Damping landing gear systems for vtol aircraft

1. A vertical takeoff and landing aircraft propulsion assembly comprising:

a damping landing gear assembly comprising:

a spring housing disposed inside the vertical takeoff and landing aircraft propulsion assembly, the spring housing forming a spring chamber;

a spring disposed in the spring chamber; and

a plunger slidably coupled to the spring housing and movable between a plurality of positions including a compressed position and an extended position;

wherein the spring biases the plunger into the extended position during flight; and

wherein the vertical takeoff and landing aircraft propulsion assembly experiences a landing force during landing, the landing force compressing the plunger into the compressed position against the bias of the spring, thereby absorbing at least a portion of the landing force.

2. The vertical takeoff and landing aircraft propulsion assembly as recited in claim 1 wherein the damping landing gear assembly further comprises a flange coupled to a distal end of the spring housing;

wherein the vertical takeoff and landing aircraft propulsion assembly comprises an airframe portion; and

wherein the flange is coupled to the airframe portion.

3. The vertical takeoff and landing aircraft propulsion assembly as recited in claim 1 wherein the spring chamber further comprises a cylindrical spring chamber.

4. The vertical takeoff and landing aircraft propulsion assembly as recited in claim 1 wherein the spring is disposed between the plunger and a proximal end of the spring housing.

5. The vertical takeoff and landing aircraft propulsion assembly as recited in claim 1 wherein the vertical takeoff and landing aircraft propulsion assembly is configured to take off and land on a landing surface, the spring biasing the plunger against the landing surface during takeoff to generate a push-off effect.

6. The vertical takeoff and landing aircraft propulsion assembly as recited in claim 1 wherein the spring further comprises a compression spring.

7. The vertical takeoff and landing aircraft propulsion assembly as recited in claim 1 wherein the spring further comprises a friction spring.

8. The vertical takeoff and landing aircraft propulsion assembly as recited in claim 1 wherein the spring further comprises a viscous spring.

9. The vertical takeoff and landing aircraft propulsion assembly as recited in claim 1 wherein the spring further comprises a solid packing material.

10. The vertical takeoff and landing aircraft propulsion assembly as recited in claim 1 wherein the spring further comprises a gas spring.

11. The vertical takeoff and landing aircraft propulsion assembly as recited in claim 10 wherein the spring housing forms an orifice.

12. The vertical takeoff and landing aircraft propulsion assembly as recited in claim 10 wherein the damping landing gear assembly further comprises an adjustable orifice coupled to a proximal end of the spring housing.

13. The vertical takeoff and landing aircraft propulsion assembly as recited in claim 1 wherein the plunger has a proximal end forming a piston disposed in the spring chamber.

14. The vertical takeoff and landing aircraft propulsion assembly as recited in claim 13 wherein the piston forms a piston cavity configured to receive the spring.

15. The vertical takeoff and landing aircraft propulsion assembly as recited in claim 1 wherein the damping landing gear assembly further comprises a landing foot coupled to a distal end of the plunger.

16. The vertical takeoff and landing aircraft propulsion assembly as recited in claim 15 wherein the landing foot further comprises one of a hard surface landing foot, a soft surface landing foot or a water surface landing foot.

17. A vertical takeoff and landing aircraft comprising:

a fuselage;

a propulsion assembly; and

a damping landing gear assembly coupled to the propulsion assembly, the damping landing gear assembly comprising:

a spring housing disposed inside the propulsion assembly, the spring housing forming a spring chamber;

a spring disposed in the spring chamber; and

a plunger slidably coupled to the spring housing and movable between a plurality of positions including a compressed position and an extended position;

wherein the spring biases the plunger into the extended position during flight; and

wherein the vertical takeoff and landing aircraft experiences a landing force during landing, the landing force compressing the plunger into the compressed position against the bias of the spring, thereby absorbing at least a portion of the landing force.

18. The vertical takeoff and landing aircraft as recited in claim 17 further comprising:

an airframe having first and second wings with first and second pylons extending therebetween, the fuselage coupled to the pylons; and

a two-dimensional distributed thrust array including the propulsion assembly attached to the airframe, the thrust array including a plurality of propulsion assemblies coupled to the first wing and a plurality of propulsion assemblies coupled to the second wing;

wherein the damping landing gear assembly further comprises a plurality of damping landing gear assemblies, each damping landing gear assembly coupled to an aft end of a respective one of the propulsion assemblies.

19. The vertical takeoff and landing aircraft propulsion assembly as recited in claim 1 wherein the vertical takeoff and landing aircraft propulsion assembly comprises a nacelle, the spring housing disposed inside the nacelle.

20. The vertical takeoff and landing aircraft propulsion assembly as recited in claim 1 further comprising a plurality of landing feet including a hard surface landing foot and a soft surface landing foot interchangeably attachable to a distal end of the plunger.