high pressure compressor aft hub assembly

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Compressor aft hub sealing system

An aft hub sealing assembly for a gas turbine engine is disclosed. The aft hub sealing assembly includes an aft hub, a bearing cap, an aft baffle, a first seal, and a second seal. The aft hub includes a body portion and a disk portion aft surface. The bearing cap ...

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CN101037960B - High pressure ratio aft fan - Google Patents

A fan assembly (30) for a gas turbine engine (10) includes a turbine rotor (36) adapted to be disposed aft of a core (20) of the gas turbine engine (10); a row of turbine blades (42) carried by the rotor (36), each turbine blade (42) extending from the rotor (36) to a tip ...

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Compressor aft hub sealing system

An aft hub sealing assembly for a gas turbine engine is disclosed. The aft hub sealing assembly includes an aft hub, a bearing cap, an aft baffle, a first seal, and a second seal. The aft hub includes a body portion and a disk portion aft surface. The bearing cap ...

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Science & Medicine: Turbine Rear Frame

12/12/2008· The balance piston static seal is mounted to the turbine rear frame hub. Stage 11 high pressure compressor bleed air is routed through the three turbine rear frame struts to generate the required axial loading through the rotor thrust balance system.

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High pressure ratio aft fan

High pressure ratio aft fan US7631484 A fan assembly for a gas turbine engine includes a turbine rotor adapted to be disposed aft of a core of the gas turbine engine; a row of turbine blades carried by the rotor, each turbine blade extending from the rotor to a tip, ...

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US20070209368A1 - High pressure ratio aft fan - Google Patents

A fan assembly for a gas turbine engine includes a turbine rotor adapted to be disposed aft of a core of the gas turbine engine; a row of turbine blades carried by the rotor, each turbine blade extending from the rotor to a tip, the turbine blades adapted to extract ...

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US-2019-13-05 - SIKORSKY: Fuselage - Main Transmission Forward and Aft Frame Assemblies

* AD US-2019-16-15 - PRATT & WHITNEY: Engine - High-Pressure Compressor Front Hub - Revision of the Airworthiness Limitations Section and the Continued Airworthiness Maintenance Programs TO see the details OF this Publication, please click OR copy the following: URL:

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Tube Assembly High Pressure Aft - NSN Part Type in Stock

Tube Assembly High Pressure Aft with part number 101-560074-1 is available in stock. Aviation Purchasing Platform is the premier parts and logistics online database for NSN parts and components. Get a quote now !

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Mechanical Design of an Experimental Aspirated Compressor

Mechanical Design of an Experimental Aspirated Compressor by Brian Joseph Schuler S.B., Massachusetts Institute of Technology (1996) Submitted to the Department of Aeronautics and Astronautics in partial fulfillment of the requirements for the degree of

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Science & Medicine: Turbine Rear Frame

12/12/2008· The balance piston static seal is mounted to the turbine rear frame hub. Stage 11 high pressure compressor bleed air is routed through the three turbine rear frame struts to generate the required axial loading through the rotor thrust balance system.

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Compressor aft hub sealing system

An aft hub sealing assembly for a gas turbine engine is disclosed. The aft hub sealing assembly includes an aft hub, a bearing cap, an aft baffle, a first seal, and a second seal. The aft hub includes a body portion and a disk portion aft surface. The bearing cap ...

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HIGH PRESSURE RATIO AFT FAN - General Electric Company

HIGH PRESSURE RATIO AFT FAN United States Patent Application 20070209368 Kind Code: A1 Abstract: A fan assembly for a gas turbine engine includes a turbine rotor adapted to be disposed aft of a core of the a row of turbine blades carried by the rotor ...

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US-2019-13-05 - SIKORSKY: Fuselage - Main Transmission Forward and Aft Frame Assemblies

* AD US-2019-16-15 - PRATT & WHITNEY: Engine - High-Pressure Compressor Front Hub - Revision of the Airworthiness Limitations Section and the Continued Airworthiness Maintenance Programs TO see the details OF this Publication, please click OR copy the following: URL:

Contact Supplier