Thrust reverser with blocker door system

1. An assembly for an aircraft propulsion system, comprising:

a fixed structure;

a translating structure configured to translate relative to the fixed structure;

a blocker door extending between a blocker door first end and a blocker door second end, the translating structure pivotally attached to the blocker door at the blocker door first end; and

a rigid linkage comprising

a first pivot attachment coupled to the fixed structure;

a second pivot attachment coupled to the translating structure; and

a third pivot attachment coupled to the blocker door at the blocker door second end;

wherein the blocker door is configured as a folding blocker door comprising an outer panel and an inner panel, the outer panel is configured between and pivotally attached to the translating structure and the inner panel, and the third pivot attachment is coupled to the inner panel; and

the outer panel, the inner panel, the translating structure and the rigid linkage are configured together as a four-bar link system.

2. The assembly of claim 1 , wherein

the rigid linkage extends between a first linkage end and a second linkage end;

the first pivot attachment is between the second pivot attachment and the third pivot attachment;

the second pivot attachment is at the first linkage end; and

the third pivot attachment is at the second linkage end.

3. The assembly of claim 1 , wherein the first pivot attachment comprises a carriage that rides within a track of the fixed structure.

4. The assembly of claim 3 , wherein the carriage comprises a roller.

5. The assembly of claim 3 , wherein a first portion of the track follows a straight trajectory and a second portion of the track follows a curved trajectory.

6. The assembly of claim 1 , wherein the outer panel extends between a first outer panel end and a second outer panel end, the outer panel is pivotally attached to the inner panel at the first outer panel end, and the outer panel is pivotally attached to the translating structure at the second outer panel end.

7. The assembly of claim 6 , wherein the first outer panel end is axially forward and radially inward of the second outer panel end with respect to a centerline of the aircraft propulsion system when the folding blocker door is in the deployed position.

8. The assembly of claim 1 , wherein the translating structure comprises a translating cascade structure.

9. The assembly of claim 1 , further comprising a biasing device configured to bias the inner panel away from the outer panel.

10. The assembly of claim 1 , further comprising a stop configured to limit pivoting between the inner panel and the outer panel.

11. An assembly for an aircraft propulsion system, comprising:

a fixed structure comprising a track;

a translating structure configured to translate relative to the fixed structure;

a blocker door pivotally attached to the translating structure; and

a linkage including a first pivot attachment, a second pivot attachment and a third pivot attachment;

the first pivot attachment comprising a carriage coupled with and adapted to ride along the track;

the second pivot attachment coupled to the translating structure; and

the third pivot attachment coupled to the blocker door at a blocker door second end;

wherein the blocker door is configured as a folding blocker door comprising an outer panel and an inner panel, the outer panel is configured between and is pivotally attached to the translating structure and the inner panel, and the third pivot attachment is coupled to the inner panel; and

the outer panel, the inner panel, the translating structure and the linkage are configured together as a four-bar link system.

12. The assembly of claim 11 , wherein a first portion of the track follows a straight trajectory and a second portion of the track follows a curved trajectory.

13. The assembly of claim 12 , wherein the first portion is substantially parallel with a centerline of the aircraft propulsion system, and the second portion curves radially inward towards the centerline as the second portion extends axially away from the first portion.

14. The assembly of claim 11 , wherein

the linkage extends between a first linkage end and a second linkage end;

the first pivot attachment is between the second pivot attachment and the third pivot attachment;

the second pivot attachment is at the first linkage end; and

the third pivot attachment is at the second linkage end.

15. The assembly of claim 11 , wherein the second pivot attachment directly and pivotally couples the linkage to the translating structure.

16. The assembly of claim 11 , wherein the second pivot attachment is located radially outboard of the first pivot attachment with respect to a centerline of the aircraft propulsion system and decoupled from the track when the blocker door is deployed into a bypass flowpath of the aircraft propulsion system.

17. An assembly for an aircraft propulsion system, comprising:

a fixed structure;

a translating structure configured to translate relative to the fixed structure;

a blocker door extending between a blocker door first end and a blocker door second end, the translating structure pivotally attached to the blocker door at the blocker door first end; and

a rigid linkage comprising

a first pivot attachment coupling the rigid linkage to the fixed structure;

a second pivot attachment directly and pivotally coupling the rigid linkage to the translating structure; and

a third pivot attachment directly and pivotally coupling the rigid linkage to the blocker door at the blocker door second end;

wherein the blocker door is configured as a folding blocker door comprising an outer panel and an inner panel, the outer panel is configured between and is pivotally attached to the translating structure and the inner panel, and the third pivot attachment is coupled to the inner panel; and

the outer panel, the inner panel, the translating structure and the rigid linkage are configured together as a four-bar link system.

18. The assembly of claim 17 , wherein the first pivot attachment comprises a carriage that rides within a track of the fixed structure.

19. The assembly of claim 18 , wherein the second pivot attachment is radially outboard of the first pivot attachment with respect to a centerline of the aircraft propulsion system when the blocker door is deployed.