Link between the exhaust casing and a structural ring of the fan duct of a jet engine
View Patent ↗An assembly including an outer ring of an exhaust casing, a structural ring of an external duct of a fan channel and of a two-flow jet engine that is concentric relative to the outer ring of the exhaust casing, and at least one first and second linking arm or rod forming a hyperstatic link by being attached by one end to the outer ring of the exhaust casing and, by the other end, to the structural ring. The link formed by the first linking arm or rod is configured to break when a predetermined load is exceeded, and the second linking arm or rod is configured to form a force-transmission path between the rings when the link is broken.
1. An assembly comprising:
an outer ring of an exhaust casing;
a structural ring of an outer duct of a by-pass duct of a two-flow jet engine which is concentric relative to the outer ring of the exhaust casing; and
a first pair of connecting rods and a second pair of connecting rods forming a hyperstatic link, first ends of the first and second pairs of the connecting rods being secured to the outer ring of the exhaust casing, and second ends of the first and second pairs of the connecting rods being secured to the structural ring,
wherein the first pair of connecting rods are configured to break when subjected to a predetermined load, and the second pair of connecting rods are configured to not break when subjected to the predetermined load and to form a path for transmission of forces between the outer ring of the exhaust casing and the structural ring when the first pair of connecting rods are broken, and
wherein a first pin passes through the second ends of the first pair of connecting rods and a second pin passes through the second ends of the second pair of connecting rods; and
wherein the first pin is a fusible pin, which can break when the first pin is subjected to the predetermined load, and the second pin includes a polarizing system for distinguishing the second pin from the first pin.
2. The assembly as claimed in claim 1 , wherein the structural ring comprises an attachment which attaches the jet engine on a structure of an aircraft, the second pair of connecting rods being closer to the attachment than the first pair of connecting rods.
3. The assembly as claimed in claim 1 , wherein the first pair of connecting rods are sized to buckle when subjected to the predetermined load.
4. The assembly as claimed in claim 1 , wherein the polarizing system is formed by a difference in diameters of heads of the first fusible pin and the second pin, and by a diameter of a passage of the head of the second pin.
5. The assembly as claimed in claim 4 , wherein the second pin passes through a plate which is fitted on one side of an attachment which attaches the jet engine on a structure of an aircraft.
6. The assembly as claimed in claim 1 , wherein attachments of the first and second pairs of connecting rods are of type with pins and clevises, and the first pair of connecting rods include at least one attachment that breaks when the first pair of connecting rods are subjected to the predetermined load.
7. The assembly as claimed in claim 6 , wherein the first and second pairs of connecting rods are inclined relative to a radial direction, and are tangentially relative to the exhaust casing ring.
8. The assembly as claimed in claim 7 , further comprising a third pair of connecting rods, the third pair of connecting rods are configured to break when subjected to the predetermined load.
9. A two-flow jet engine with a front fan and a secondary flow duct which extends downstream from the fan at least as far as a plane of the exhaust casing comprising an assembly according to claim 1 .