# US 11,299,292 B2 · Deployable landing pads for vertical landing and takeoff vehicles and methods incorporating the same

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- Number: US 11,299,292 B2
- Document ID: US11299292B2
- Status: Granted
- Kind: B2
- Application number: 16/527,761
- Filed: 2019-07-31
- Published: 2021-02-04
- Granted: 2022-04-12
- Earliest claimed: 2019-07-31
- Assignees: Toyota Jidosha Kabushiki Kaisha
- Applicants: Toyota Jidosha Kabushiki Kaisha
- Inventors: James J. Kuffner, Jr.
- Web page: https://patentgrep.com/patent/US11299292B2

## CPC

- B64F 1/007: {Helicopter portable landing pads}
- B64U 80/86: Land vehicles
- B64F: GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64U: UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR

## Abstract

A method of deploying a landing pad, for a vertical takeoff and landing vehicle, relative to a surface of an environment in which the landing pad is disposed, includes stowing an adjustable body of the landing pad in a stowed state. The adjustable body includes a platform surface that in the stowed state defines a first planar surface area relative to the surface, the first planar surface area being inoperable to receive the vertical takeoff and landing vehicle thereon. The method includes deploying the adjustable body from the stowed state to a deployed state. In the deployed state the platform surface defines a second planar surface area greater than the first planar surface area, the second surface planar area of the platform surface is sized and shaped to receive the vertical takeoff and landing vehicle thereon in the deployed state.

## Claims

### Claim 1

A method of deploying a landing pad, for a vertical takeoff and landing vehicle, relative to a surface of an environment in which the landing pad is disposed, the method comprising:
stowing an adjustable body of the landing pad in a stowed state, the adjustable body includes a platform surface, in the stowed state the platform surface defines a first planar surface area relative to the surface, the first planar surface area being inoperable to receive the vertical takeoff and landing vehicle thereon; and
deploying the adjustable body from the stowed state to an intermediate state by moving the adjustable body upwardly, and then deploying the adjustable body to a deployed state by moving the adjustable body downwardly toward the surface, in the deployed state the platform surface defines a second planar surface area greater than the first planar surface area, the second planar surface area of the platform surface is sized and shaped to receive the vertical takeoff and landing vehicle thereon in the deployed state.

### Claim 2 (depends on 1)

The method of claim 1, wherein in the stowed state the platform surface extends generally parallel to a central axis of the adjustable body and in the deployed state the platform surface extends generally perpendicular to the central axis, and
wherein adjusting the adjustable body from the stowed state to the deployed state includes translating the platform surface radially outward relative to the central axis.

### Claim 3 (depends on 2)

The method of claim 2, wherein in the stowed state the adjustable body is at least partially received within a cavity extending downwardly from the surface, the cavity extending generally parallel with the central axis of the adjustable body.

### Claim 4 (depends on 3)

The method of claim 3, wherein in the stowed state a top end of the adjustable body is positioned level with or beneath the surface.

### Claim 5 (depends on 4)

The method of claim 4, wherein:
in the intermediate state the platform surface defines the first planar surface area relative to the surface, the platform surface extends generally parallel to the central axis, and the top end of the adjustable body is positioned a predetermined distance above the surface.

### Claim 6 (depends on 1)

The method of claim 1, wherein the adjustable body includes a material that is attached to and extends between a plurality of beams such that extending the adjustable body from the stowed state to the deployed state comprises
separating the plurality of beams relative one another from a compacted position to an expanded position.

### Claim 7 (depends on 6)

The method of claim 6, further comprising
widening the material positioned between the plurality of beams when separating the plurality of beams from the compacted position to the expanded position such that the material forms the platform surface.

### Claim 8

A deployable landing pad assembly for a vertical takeoff and landing vehicle, relative to a surface of an environment in which the landing pad is disposed, the deployable landing pad assembly comprising:
an adjustable body that includes an adjustable platform surface, the adjustable body movable between a stowed state, an intermediate state, and a deployed state, in the stowed state the platform surface defines a first planar surface area relative to the surface, the first planar surface area being inoperable to receive the vertical takeoff and landing vehicle thereon, in the deployed state the platform surface defines a second planar surface area greater than the first planar surface area, the second surface planar area of the platform surface is sized and shaped to receive the vertical takeoff and landing vehicle thereon in the deployed state; and
a deployment mechanism configured to move the adjustable body from the stowed state to the intermediate state by moving the adjustable body upwardly, and then to the deployed state by moving the adjustable body downwardly toward the surface.

### Claim 9 (depends on 8)

The deployable landing pad assembly of claim 8, wherein in the stowed state the platform surface of the adjustable body has a generally cylindrical shape that extends generally parallel to a central axis of the adjustable body, and in the deployed state the platform surface of the adjustable body has a generally planar shape that extends generally perpendicular to the central axis of the adjustable body.

### Claim 10 (depends on 9)

The deployable landing pad assembly of claim 9, wherein the deployment mechanism is configured to translate the platform surface radially outward relative to the central axis when moving the adjustable body from the stowed state to the deployed state.

### Claim 11 (depends on 10)

The deployable landing pad assembly of claim 10, wherein in the stowed state the adjustable body is at least partially received within a cavity extending downwardly from the surface, the cavity extending generally parallel with the central axis of the adjustable body.

### Claim 12 (depends on 11)

The deployable landing pad assembly of claim 11, wherein in the stowed state a top end of the adjustable body is positioned level with or beneath the surface.