Aircraft propulsion system with variable area inlet

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

a variable area inlet comprising an outer airflow inlet passage, an inner airflow inlet passage, an inlet structure and a center body structure, the outer airflow inlet passage radially between the inlet structure and the center body structure, the inner airflow inlet passage formed within the center body structure, the center body structure comprising a valve configured to regulate air flow through the inner airflow inlet passage, and the valve comprising a first door configured to pivot between a closed position and an open position; and

an inlet duct configured to receive air from the outer airflow inlet passage when the first door is in the closed position, and the inlet duct configured to receive air from the outer airflow inlet passage and the inner airflow inlet passage when the first door is in the open position;

wherein the inlet duct is configured to direct air received from the outer airflow inlet passage and the inner airflow inlet passage into a core flowpath of the aircraft propulsion system when the first door is in the open position.

2. The assembly of claim 1 , wherein the inner airflow inlet passage comprises an annular passage.

3. The assembly of claim 1 , wherein the outer airflow inlet passage circumscribes the inner airflow inlet passage.

4. The assembly of claim 1 , wherein the inner airflow inlet passage extends within the center body structure from an inlet into the center body structure to an outlet from the center body structure.

5. The assembly of claim 4 , wherein the inlet is axially forward of the outer airflow inlet passage.

6. The assembly of claim 4 , wherein the first door is located at the inlet.

7. The assembly of claim 4 , wherein the first door is located at the outlet.

8. The assembly of claim 1 , wherein the first door is connected to another component of the center body structure by a hinge.

9. The assembly of claim 1 , wherein

the first door is configured to pivot about a pivot axis between the closed position and the open position; and

the pivot axis is perpendicular to a centerline of the variable area inlet.

10. The assembly of claim 1 , wherein the first door is configured to pivot in a radially inward direction towards a centerline of the variable area inlet from the closed position to the open position.

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

a variable area inlet comprising an outer airflow inlet passage, an inner airflow inlet passage, an inlet structure and a center body structure, the outer airflow inlet passage radially between the inlet structure and the center body structure, the inner airflow inlet passage formed within the center body structure, the center body structure comprising a valve configured to regulate air flow through the inner airflow inlet passage, and the valve comprising a first door configured to pivot between a closed position and an open position; and

an inlet duct configured to receive air from the outer airflow inlet passage when the first door is in the closed position, and the inlet duct configured to receive air from the outer airflow inlet passage and the inner airflow inlet passage when the first door is in the open position;

wherein the valve further comprises a second door;

wherein the first door is circumferentially next to the second door when the first door and the second door are closed; and

wherein the first door circumferentially overlaps the second door when the first door and the second door are open.

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

a variable area inlet comprising an outer airflow inlet passage, an inner airflow inlet passage, an inlet structure and a center body structure, the outer airflow inlet passage radially between the inlet structure and the center body structure, the inner airflow inlet passage formed within the center body structure, the center body structure comprising a valve configured to regulate air flow through the inner airflow inlet passage, and the valve comprising a first door configured to pivot between a closed position and an open position; and

an inlet duct configured to receive air from the outer airflow inlet passage when the first door is in the closed position, and the inlet duct configured to receive air from the outer airflow inlet passage and the inner airflow inlet passage when the first door is in the open position;

wherein the valve further comprises a second door and an actuator; and

wherein the actuator is configured to concurrently pivot the first door and the second door.

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

a variable area inlet comprising an outer airflow inlet passage, an inner airflow inlet passage, an inlet structure and a center body structure, the outer airflow inlet passage radially between the inlet structure and the center body structure, the inner airflow inlet passage formed within the center body structure, the center body structure comprising a valve configured to regulate air flow through the inner airflow inlet passage, and the valve comprising a first door configured to pivot between a closed position and an open position; and

an inlet duct configured to receive air from the outer airflow inlet passage when the first door is in the closed position, and the inlet duct configured to receive air from the outer airflow inlet passage and the inner airflow inlet passage when the first door is in the open position;

wherein the valve further comprises a track, an actuator, a slider and a first linkage;

wherein the track is configured with a fixed component of the center body structure;

wherein the actuator is attached to the slider;

wherein the slider is mated with and is configured to translate along the track; and

wherein the first linkage is between and pivotably connected to the slider and the first door.

14. The assembly of claim 13 , wherein

the valve further comprises a second door and a second linkage;

the second door is configured to pivot between a closed position and an open position; and

the second linkage is between and pivotably connected to the slider and the second door.

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

a variable area inlet comprising an outer airflow inlet passage, an inner airflow inlet passage, an inlet structure and a center body structure, the outer airflow inlet passage radially between the inlet structure and the center body structure, the inner airflow inlet passage formed within the center body structure, the center body structure comprising a valve configured to regulate air flow through the inner airflow inlet passage, and the valve comprising a first door configured to pivot between a closed position and an open position; and

an inlet duct configured to receive air from the outer airflow inlet passage when the first door is in the closed position, and the inlet duct configured to receive air from the outer airflow inlet passage and the inner airflow inlet passage when the first door is in the open position;

wherein the inlet duct is configured to direct air received from the outer airflow inlet passage and the inner airflow inlet passage into a bypass flowpath of the aircraft propulsion system when the first door is in the open position.

16. The assembly of claim 15 , wherein the inner airflow inlet passage comprises an annular passage.

17. The assembly of claim 15 , wherein the outer airflow inlet passage circumscribes the inner airflow inlet passage.

18. The assembly of claim 15 , wherein the inner airflow inlet passage extends within the center body structure from an inlet into the center body structure to an outlet from the center body structure.

19. The assembly of claim 15 , wherein the first door is connected to another component of the center body structure by a hinge.

20. The assembly of claim 15 , wherein

the first door is configured to pivot about a pivot axis between the closed position and the open position; and

the pivot axis is perpendicular to a centerline of the variable area inlet.