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US 8,985,508 B2Granted
Suspension assembly for an aircraft turbojet engine
AssigneeAircelle
InventorsPierre Caruel, Guy Bernard Vauchel
Life of this patent
Estimating the term…
Abstract
A suspension assembly for an aircraft turbojet engine includes a pylon and connecting rods for taking up the thrust of the turbojet engine which is connected to the pylon. In particular, the suspension assembly includes an insulator which is separate from the pylon and thermally insulates the connecting rods from the turbojet engine.
Claims9
A suspension assembly for an aircraft turbojet engine, comprising:
- a pylon and connecting rods, wherein said connecting rods extend from an upstream part of a gas generator of said turbojet engine to a rear part of said pylon and said connecting rods are configured to take up thrust of said turbojet engine connected to said pylon,
- insulating means configured to thermally insulate the connecting rods from the turbojet engine, said insulating means being separate from said pylon.
Dependencies are inferred from the claim text.