Aircraft propulsion system with variable area inlet

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

a variable area inlet comprising a fixed structure and a moveable structure, the variable area inlet configured to open and close an airflow inlet passage into the aircraft propulsion system;

the moveable structure configured to move axially along a centerline between an aft position and a forward position, and the moveable structure comprising an inlet lip structure and a deflector;

wherein, when the moveable structure is in the aft position, the airflow inlet passage is closed, and the deflector is at least partially recessed into the fixed structure; and

wherein, when the moveable structure is in the forward position, the airflow inlet passage is opened axially between an aft end of the inlet lip structure and a forward end of the fixed structure, and a forward end of the deflector is disposed axially at the forward end of the fixed structure;

wherein a blind cavity projects axially partially into the variable area inlet when the moveable structure is in the forward position; and

wherein the blind cavity extends radially between the deflector and the fixed structure when the moveable structure is in the forward position.

2. The assembly of claim 1 , wherein

the inlet lip structure comprises a tubular inlet lip structure; and

the deflector comprises a tubular deflector.

3. The assembly of claim 1 , wherein a pylon extends axially between and is connected to the inlet lip structure and the deflector.

4. The assembly of claim 1 , wherein the deflector is configured to move axially with the inlet lip structure as the moveable structure moves between the aft position and the forward position.

5. The assembly of claim 1 , wherein the deflector is configured to form a virtual ramp into the airflow inlet passage when the moveable structure is in the forward position.

6. The assembly of claim 1 , wherein

a leading edge of the deflector is abutted radially against the fixed structure when the moveable structure is in the aft position; and

the leading edge of the deflector is radially displaced from the fixed structure when the moveable structure is in the forward position.

7. The assembly of claim 6 , wherein a radius of the leading edge of the deflector to the centerline remains uniform as the deflector moves with the moveable structure axially along the centerline between the aft position and the forward position.

8. The assembly of claim 1 , wherein the variable area inlet is configured without the blind cavity when the moveable structure is in the aft position.

9. The assembly of claim 1 , wherein the deflector extends circumferentially about a portion of the fixed structure at the forward end of the fixed structure when the moveable structure is in the forward position.

10. The assembly of claim 1 , wherein, when the moveable structure is in the aft position, the aft end of the inlet lip structure is abutted axially against the forward end of the fixed structure.

11. The assembly of claim 1 , wherein the airflow inlet passage extends radially through the variable area inlet when the moveable structure is in the forward position.

12. The assembly of claim 1 , further comprising:

an inlet duct;

the airflow inlet passage comprising an outer airflow inlet passage, and the variable area inlet further comprising an inner airflow inlet passage at a forward end of the moveable structure;

the inlet duct fluidly coupled with the inner airflow inlet passage when the moveable structure is in the aft position, and the inlet duct fluidly coupled with the inner airflow inlet passage and the outer airflow inlet passage when the moveable structure is in the forward position.

13. The assembly of claim 12 , wherein the inlet duct is configured to direct air received from the inner airflow inlet passage and the outer airflow inlet passage into at least one of a core flowpath or a bypass flowpath of the aircraft propulsion system when the moveable structure is in the forward position.

14. The assembly of claim 12 , wherein the variable area inlet is configured to regulate airflow through the inner airflow inlet passage by moving the moveable structure between the aft position and the forward position.

15. The assembly of claim 1 , wherein

the airflow inlet passage comprises a plurality of ports through the variable area inlet; and

the plurality of ports are arranged circumferentially about the centerline in an array.

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

a variable area inlet comprising a fixed structure, a moveable structure, an inner airflow inlet passage, an outer airflow inlet passage and an inlet duct, the variable area inlet configured to regulate airflow through the outer airflow inlet passage by translating the moveable structure axially along a centerline between an aft position and a forward position, and the moveable structure including an inlet lip structure and a deflector;

the inner airflow inlet passage at a forward end of the moveable structure and circumscribed by the inlet lip structure when the moveable structure is at the aft position and the forward position;

the outer airflow inlet passage extending axially between the inlet lip structure and the fixed structure when the moveable structure is at the forward position, and the deflector configured to provide a virtual ramp into the inner airflow inlet passage when the moveable structure is at the forward position; and

the inlet duct configured to receive airflow from the inner airflow inlet passage and the outer airflow inlet passage when the moveable structure is at the forward position;

wherein a blind cavity projects axially partially into the variable area inlet when the moveable structure is in the forward position; and

wherein the blind cavity extends radially between the deflector and the fixed structure when the moveable structure is in the forward position.

17. The assembly of claim 16 , wherein

an aft end of the inlet lip structure is axially spaced from a forward end of the fixed structure when the moveable structure is at the forward position to open the outer airflow inlet passage; and

the aft end of the inlet lip structure is axially abutted with the forward end of the fixed structure when the moveable structure is at the aft position to close the outer airflow inlet passage.

18. The assembly of claim 16 , wherein

a forward end of the deflector is axially displaced from a forward end of the fixed structure when the moveable structure is at the aft position; and

the forward end of the deflector is axially at, and radially spaced from, the forward end of the fixed structure when the moveable structure is at the forward position to provide the virtual ramp into the inner airflow inlet passage.

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

a variable area inlet comprising a fixed structure, an inlet lip structure and a deflector, the variable area inlet configured to open and close an airflow inlet passage into the aircraft propulsion system;

the inlet lip structure configured to move axially along a centerline between an aft position and a forward position, the airflow inlet passage closed when the inlet lip structure is at the aft position, and the airflow inlet passage is opened axially between an aft end of the inlet lip structure and a forward end of the fixed structure when the inlet lip structure is at the forward position; and

a leading edge of the deflector abutted radially against the fixed structure when the inlet lip structure is at the aft position, and the leading edge of the deflector disposed axially at and radially displaced from the forward end of the fixed structure when the inlet lip structure is at the forward position;

wherein a blind cavity projects axially partially into the variable area inlet when the inlet lip structure is in the forward position; and

wherein the blind cavity extends radially between the deflector and the fixed structure when the inlet lip structure is in the forward position.