Spring for a cascade-type thrust reverser shutter for an aircraft jet engine
View Patent ↗This leaf spring ( 17 ) for a thrust reverser shutter ( 13 ) is noteworthy in that it has two branches ( 19, 21 ) defining a U shape, the ends ( 19 a, 19 b, 21 a, 21 b ) of these branches being able to cooperate respectively with a shutter ( 13 ) of said reverser and with a link ( 15 ) for actuating this shutter.
1. A leaf spring for a thrust reverser shutter, comprising: at least one shutter; two branches defining a U-shape, wherein one of the respective ends of the branches is fixed to said at least one shutter of a thrust reverser and the other respective ends of the other branch has turned-over portions defining a bearing for one end of a link rod that actuates the shutter.
2. The leaf spring as claimed in claim 1 , wherein said ends are positioned substantially facing one another.
3. The leaf spring as claimed in claim 1 , wherein at least one of said branches comprises two parts in a form of a fork.
4. The leaf spring as claimed in claim 1 , wherein the branch of said leaf spring having the turned-over portions has a cross section that decreases from a base of said U-shape toward an end of the branch having the turned-over portions.
5. The leaf spring as claimed in claim 1 , wherein the turned-over portions of said branch having the turned-over-portions are able to act as bearing for said link rod.
6. The leaf spring as claimed in claim 1 , wherein the branch of said spring fixed to said shutter has mounting flats near the end.
7. The leaf spring as claimed in claim 1 , wherein the leaf spring is at least partially formed of a titanium-based alloy.
8. The leaf spring as claimed in claim 1 , wherein the leaf spring is at least partially formed of a composite material.
9. A cascade-type thrust reverser, comprising at least one leaf spring as claimed in claim 1 .
10. A jet engine nacelle, comprising a thrust reverser as claimed in claim 9 .