IP Library Granted Patent US 12,409,948
Granted Patent B2
US 12,409,948 · App. 18/279,417 · Granted Sep 9, 2025

Lightning induction system and method therefor

Inventors: Masato Maruyama (Musashino, JP); Jun Kato (Musashino, JP); Toshihisa Masuda (Musashino, JP); Naomichi Nakamura (Musashino, JP)
Assignee: Nippon Telegraph and Telephone Corporation
B64D45/02B64U2101/00
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 12,409,948
App. No.
18/279,417
Granted
Sep 9, 2025
Kind
B2
Abstract

A lightning induction system includes a plurality of flight vehicles 3 that fly between a lightning originating point 1 in the sky where lightning is generated and a ground surface 2 . The flight vehicles 3 each include: a flight unit 10 that generates lift force and propulsion force; a conductor cable 20 that is engaged with the flight unit 10 , extends downward, and has a predetermined length; and a weight unit 30 connected to the lower end of the conductor cable 20 . The flight unit 10 is disposed in a Faraday cage 11 . The Faraday cage 11 has a sphere shape, and the flight unit 10 is fixed by a support pillar 12 extending downward from the inner side of the top of the sphere.

Claims (22)

1. A lightning induction system comprising a plurality of flight vehicles that fly between a lightning originating point in the sky where lightning is generated and a ground surface,

wherein the flight vehicles each include:

a flight unit that generates lift force and propulsion force;

a conductor cable that is engaged with the flight unit, extends downward, and has a predetermined length; and

a weight unit connected to a lower end of the conductor cable, wherein a conductor cable of an upper flight vehicle is configured to induce an energy of the lightning that has struck a flight unit of the upper flight vehicle to a lower flight vehicle through the weight unit.

2. The lightning induction system according to claim 1 , wherein

the weight unit engaged with a first flight unit of flight units includes an altitude detection unit that measures an altitude and transmits the measured altitude to a second flight unit, and

wherein the second flight unit includes a flight control unit that receives the measured altitude and controls the lift force so as to maintain a predetermined altitude difference from the weight unit of the first flight unit,

wherein the first flight unit and the second flight unit form a relay of lightning induction path to the ground.

3. The lightning induction system of claim 1 , further comprising:

a first conductor cable that is engaged with a first flight unit of flight units, extending in a horizontal direction; and

a second conductor cable that is engaged with a second flight unit of the flight units, extending in a horizontal direction,

wherein the first conductor cable and the second conductor cable are oriented in a substantially horizontal direction between the first flight unit and the second flight unit, wherein the first flight unit and the second flight unit form a horizontal relay of lightning induction path.

4. The lightning induction system according to claim 1 , wherein the flight unit is disposed in a Faraday cage.

5. The lightning induction system according to claim 4 , wherein

the Faraday cage has a sphere shape, and

the flight unit is fixed by a support pillar extending downward from an inner side of a top of the Faraday cage.

6. A lightning induction method for inducing energy of lightning striking a ground surface from a lightning originating point in the sky where lightning is generated, to the ground surface via a plurality of flight vehicles,

wherein the flight vehicles each include:

a flight unit that generates lift force and propulsion force;

a conductor cable that is engaged with the flight unit, extends downward, and has a predetermined length; and

a weight unit connected to a lower end of the conductor cable, wherein a conductor cable of an upper flight vehicle is configured to induce an energy of the lightning that has struck a flight unit of the upper flight vehicle to a lower flight vehicle through the weight unit.

Assignments (2)
CHANGE OF NAME Recorded Aug 14, 2025
From: NIPPON TELEGRAPH AND TELEPHONE CORPORATION
To: NTT, INC.
Reel/Frame 072471/0579 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 27, 2023
From: MARUYAMA, MASATO; KATO, JUN; MASUDA, TOSHIHISA; NAKAMURA, NAOMICHI
To: NIPPON TELEGRAPH AND TELEPHONE CORPORATION
Reel/Frame 065368/0162 →
Continuity (1)
Related Publication 20240182168A1 · Jun 6, 2024
References Cited (9)
US 20100212925A1 · Canham · 2010 [cited by examiner]
US 20170283053A1 · Toda · 2017 [cited by examiner]
CN 107539466 · 2018 [cited by applicant]
DE 102022002219A1 · 2023 [cited by examiner]
KR 20170033625 · 2017 [cited by applicant]
KR 20170033625A · 2017 [cited by examiner]
WO WO2015049798 · 2015 [cited by applicant]
Monoist.co.jp [online], “A system that prevents lightning strike damage with drones,” Nov. 2020, retrieved on Aug. 29, 2023, retreived from URL<https://monoist.atmarkit.co.jp/mn/articles/2011/20/news052.html>, 7 pages (… [cited by applicant]
[No Author Listed], “Lightning control and charging technology,” NTT R&D Forum 2020 Connect, online, Nov. 17-20, 2020, 2 pages (with English translation). [cited by applicant]