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FR2071008A7
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Reducing fatigue failure in case-hardened articles - by - chem removal of imperfect superficial layer
|
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DE1953761A1
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Device for controlling the rudders of aircraft
|
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GB1298557A
|
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Improvements in or relating to rotors for rotary-wing aircraft
|
|
GB1291271A
|
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Improvements in or relating to power transmitting mechanisms, and applications thereof, notably to helicopters
|
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FR2050235A1
|
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Expanded polystyrene shock absorbant - instrument mounting for space craft
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GB1278489A
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Helicopter rotor hub assembly
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|
GB1262921A
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Machine tool for cutting variable-pitch threads
|
|
GB1236089A
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An alarm system for use on board an aircraft
|
|
GB1201660A
|
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Device for combining the braking on the wheels of air and land vehicles
|
|
GB1215228A
|
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Improved hinge arrangement for deployable appurtenances on a body
|
|
GB1222524A
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Improved device for increasing the safety of aircraft during automatic landings by improved overall longitudinal control
|
|
GB1166792A
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Improvements in or relating to Devices for the Diversity Reception of Radio Signals, Notably from a Mobile Transmitter
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GB1223602A
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Improvements in or relating to flight control systems for controlling lift and propulsion devices
|
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GB1199618A
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Improvements in or relating to Large-capacity Aircraft and more particularly to their Main Landing-Gear
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GB1195590A
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Improvements in or relating to Interconnection Devices
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|
GB1185698A
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Improvements in or relating to Helicopter Landing Gear
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|
GB1156871A
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Improvements in or relating to Underwater Propulsion Systems for a Water to Air Missile
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|
US3405891A
|
|
Variable-geometry aircraft with two wing hinge axes on the fuselage
|
|
US3381918A
|
|
Variable-geometry aircraft
|
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GB1098907A
|
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Device for the handling of rigid loads
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