EP3070313A1
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Firewall assembly for a wall portion in a turbo engine having different material layers
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GB201421773D0
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Air intake arrangement
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GB201420175D0
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Gas turbine engine
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DE102014221049A1
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Arrangement and method for blowing off compressor air in an engine
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DE102014220317A1
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Aircraft gas turbine engine with shock absorbing element for fan blade loss
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DE102014114473A1
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Gas turbine with at least two coaxial with each other and at least partially formed as hollow shafts waves
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GB201417505D0
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A gas turbine architecture
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GB201417504D0
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A gas turbine architecture
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DE102014114043A1
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Aero engine with a compressor device
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DE102014219552A1
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Guide vane adjusting a gas turbine
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DE102014219050A1
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Method and device for machining blade tips of a compressor rotor of a gas turbine
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DE102014219063A1
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Concentric component arrangement of a gas turbine
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DE102014218350A1
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Sound-absorbing arrangement for an engine nacelle and engine nacelle with such an arrangement
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DE102014113128A1
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Tank device of an aircraft engine with a device for introducing oil
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DE102014113132A1
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Aircraft with a storage chamber and a device for introducing oil
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DE102014112955A1
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Housing device of a jet engine
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DE102014112960A1
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Housing device of a jet engine
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DE102014112954A1
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Housing device of a jet engine
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DE102014217884A1
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Filling elements of a fan of a gas turbine
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DE102014217887A1
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Filling elements of a fan of a gas turbine
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