Thrust reverser with blocker door lock
An assembly is provided for an aircraft propulsion system. This assembly includes a fixed structure, a translating structure and a thrust reverser. The translating structure is configured to translate between a stowed position and a deployed position. The thrust reverser includes a blocker door, an actuation linkage and a door lock. The blocker door is pivotally coupled to the translating structure. The actuation linkage operatively couples the blocker door to the fixed structure such that translation of the translating structure to the deployed position actuates pivoting of the blocker door into a flowpath. The door lock is configured to lock the actuation linkage to the translating structure such that the pivoting of the blocker door into the flowpath is delayed as the translating structure translates from the stowed position towards the deployed position.
1. An assembly for an aircraft propulsion system, comprising:
a fixed structure;
a translating structure configured to translate between a stowed position and a deployed position; and
a thrust reverser including a blocker door, an actuation linkage and a door lock;
the blocker door pivotally coupled to the translating structure;
the actuation linkage operatively coupling the blocker door to the fixed structure such that translation of the translating structure to the deployed position actuates pivoting of the blocker door into a flowpath; and
the door lock configured to lock the actuation linkage to the translating structure such that the pivoting of the blocker door into the flowpath is delayed as the translating structure translates from the stowed position towards the deployed position;
wherein the door lock is configured to lock the actuation linkage to the translating structure for at least a first one-tenth of a distance the translating structure translates from the stowed position to the deployed position.
2. The assembly of claim 1 , wherein the door lock includes
a catch fixed to the translating structure; and
a latch coupled to the actuation linkage and configured to mate with the catch to lock the actuation linkage to the translating structure.
3. The assembly of claim 2 , wherein
the catch comprises a catch land; and
the latch comprises a latch element disposed radially outboard of the catch land and radially engageable with the catch land when the door lock locks the actuation linkage to the translating structure.
4. The assembly of claim 2 , wherein the latch comprises a latch crank.
5. The assembly of claim 2 , wherein
the latch includes a latch element, a first lever section and a second lever section;
the latch element is configured to engage the catch to lock the actuation linkage to the translating structure, and the latch element is connected to the first lever section at a distal first end of the first lever section;
the first lever section meets the second lever section at an elbow and projects out from the second lever section to the distal first end;
the second lever section projects out from the first lever section to a distal second end of the second lever section, and the second lever section is coupled to the actuation linkage at the distal second end; and
the latch is pivotally coupled to the blocker door at the elbow.
6. The assembly of claim 1 , wherein
the actuation linkage includes a structure link and a door link;
the structure link is between and pivotally coupled to the fixed structure and the door link; and
the door link is between and pivotally coupled to the structure link and the blocker door.
7. The assembly of claim 6 , wherein the door link is configured to actuate the door lock.
8. The assembly of claim 6 , wherein
the door lock includes a catch and a latch;
the catch is fixed to the translating structure; and
the latch is coupled to the door link.
9. The assembly of claim 6 , wherein
the translating structure forms a peripheral boundary of the flowpath;
the structure link and the door link are outside of the flowpath when the translating structure is in the stowed position; and
the structure link and the door link are disposed in of the flowpath when the translating structure is in the deployed position.
10. The assembly of claim 6 , wherein the structure link comprises a Y-shaped link pivotally attached to the fixed structure through a pair of laterally spaced pivot joints between the Y-shaped link and the fixed structure.
11. The assembly of claim 1 , wherein the translating structure forms a first peripheral boundary of the flowpath and the blocker door forms a second peripheral boundary of the flowpath when the translating structure is in the stowed position.
12. The assembly of claim 1 , further comprising a fixed cascade structure projecting into an internal cavity of the translating structure when the translating structure is in the stowed position.
13. The assembly of claim 1 , wherein the door lock is disposed radially between the fixed cascade structure and the blocker door when the translating structure is in the stowed position.
14. The assembly of claim 1 , wherein the actuation linkage is configured to
push the blocker door away from the translating structure during a first portion of the pivoting of the blocker door; and
pull the blocker door further away from the translating structure during a second portion of the pivoting of the blocker door.
15. An assembly for an aircraft propulsion system, comprising:
a fixed structure;
a translating structure configured to translate between a stowed position and a deployed position; and
a thrust reverser including a blocker door, an actuation linkage and a door lock;
the blocker door pivotally coupled to the translating structure;
the actuation linkage operatively coupling the blocker door to the fixed structure such that translation of the translating structure to the deployed position actuates pivoting of the blocker door into a flowpath; and
the door lock configured to lock the actuation linkage to the translating structure such that the pivoting of the blocker door into the flowpath is delayed as the translating structure translates from the stowed position towards the deployed position;
wherein the door lock is configured to lock the actuation linkage to the translating structure for no more than a first one-sixth of a distance the translating structure translates from the stowed position to the deployed position.
16. An assembly for an aircraft propulsion system, comprising:
a fixed structure;
a translating structure configured to translate between a stowed position and a deployed position; and
a thrust reverser including a blocker door, an actuation linkage and a door lock;
the blocker door pivotally coupled to the translating structure;
the actuation linkage operatively coupling the blocker door to the fixed structure such that translation of the translating structure to the deployed position pivots the blocker door into a flowpath; and
the door lock including a catch and a latch, the catch fixed to the translating structure, the latch coupled to the actuation linkage and pivotally coupled to the blocker door, and the latch configured to mate with the catch when the translating structure is in the stowed position.
17. The assembly of claim 16 , wherein
the latch includes a first lever section and a second lever section that meets the first lever section at an elbow, and the latch is pivotally coupled to the blocker door at the elbow; and
the second lever section projects out from the first lever section to a distal end of the second lever section, and the second lever section is pivotally coupled to the actuation linkage at the distal end.
18. The assembly of claim 17 , wherein
the latch further includes a latch element;
the latch element projects laterally out from the first lever section and is configured to mate with the catch when the translating structure is in the stowed position.