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FR2570133A1
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Device for directing a flow of air at any point over an entire blade height at the inlet of a wheel of an axial compressor
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US3903691A
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Method and devices for avoiding the formation of thermal imbalances in turbine engines
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US3908362A
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Bypass turbojet with variable pitch low pressure compressor for thermal load control
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US3535873A
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Gas turbine cooling devices
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GB1112133A
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Improvements in or relating to combustion chambers
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DE1267035B
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Control and regulation system for gas turbine engines to drive propellers or helicopter rotors
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GB996659A
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Improvements in or relating to gas turbine engines
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GB922255A
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Improvements in and relating to control method and system for aircraft powerplants comprising a gas turbine driving a variable pitch propelling device
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GB916896A
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Improvements in and relating to axial-flow compressors operating at ultrasonic and supersonic speeds
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DE1403597A1
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Blade for compressor with axial flow
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GB925536A
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Improvements in and relating to control devices for gas turbines
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DE1259647B
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Control and regulation system for gas turbine engines
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GB930148A
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Improvements in and relating to fuel feed systems for gas turbines and applications thereof
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GB867849A
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Improvements in or relating to axial flow compressors, and their applications
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GB866988A
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Improvements in or relating to the fuel feed systems of turbojet engines
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GB860283A
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Improvements in or relating to regulating apparatus having a hydraulic servo-control
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GB837738A
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Improvements in or relating to rotary injection devices for gas turbine combustion chambers
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GB850979A
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Improvements in or relating to methods of fastening and locking blades of turbines, compressors and like machines
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GB825186A
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Improvements in or relating to methods of and systems for supplying fuel for turbojet engines
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GB805695A
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Improvements in or relating to methods of and systems for supplying fuel for turbojet engines
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