초록 ▼

A thrust reverser system includes a translating cascade, a blocker door, and a drive link. The drive link may be pivotably coupled to the translating cascade and the blocker door. The translating cascade may be coupled to a translating sleeve of a nacelle. The drive link may cause the blocker door t

A thrust reverser system includes a translating cascade, a blocker door, and a drive link. The drive link may be pivotably coupled to the translating cascade and the blocker door. The translating cascade may be coupled to a translating sleeve of a nacelle. The drive link may cause the blocker door to deploy in response to the translating cascade moving in an aft direction. The blocker door may be pivotably coupled to a fixed aft portion of the nacelle.

대표청구항 ▼

1. A thrust reverser system comprising: a translating cascade coupled to a translating sleeve;a fixed forward portion and a fixed aft portion, wherein the fixed forward portion and the fixed aft portion form a portion of a nacelle loft line, and wherein the translating sleeve is located between the

1. A thrust reverser system comprising: a translating cascade coupled to a translating sleeve;a fixed forward portion and a fixed aft portion, wherein the fixed forward portion and the fixed aft portion form a portion of a nacelle loft line, and wherein the translating sleeve is located between the fixed forward portion and the fixed aft portion;a blocker door configured to pivot about an aft end of the blocker door; anda drive link operatively coupled to the translating cascade and the blocker door. 2. The thrust reverser system of claim 1, wherein the blocker door is pivotably coupled to the fixed aft portion. 3. The thrust reverser system of claim 1, wherein the drive link is stowed within a fan cowl. 4. The thrust reverser system of claim 1, wherein the drive link is coupled to a forward end of the blocker door. 5. The thrust reverser system of claim 1, wherein the drive link is configured to deploy the blocker door in response to the translating cascade moving in an aft direction. 6. The thrust reverser system of claim 1, wherein the nacelle comprises a split sleeve. 7. The thrust reverser system of claim 1, wherein the blocker door forms a portion of the nacelle loft line. 8. A nacelle having a thrust reverser comprising: a fixed forward portion;a fixed aft portion, wherein the fixed forward portion and the fixed aft portion form a portion of a nacelle loft line;a translating sleeve located between the fixed forward portion and the fixed aft portion;a translating cascade coupled to the translating sleeve; anda blocker door coupled to the translating cascade by a drive link, wherein the blocker door is configured to rotate about a pivot located at an aft end of the blocker door. 9. The nacelle of claim 8, wherein the blocker door is pivotably coupled to the fixed aft portion. 10. The nacelle of claim 8, wherein the drive link is configured to be stowed in the fixed forward portion. 11. The nacelle of claim 8, wherein the drive link is coupled to a forward end of the blocker door. 12. The nacelle of claim 8, wherein the drive link is configured to deploy the blocker door in response to the translating cascade moving in an aft direction. 13. The nacelle of claim 8, wherein the translating sleeve is configured to overlap the fixed aft portion in a deployed position. 14. The nacelle of claim 8, further comprising a forward seal between the fixed forward portion and the translating sleeve, and an aft seal between the translating sleeve and the fixed aft portion.