SYSTEM FOR ATTACHING A TURBOJET ENGINE SPINNER

According to the invention, the upstream rotor of a turbomachine, of longitudinal axis L-L, comprising a spinner (2) coaxial with the axis L-L and which is attached removably to the upstream end of the rotor (1) by attachment means, is characterized in that the said attachment means comprise a dog c...

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Bibliographic Details
Main Authors PATSOURIS EMMANUEL, BART JACQUES RENE
Format Patent
LanguageEnglish
Published 05.12.2013
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Summary:According to the invention, the upstream rotor of a turbomachine, of longitudinal axis L-L, comprising a spinner (2) coaxial with the axis L-L and which is attached removably to the upstream end of the rotor (1) by attachment means, is characterized in that the said attachment means comprise a dog clutch (3, 9, 10) and rotation-proofing means preventing the spinner (2) from rotating with respect to the rotor (1).
Bibliography:Application Number: US201313845808