High temperature turbine engine structure

Patent · Tue Aug 04 00:00:00 EDT 1992

OSTI ID:6907546

Boyd, Gil

This patent describes a combustion turbine engine. It comprises: an inlet, an outlet, and a flow path communicating a flow of fluid therebetween, the engine including a rotatable compressor inducting a flow of ambient air via the inlet and delivering this air pressurized to a combustor, means delivering a flow of fuel to the combustor to support combustion in the pressurized air to produce a flow of high temperature combustion products, and a turbine expanding the combustion products for discharge into ambient air via the outlet to derive mechanical power therefrom driving the compressor.

• Assignee: Allied-Signal Inc., Morristownship, Morris County, NJ (United States)
• Patent Number(s): US 5134842; A
• Application Number: PPN: US 7-610499
• OSTI ID: 6907546
• Country of Publication: United States
• Language: English

Related Subjects

33 ADVANCED PROPULSION SYSTEMS
330103* -- Internal Combustion Engines-- Turbine
330603 -- Vehicle Design Factors-- Engine System
ALIGNMENT
CERAMICS
CHEMICAL REACTIONS
COMBUSTION
COMPRESSORS
ELEMENTS
EQUIPMENT
FLUID FLOW
INTAKE STRUCTURES
MACHINERY
MECHANICAL PROPERTIES
MECHANICAL STRUCTURES
METALS
OXIDATION
ROTORS
TENSILE PROPERTIES
THERMOCHEMICAL PROCESSES
TORQUE
TURBINES
TURBOMACHINERY