outer air seal with cored passages

Method for controlling the clearance at the tips of blades of a turbine rotor

Turbine Shroud Cooling Assembly for a Gas Turbine System

Actuator mounting system and method of mounting

Systems for heating rotor disks in a turbomachine

Clearance control system for a gas turbine

GAS TURBINE ENGINE CASE WITH HEATING LAYER AND METHOD

Surface area augmentation of hot-section turbomachine component

Turbine Shell Having A Plate Frame Heat Exchanger

Method and apparatus to control part-load performance of a turbine

Low-ductility turbine shroud

Mounting apparatus for low-ductility turbine shroud

Active turbine tip clearance control system

Turbine component cooling with closed looped control of coolant flow

Gas turbine engine having a multi-variable closed loop controller for regulating tip clearance

Radial active clearance control for a gas turbine engine

Systems and methods for adjusting clearances in turbines

Systems and methods for adjusting clearances in turbines

Gas turbine engine lockout reduction

Gas turbine engine with structure for directing compressed air on a blade ring

Gas turbine engine component having wavy cooling channels with pedestals

Active clearance control system and method for gas turbine

Turbine blade tip clearance control

Gas Turbine

Turbine Shroud Impingement System with Bellows

Blade outer air seal assembly leading edge core configuration

Manufacturing of turbine shroud segment with internal cooling passages

Blade outer air seal with multi impingement plate assembly

GAS TURBINE ENGINE ACTIVE CLEARANCE CONTROL

BLADE OUTER AIR SEAL WITH PASSAGE JOINED CAVITIES

Tip clearance control for turbine blades

COOLED RING SEGMENT

Turbomachine clearance control configuration using a shape memory alloy or a bimetal

HEATING SYSTEM FOR USE IN A TURBINE ENGINE AND METHOD OF OPERATING SAME

Ceramic matrix composite shroud attachment system

GAS TURBINE ENGINE COMPONENT

Aircraft gas turbine

Method of matching thermal response rates between a stator and a rotor and fluidic thermal switch for use therewith

Gas turbine engine

Core runout ceiling for turbine components

Control unit and a method for controlling blade tip clearance

Compressor tip clearance control and gas turbine engine

Controlling blade tip clearances in a turbine engine

Platform with cooling circuit

Device for supporting a turbine ring, turbine having such a device, and turbine engine having such a turbine

Shroud structure for gas turbine

Endwall component for a turbine stage of a gas turbine engine

Turbine shroud thermal distortion control

Gas turbine manifold mounting arrangement including a clevis

Turbine stage shroud segment

Cooling system of ring segment and gas turbine

TURBINE ALIGNMENT CONTROL SYSTEM AND METHOD

Seal clearance control on non-cowled gas turbine engines

Rotor blade tip clearance control

Active tip clearance control for shrouded gas turbine blades and related method

TURBINE GUIDE VANE SUPPORT FOR A GAS TURBINE AND METHOD FOR OPERATING A GAS TURBINE

TURBINE SHROUD SUPPORT THERMAL SHIELD

Ring sector of turbomachine turbine

Cooling system of ring segment and gas turbine

Shroud seal segments arrangement in a gas turbine

Heating system for a turbine

Gas turbine and operating method thereof

Gas turbine plant

Axial-centrifugal compressor having system for controlling play

High pressure turbine of a turbomachine with improved assembly of the mobile blade radial clearance control box

Cooling system of ring segment and gas turbine

System and method for clearance control in a rotary machine

Turbine engine having cooling pin

Compressor for a gas turbine

Turbine casing cooling

Thermal control system for turbines

Active tip clearance control arrangement for gas turbine engine

Scoop of a running-gap control system of an aircraft gas turbine

Methods and systems for controlling gas turbine clearance

Running-gap control system of an aircraft gas turbine

Combination of mechanical actuator and case cooling apparatus

Closed-loop control for a gas turbine with actively stabilized compressor

Systems and methods of reducing heat loss from a gas turbine during shutdown

Compressor clearance control system using bearing oil waste heat

Compressor clearance control system using turbine exhaust

Method of matching thermal response rates between a stator and a rotor and fluidic thermal switch for use therewith

Turbine shroud thermal distortion control

Bypass air scoop for gas turbine engine

Heat exchanger to cool turbine air cooling flow

Asymmetrical gas turbine cooling port locations

Dual stage turbine shroud

Flow inhibitor of turbomachine shroud

Device, system and method for thermally activated displacement

SYSTEM AND METHOD FOR ADJUSTING CLEARANCE IN A GAS TURBINE

Processes for the formation of positive features on shroud components, and related articles

Rotor path arrangements

Predictive model based control system for heavy duty gas turbines

Control system

Method, system, and apparatus for reducing a turbine clearance

Method and device for cooling a component of a turbine

Asymmetrical member for locking ring sectors to a turbine engine casing

Vortex cooled turbine blade outer air seal for a turbine engine

Turbine shroud thermal distortion control

Arrangement for automatic running gap control on a two or multi-stage turbine

Turbine blade tip clearance system

Gas turbine engine with valve for establishing communication between two enclosures

Protection device for a turbine stator

MANUFACTURABLE AND INSPECTABLE COOLING MICROCIRCUITS FOR BLADE-OUTER-AIR-SEALS

Control of clearance at blade tips in a high-pressure turbine of a turbine engine

Mounting System for Impingement Cooling Manifold

METHOD AND APPARATUS FOR CLEARANCE CONTROL OF TURBINE BLADE TIP

Gas turbine engine case for clearance control

Apparatus and method for reducing eccentricity and out-of-roundness in turbines

Aircraft gas turbine engine blade tip clearance control

Impingement cooled structure

Gas turbine engine blade tip clearance apparatus and method

Heat shield for sealing a flow channel of a turbine engine

Rotor seal segment

Methods and system for recuperated circumferential cooling of integral turbine nozzle and shroud assemblies

Tip clearance control system

Integrated support/thermocouple housing for impingement cooling manifolds and cooling method

Apparatus and method for active gap monitoring for a continuous flow machine

Blade clearance system for a turbine engine

Methods and system for cooling integral turbine shround assemblies

Method and system to facilitate cooling turbine engines

Methods and system for recuperated cooling of integral turbine nozzle and shroud assemblies

Compound clearance control engine

Transpiration clearance control turbine

Turbomachine turbine ring sector

Turbine case impingement cooling for heavy duty gas turbines

Method and apparatus for operating gas turbine engines

METHODS AND SYSTEMS FOR CONTROLLING GAS TURBINE CLEARANCE

Clearance control apparatus

Method of joining a microwave transparent component to a host component

Heat accumulation segment

Gas turbine with a compressor housing which is protected against cooling down and method for operating a gas turbine

Compensating for blade tip clearance deterioration in active clearance control

Device for tuning clearance in a gas turbine, while balancing air flows

Device for cooling a turbomachine turbine casing

Thermal control of gas turbine engine rings for active clearance control

System and method to exhaust spent cooling air of gas turbine engine active clearance control

Multi-range clearance measurement system and method of operation

Integrated turbine sealing air and active clearance control system and method

Active clearance control system for gas turbine engines

Turbine shroud assembly and method for assembling a gas turbine engine

Shroud with aero-effective cooling

Device for controlling clearance in a gas turbine

Manufacturable and inspectable cooling microcircuits for blade-outer-air-seals

Access port for dirt removal for gas turbine engine

Dirt separator for gas turbine air supply

Systems and methods for monitoring thermal growth and controlling clearances, and maintaining health of turbo machinery applications

Cooled turbine shroud

Turbine shroud segment impingement cooling on vane outer shroud

Cooled component of a fluid-flow machine, method of casting a cooled component, and a gas turbine

Turbine blade tip clearance control

Method for setting a radial gap of an axial-throughflow turbomachine and compressor

System for actively controlling compressor clearances

Shroud block with enhanced cooling

Turbine engine stator including shape memory alloy and clearance control method

Gas turbine

Shroud leading edge cooling

Casing arrangement

Turbine case cooling

Methods and apparatus for maintaining rotor assembly tip clearances

Gas turbine engine comprising a casing surrounding a rotary assembly and a manifold secured to the casing via a securing arrangement

Controlling air flow to a turbine shroud for thermal control

Arrangement for the automatic running gap control on a two or multi-stage turbine

Gas turbine clearance control devices

Method and system for active tip clearance control in turbines

Hybrid turbine tip clearance control system

Blade tip clearance control

Turbine tip clearance control system

Cooling arrangement

Blade tip clearance control

Network cooled coated wall

Part load blade tip clearance control

Device for controlling clearance in a gas turbine

Internally cooled brush seal backing plate and method

CMC component with cooling cavity

Open rotor gas turbine engine with adaptive turbine clearance control system and method

Methods and apparatus to control a surface of an aircraft engine

Blade tip clearance probe/lead cooling jacket

Turbine assembly with clearance sensor having integrated internal cooling

Variable flowpath casings for blade tip clearance control

Passive cooling system for tip clearance optimization

Turbine stator vanes having inserts and splitter plates