IP Library Granted Patent US 12680245
Granted Patent B2
US 12680245 · App. 18/377,302 · Granted Jul 14, 2026

Vertiport having damping material covering portion of base surface of launching platform

Inventor: Yahia Ismail (Redmond, WA)
Assignee: Supernal, LLC
E01F3/00B64F1/26
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 12680245
App. No.
18/377,302
Granted
Jul 14, 2026
Kind
B2
Abstract

A vertiport is disclosed. The vertiport includes a launching platform having a base surface and a damping material such that the damping material covers at least a portion of the base surface.

Claims (32)

1 . A vertiport for an aircraft, the vertiport comprising:

a launching platform comprising a base surface and a damping material, wherein the damping material covers at least a portion of the base surface, and wherein the damping material comprises:

a base material, wherein the base material is a rubber material selected to reduce deformation with use; and

a filling material inserted into the base material such that the base material substantially surrounds or encloses the filling material, wherein the filling material is an acoustically absorbing material.

2 . The vertiport of claim 1 , wherein the base surface has a shape comprising at least one of: a cylindrical shape, a rectangular shape, a cubical shape, a conical-frustum shape, and a trapezoidal shape.

3 . The vertiport of claim 1 , wherein the base surface has a material composition comprising at least one of: clay, concrete, cement, stone, pavement, and metal.

4 . The vertiport of claim 1 , wherein the damping material has an acoustically varying impedance across the length of the base material.

5 . The vertiport of claim 1 , wherein the damping material further comprises a stiffness to damping ratio such that the base material is configured to support passenger ingress to and egress from an aircraft on the vertiport.

6 . The vertiport of claim 1 , wherein the rubber material comprises a natural rubber.

7 . The vertiport of claim 1 , wherein the damping material has a constant thickness across the portion of the base surface covered by the damping material.

8 . The vertiport of claim 1 , wherein the damping material has a variable thickness across the portion of the base surface covered by the damping material.

9 . The vertiport of claim 8 , wherein the variable thickness of the damping material comprises a thickness that is greater towards a radially outward distance from a center of the base surface.

10 . The vertiport of claim 1 , further comprising a supporting structure, wherein the supporting structure supports at least a portion of the launching platform.

11 . The vertiport of claim 10 , wherein one or more damping pads is applied to the supporting structure.

12 . The vertiport of claim 10 , wherein the supporting structure is external to the launching platform.

13 . A method of moving an aircraft with respect to a launching platform of a vertiport, wherein the launching platform comprises a base surface and a damping material, and wherein the damping material covers at least a portion of the base surface, the method comprising:

moving the aircraft with respect to the launching platform, such that the damping material reduces noise from the aircraft, and wherein the damping material comprises:

a base material, wherein the base material is a rubber material selected to reduce deformation with use; and

a filling material inserted into the base material such that the base material substantially surrounds or encloses the filling material, wherein the filling material is an acoustically absorbing material.

14 . The method of claim 13 , wherein the damping material absorbs noise from the aircraft.

15 . The method of claim 13 , wherein the moving the aircraft comprises landing the aircraft on the launching platform, such that the damping material reduces noise from the aircraft during landing.

16 . The method of claim 13 , wherein the moving the aircraft comprises the aircraft taking off from the launching platform, such that the damping material reduces noise from the aircraft during takeoff.

17 . A vertiport for an aircraft, the vertiport comprising:

an infrastructure;

a support surface extending above the infrastructure; and

a launching platform installed on a top of the support surface comprising a base surface and a damping material, wherein the damping material covers at least a portion of the base surface, and wherein the damping material comprises:

a base material, wherein the base material is a rubber material selected to reduce deformation with use; and

a filling material inserted into the base material such that the base material substantially surrounds or encloses the filling material, wherein the filling material is an acoustically absorbing material.

18 . The vertiport of claim 17 , wherein the infrastructure comprises a substantially rounded structure, and wherein the support surface extends upwards from a central portion of the substantially rounded structure of the infrastructure.

19 . The vertiport of claim 17 , wherein the infrastructure comprises a floating structure in a water-based environment.

20 . The vertiport of claim 17 , wherein the infrastructure comprises an elevated structure on a roof of a building in an environment.

21 . The vertiport of claim 1 , wherein the damping material has a thickness between 1 to 5 inches.