Back to results
US 2014/0112770 A1Published application
Turbojet engine cold stream flow path suspended from the exhaust case by radial crevice mounts and link rods
AssigneeSnecma
InventorsThomas Gérard, Daniel Riviere, François Robert Bellabal, Olivier Renon, Guilhem Seize
Life of this patent
Estimating the term…
Abstract
A bypass turbojet engine including a cylindrical cold stream flow path supported by link rods which are attached to a cylindrical outer shell ring of an exhaust case at attachment points. The attachment points for the exhaust case are crevice mounts including lugs that extend radially from the outer shell ring, a bore of the crevice mounts being directed in a direction of generatrices of the outer shell ring.
Claims10
1-9. (canceled)
A bypass turbojet engine comprising:
- a cylindrical outer fan duct borne by link rods attached to a cylindrical outer shell ring of an exhaust case at attachment points;
- wherein the attachment points of the exhaust case are clevis mounts including lugs that extend radially from the outer shell ring,
- a bore of the clevis mounts being oriented in a direction of generatrices of the outer shell ring.
Dependencies are inferred from the claim text.