Wind & Renewable Energy Patents
Airborne Wind Energy Patents
Tethered kites and drones flying crosswind to harvest high-altitude wind — where autonomous flight-control reliability is the make-or-break and fly-gen vs ground-gen is the core architectural split — airborne-wind-energy patent landscape for renewable-energy and aerospace founders.
FAQ
Who holds airborne wind energy patents and why does AWE matter (and why has it struggled)?
Airborne wind energy patents cover kite/wing innovations; tether innovations; ground-station/generator innovations; and control/autonomy innovations — with IP held by airborne-wind companies, wind/energy companies, and research organizations. WHY AIRBORNE WIND ENERGY: AIRBORNE WIND ENERGY (AWE) harvests the stronger, steadier wind at HIGH ALTITUDE using a TETHERED kite, wing, or drone instead of a tall, material-heavy tower; the wing flies CROSSWIND — sweeping fast loops (a 'FIGURE-EIGHT' or circular path) perpendicular to the wind — so that, like the tip of a conventional turbine blade, it travels much faster than the wind and generates far more power than its modest size would suggest; there are TWO core architectures: FLY-GEN (onboard turbines mounted on the wing generate electricity in the air, which is sent DOWN a CONDUCTIVE TETHER to the ground — Makani's approach) and GROUND-GEN / PUMPING (the wing pulls the TETHER OUT under high tension, spinning a GROUND-based generator via a winch/drum during the 'reel-out' power phase, then the wing is de-powered and the tether REELED back IN cheaply during a 'reel-in' phase — yielding net positive energy per pumping cycle); the PROMISE is compelling — for the same swept area you use FAR LESS material than a steel-and-concrete tower, and you reach higher, steadier winds unavailable to fixed turbines; the CATCH is that it is brutally hard to do RELIABLY. The brutal CHALLENGES: the CONTROL/AUTONOMY (autonomously launching, flying crosswind, and landing the wing reliably for 20+ years through gusts, wind shifts, and component faults — the central make-or-break, and the single hardest problem), the TETHER (strength-to-weight, aerodynamic DRAG, electrical conductivity for fly-gen, and WEAR/FATIGUE over millions of bending cycles), the KITE/WING (rigid vs soft wing aerodynamics, structure, and any onboard turbines), and the GROUND STATION/GENERATOR plus SAFETY and AIRSPACE. MAJOR PLAYERS: MAKANI (Google X / Alphabet — a fly-gen pioneer that WOUND DOWN in 2020, after which Alphabet pledged its AWE patent portfolio as a non-assertion / open resource for the field), KITEPOWER, SKYSAILS POWER, TWINGTEC, WINDLIFT, and the now-defunct AMPYX POWER. HONEST CAVEAT: AWE is still PRE-COMMERCIAL — no AWE system is yet a proven, bankable, utility-scale product, and several of its best-funded leaders (Makani, Ampyx) have SHUT DOWN. The reason is the same one that defines the IP: autonomous flight RELIABILITY over a 20-year life is unforgiving. Kite/wing, tether, ground-station/generator, and control/autonomy are the core AWE patent domains. (Note: the airborne devices (KITE/WING, TETHER, GROUND STATION) are device IP and the CONTROL methods are PROCESS IP — §101-RESILIENT when tied to the physical system — so claim the wing, tether, ground station, and control methods.)
What kite/wing and tether innovations are patentable?
Kite/wing innovations; tether innovations; rigid-wing and soft-wing innovations; and conductive-tether innovations represent core airborne-wind-energy patent domains — and the kite/wing (the airborne harvester) and the tether (the lifeline) are foundational, high-value, §101-resilient capabilities. KITE/WING PATENTS: the airborne harvester — RIGID WING (a fixed-structure aircraft-like wing, often carrying onboard turbines for fly-gen — high aerodynamic efficiency and controllability, but heavier and harder to launch/land, the Makani-style approach), SOFT WING / KITE (a flexible, lightweight inflatable or fabric kite — cheap, packable, crash-tolerant, favored by ground-gen players like Kitepower and SkySails, but with lower efficiency and harder shape control), CROSSWIND AERODYNAMICS (wing shape, control surfaces, and bridle/depower systems that let the wing fly fast figure-eight or circular loops and modulate lift between the power and recovery phases), and ONBOARD TURBINES (for fly-gen, the rotors/generators carried ON the wing that also serve as propellers for hover launch/landing); wing methods are core, high-value, DISTINCTIVE structural/aerodynamic IP, §101-resilient (rigid vs soft wing designs, crosswind aero, depower, and onboard turbines are the central, contested, defensible IP, since the wing is what actually harvests the wind and the rigid-vs-soft choice drives the whole architecture). TETHER PATENTS: the lifeline — HIGH-STRENGTH LOW-DRAG TETHER (a rope of ultra-high-strength fiber (e.g., UHMWPE/aramid) that must carry enormous tension at minimal weight AND minimal aerodynamic DRAG, since tether drag is a dominant loss as the line sweeps through the air), CONDUCTIVE TETHER (for fly-gen, integrating copper/aluminum conductors to carry power and signals down to the ground while staying flexible and strong — a hard combined electrical-and-mechanical design), TETHER WEAR/FATIGUE (surviving millions of bending, abrasion, and tension cycles over a vehicle's reel-in/reel-out life — fatigue and wear are a key reliability and replacement-cost problem), and TERMINATION/SENSING (anchoring, strain relief, and embedded sensing); tether methods are core, high-value, DISTINCTIVE IP, §101-resilient (high-strength low-DRAG tethers, conductive tethers for fly-gen, and WEAR/FATIGUE solutions are the central, contested, defensible IP, since the tether's drag, weight, conductivity, and lifetime cap what the whole system can achieve). RIGID-WING / SOFT-WING PATENTS: the architectural split — rigid wings (efficient, fly-gen-friendly) vs soft kites (cheap, packable, ground-gen-friendly); wing-type methods are high-value structural IP, §101-resilient (the wing type is the device). CONDUCTIVE-TETHER PATENTS: power-and-signal-carrying tethers for fly-gen; conductive-tether methods are high-value IP, §101-resilient (the conductive tether is the fly-gen lifeline). Kite/wing, tether, rigid/soft-wing, and conductive-tether are the highest-value core IP because the wing harvests the wind and the tether's strength, drag, conductivity, and fatigue life set the ceiling on what airborne wind can deliver.
What ground-station/generator and control/autonomy innovations are patentable?
Ground-station/generator innovations; control/autonomy innovations; pumping/ground-gen innovations; and autonomous-crosswind-flight innovations represent additional airborne-wind-energy patent domains — and the ground station/generator (where power is made or landed) and the control/autonomy (the HEART) turn the wing and tether into a working power plant. GROUND STATION/GENERATOR PATENTS: where it comes together — PUMPING / GROUND-GEN WINCH + GENERATOR (the drum/winch and generator that the tether drives during reel-out, plus the motoring drive that reels the de-powered wing back in cheaply — including the power-smoothing needed because pumping makes power in pulsed cycles, not continuously), FLY-GEN POWER ELECTRONICS (for fly-gen, the ground-side converters/inverters that condition power arriving down the conductive tether and feed the grid), LAUNCH/LAND SYSTEM (the mast, perch, or vertical-takeoff scheme that gets the wing safely into the air and back down — autonomous launch and recovery is one of the hardest, most failure-prone steps), and SAFETY/AIRSPACE/SITING (containment, fail-safe descent, and airspace integration); ground-station methods are core, high-value, DISTINCTIVE IP, §101-resilient when tied to the system (the PUMPING winch+generator, fly-gen power electronics, and LAUNCH/LAND system are core, contested, defensible IP, since converting tether motion to grid power — and reliably launching and landing — is half the machine). CONTROL/AUTONOMY PATENTS: the HEART — AUTONOMOUS CROSSWIND FLIGHT CONTROL (the closed-loop control laws that fly the wing in stable, optimal figure-eight/circular loops, maximize power, and manage the power/recovery (or reel-out/reel-in) cycle), SENSING/STATE ESTIMATION (estimating wing position, attitude, airspeed, tether tension, and wind from onboard and ground sensors), FAULT HANDLING / FAIL-SAFE (detecting gusts, wind drop-outs, actuator or sensor faults and recovering or landing safely — the crux of 20-year reliability), and AUTONOMOUS LAUNCH/LAND CONTROL; control methods are core, high-value, DISTINCTIVE PROCESS IP, §101-resilient when tied to the system (AUTONOMOUS CROSSWIND CONTROL and FAULT HANDLING are THE core, contested, defensible IP, since reliable autonomous flight for two decades is the make-or-break that has DEFEATED well-funded leaders — solving it is the whole game). PUMPING/GROUND-GEN PATENTS: tether-driven winch+generator pumping systems; pumping methods are high-value IP, §101-resilient when tied to the system (ground-gen pumping is the dominant commercial architecture today). AUTONOMOUS-CROSSWIND-FLIGHT PATENTS: control laws for autonomous crosswind power flight; autonomous-flight methods are high-value PROCESS IP, §101-resilient when tied to the system (autonomous flight is the heart). Ground-station/generator, control/autonomy, pumping/ground-gen, and autonomous-crosswind-flight are the highest-value IP because the ground station makes or lands the power and autonomous control reliability is the single problem that decides whether AWE works at all.
What IP strategy should airborne wind energy startup founders use?
Airborne wind energy startup IP strategy must navigate the devices-and-control-are-§101-resilient (AWE IP is DEVICE IP (kite/wing, tether, ground station) and PROCESS IP (control methods) — §101-RESILIENT when tied to the physical system — so wing, tether, ground-station, and control-method claims are strong; pure abstract algorithms claimed alone are weaker, so always tie control claims to the wing/tether/ground hardware), the autonomous-control-reliability-is-the-central-make-or-break (the single hardest, most decisive problem is RELIABLY launching, flying crosswind, and landing the wing AUTONOMOUSLY for 20+ years through gusts and faults — this, not raw aerodynamics, is why AWE is hard and why leaders have FAILED, so the control/autonomy + fault-handling IP and demonstrated reliability are the true make-or-break), the fly-gen-vs-ground-gen-is-the-core-architectural-split (the field forks into FLY-GEN (onboard turbines + conductive tether — efficient, but heavy, complex, conductive-tether-dependent — Makani's path) and GROUND-GEN/PUMPING (tether spins a ground winch+generator in reel-out/reel-in cycles — simpler airborne unit, soft kites, dominant today — Kitepower/SkySails/TwingTec) — pick a side, since it drives wing, tether, and ground-station IP), the soft-kite-vs-rigid-wing-tradeoff (soft kites are cheap, packable, crash-tolerant, and ground-gen-friendly but lower-efficiency and harder to control; rigid wings are efficient and fly-gen-friendly but heavy and launch/land-hard — a core design+IP fork), the tether-is-a-first-order-constraint (tether DRAG, weight, conductivity (for fly-gen), and WEAR/FATIGUE directly cap performance and drive replacement cost — first-order IP, not a detail), the pre-commercial-and-leaders-have-failed-reality (be HONEST: AWE is PRE-COMMERCIAL — no bankable utility-scale product yet, and Makani (Google X) and Ampyx Power SHUT DOWN — so investors and the IP story must center demonstrated RELIABILITY and a credible path, not just patents), the makani-patent-pledge-is-a-field-resource (Alphabet wound down Makani in 2020 and pledged its substantial AWE patent portfolio as a NON-ASSERTION / open resource — a notable, well-documented field asset to understand for both FTO and learning — do NOT, however, treat 'open' as infinite freedom; verify scope), the safety-airspace-and-siting-are-gating (autonomous flying tethered craft raise real safety, fail-safe-descent, and AIRSPACE/permitting questions that gate deployment — IP and design must address containment and fail-safe), the demonstrated-reliability-capacity-factor-and-LCOE-decide (AWE is proven by demonstrated autonomous flight HOURS, RELIABILITY/availability, capacity factor, and LCOE vs conventional wind — honest, demonstrated reliability is decisive, far more than patents, in a field where lab/demo promise has repeatedly failed to scale), the wing-tether-groundstation-vs-control-business-models (a startup can lead with a wing/tether/ground-station hardware edge or a control/autonomy software edge — but the durable moat is the integrated system + proven reliability), and the incumbent-and-FTO (Makani's pledged portfolio, Kitepower, SkySails Power, TwingTec, Windlift, and academia hold AWE IP — so a startup needs a genuinely novel wing/tether/ground-station/control edge, demonstrated reliability, and FTO); understand that autonomous control reliability is the central make-or-break and fly-gen vs ground-gen is the core architectural split, so the durable startup IP is in autonomous crosswind control + fault handling, a chosen architecture's wing/tether/ground-station, and demonstrated 20-year-credible reliability — with proven autonomous reliability the real moat, and that §101-resilient device + control-method IP, demonstrated flight hours/reliability/capacity-factor/LCOE, and FTO matter as much as patents; identify whitespace in control/autonomy, low-drag/conductive tethers, and launch/land systems. AIRBORNE WIND ENERGY STARTUP IP STRATEGY: KITE/WING, TETHER, GROUND-STATION/GENERATOR, AND CONTROL/AUTONOMY ARE THE IP: patent the wing, tether, ground station, and control methods — device + process claims (§101-resilient when tied to the system); DEVICES-AND-CONTROL-ARE-§101-RESILIENT: DEVICE IP (kite/wing, tether, ground station) + control PROCESS IP — §101-RESILIENT tied to the physical system (tie control claims to hardware); AUTONOMOUS-CONTROL-RELIABILITY-IS-THE-CENTRAL-MAKE-OR-BREAK: reliably launching, flying crosswind, and landing AUTONOMOUSLY for 20+ years through gusts/faults is the hardest, most decisive problem — and why leaders FAILED; FLY-GEN-VS-GROUND-GEN-IS-THE-CORE-ARCHITECTURAL-SPLIT: FLY-GEN (onboard turbines + conductive tether — Makani) vs GROUND-GEN/PUMPING (tether spins a ground winch+generator, reel-out/reel-in — dominant today) — pick a side; SOFT-KITE-VS-RIGID-WING-TRADEOFF: soft kites (cheap/packable/ground-gen) vs rigid wings (efficient/fly-gen/launch-hard) — a core fork; TETHER-IS-A-FIRST-ORDER-CONSTRAINT: tether DRAG/weight/conductivity/WEAR-FATIGUE cap performance and drive replacement cost; PRE-COMMERCIAL-AND-LEADERS-HAVE-FAILED-REALITY: AWE is PRE-COMMERCIAL — no bankable utility-scale product, and Makani (Google X) + Ampyx Power SHUT DOWN — center demonstrated RELIABILITY; MAKANI-PATENT-PLEDGE-IS-A-FIELD-RESOURCE: Alphabet pledged Makani's AWE portfolio as a NON-ASSERTION / open resource (verify scope, useful for FTO + learning); SAFETY-AIRSPACE-AND-SITING-ARE-GATING: autonomous tethered craft raise safety/fail-safe/AIRSPACE/permitting issues — address containment + fail-safe; DEMONSTRATED-RELIABILITY-CAPACITY-FACTOR-AND-LCOE-DECIDE: proven by autonomous flight HOURS/RELIABILITY/capacity factor/LCOE vs conventional wind — demonstrated reliability decisive (demo promise has repeatedly failed to scale); WING-TETHER-GROUNDSTATION-VS-CONTROL-BUSINESS-MODELS: lead with hardware (wing/tether/ground station) or control/autonomy software — but the moat is the integrated system + reliability; INCUMBENT-AND-FTO: Makani's pledged portfolio + Kitepower/SkySails Power/TwingTec/Windlift + academia — need a novel edge + demonstrated reliability + FTO; WHEN TO PATENT: NOVEL WING/TETHER/GROUND-STATION/CONTROL WITH DATA: file once it shows data (a control law + wing/tether/ground station + demonstrated flight/reliability) — device + process claims; demonstrated autonomous flight hours, reliability, capacity factor, and LCOE are the critical AWE IP metrics; KEY FTO CHECKLIST: Makani's pledged portfolio + Kitepower/SkySails Power/TwingTec/Windlift + academia; kite/wing (RIGID vs SOFT wing/crosswind aero/depower/onboard turbines — §101-resilient, the airborne harvester); tether (high-strength LOW-DRAG/CONDUCTIVE for fly-gen/WEAR-FATIGUE — §101-resilient, the lifeline); rigid-wing/soft-wing; conductive-tether (the fly-gen lifeline); ground station/generator (PUMPING winch+generator/fly-gen power electronics/LAUNCH-LAND system/safety-airspace — §101-resilient tied to system, where power is made/landed); control/autonomy (AUTONOMOUS CROSSWIND CONTROL/sensing/FAULT HANDLING-fail-safe/launch-land control — §101-resilient tied to system, THE heart and make-or-break); pumping/ground-gen (dominant architecture); autonomous-crosswind-flight (the heart); device + control-method the §101-resilient strength; autonomous control reliability the central make-or-break; fly-gen vs ground-gen the core architectural split; soft kite vs rigid wing a core fork; tether a first-order constraint; pre-commercial + leaders have failed (Makani, Ampyx) — center demonstrated reliability; Makani patent pledge a field resource; safety + airspace + siting gating; demonstrated reliability + capacity-factor + LCOE decide.
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