Turbojet engine comprising a connector arm for ancillary systems, and the connector arm for ancillary systems
The present invention concerns a turbofan jet engine comprising an outer fan duct, an inner fan duct, fluid-conveying ancillaries located outside the outer fan duct, fluid-conveying ancillaries located inside the inner fan duct, characterized by the fact that at least one removable modular arm formi...
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Format: | Patent |
Sprache: | eng |
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Zusammenfassung: | The present invention concerns a turbofan jet engine comprising an outer fan duct, an inner fan duct, fluid-conveying ancillaries located outside the outer fan duct, fluid-conveying ancillaries located inside the inner fan duct, characterized by the fact that at least one removable modular arm forming a connection for ancillaries is arranged between the outer fan duct and the inner fan duct. With the invention, the connection of ancillaries outside the outer fan duct to ancillaries inside the inner fan duct is achieved simply by means of a removable arm that is easy to mount and dismount. |
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