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US 11,597,534 B2Granted
Aircraft launching systems and methods
AssigneeThe Boeing Company
InventorSteve G. Mackin
Life of this patent
Estimating the term…
Abstract
An aircraft launching system and method include a first lifting sub-system including a first tether that removably couples to an aircraft, and a second lifting sub-system including a second tether that couples the first lifting sub-system to the second lifting sub-system.
Claims21
An aircraft launching system, comprising:
- a first lifting sub-system including a first tether that removably couples to an aircraft, wherein the first tether is selectively deployable in relation to the first lifting sub-system;
- and
- a second lifting sub-system including a second tether that couples the first lifting sub-system to the second lifting sub-system, wherein the second tether is selectively deployable in relation to the second lifting sub-system,
- wherein the first lifting sub-system is configured to independently lift the aircraft to a first altitude off and above ground, and
- wherein the second lifting sub-system is configured to lift the first lifting sub-system and the aircraft off and above the ground so that the aircraft is at a second altitude that is greater than the first altitude.
2 more elements
An aircraft launching method, comprising:
- removably coupling an aircraft to a first tether of a first lifting sub-system;
- coupling the first lifting sub-system to a second tether of a second lifting sub-system;
- lifting, independently by the first lifting sub-system, the aircraft to a first altitude off and above ground;
- lifting, by the second lifting sub-system, the first lifting sub-system and the aircraft off and above the ground so that the aircraft is at a second altitude that is greater than the first altitude;
- selectively deploying the first tether in relation to the first lifting sub-system;
- and
- selectively deploying the second tether in relation to the second lifting sub-system.
4 more elements
An aircraft launching system, comprising:
- a first lifting sub-system including a first tether that removably couples to an aircraft, wherein the first tether is selectively deployable in relation to the first lifting sub-system;
- a second lifting sub-system including a second tether that couples the first lifting sub-system to the second lifting sub-system, wherein the second tether is selectively deployable in relation to the second lifting sub-system;
- and
- a power source that supplies power to one or both of the first lifting sub-system or the second lifting sub-system, wherein the aircraft receives power from the power source,
- wherein the first lifting sub-system is configured to independently lift the aircraft off and above ground to a first altitude,
- wherein the second lifting sub-system is configured to lift the first lifting sub-system and the aircraft off and above the ground so that the aircraft is at a second altitude that is greater than the first altitude,
- wherein the aircraft is operated to reach a launch airspeed at the second altitude and detach from the first tether after reaching the launch airspeed.
4 more elements
Dependencies are inferred from the claim text.