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DE1272735B
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Gas outlet device, in particular for aircraft jet engines
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GB1178437A
|
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Bypass Turbo-Jet Engine for VTOL Aircraft.
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|
GB1167518A
|
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Control Arrangement Comprising Two Hand Levers
|
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GB1166292A
|
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By-Pass Turbojet Engine for STOL or VTOL Aircraft.
|
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GB1147076A
|
|
Improvements relating to gas turbine installations
|
|
US3403734A
|
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Control means for rotary wing aircraft
|
|
DE1274893B
|
|
Twin-flow turbine jet engine for aircraft taking off and landing vertically
|
|
DE1277639B
|
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Additional combustion device for heating the gases of a turbine jet engine
|
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DE1235775B
|
|
Lip whistle
|
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DE1228856B
|
|
Internal combustion engine with continuous combustion, in particular a gas turbine system
|
|
DE1254023B
|
|
Gas outlet device, especially for aircraft jet engines, with a pivotable jet pipe
|
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GB1081605A
|
|
Improvements in or relating to balance weights and their location on rotary bodies
|
|
DE1273914B
|
|
Lubricator on a gear
|
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DE1231962B
|
|
Device for the allocation of the fuel to the ignition device of the afterburner of jet engines
|
|
DE1228858B
|
|
Device for distributing the fuel to the ignition device of the afterburner of turbine jet engines
|
|
DE1219804B
|
|
Turbine jet engine for aircraft taking off and landing vertically
|
|
DE1237905B
|
|
Twin-flow turbine jet engine for aircraft taking off and landing vertically
|
|
DE1225447B
|
|
Device for regulating the fuel supply to the ignition device of the afterburner of jet engines
|
|
DE1231959B
|
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As a twin-flow engine in single-shaft design, lift jet engine for aircraft
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