H3 Dynamics Holdings Pte. Ltd.

Harshavardhan Thakar

Taras Wankewycz

Matthew Mehmet Crawford

Cher Chuan Lee

Bo Han

Mehmet Kesmez

The application provides an autonomous refueling vehicle for a hydrogen-electric aircraft, which includes two or more wings. The wings are provided with one or more removable electric propulsion pods. The autonomous refueling vehicle includes a hydrogen refueling module adapted to connect to the propulsion pods and to a hydrogen source. The autonomous refueling vehicle includes also includes a propulsion pod handling device, which is adapted to remove the propulsion pod from the wings and to position the propulsion pods on the hydrogen refueling module such that the propulsion pods are connected to the hydrogen refueling module. The autonomous refueling vehicle is also adapted to autonomously move itself to the hydrogen source to allow the hydrogen refueling module to removably connect to the hydrogen source for refueling of the propulsion pods.

Unmanned vehicle

An unmanned vehicle module can include, in some aspects, a landing platform including a landing area for receiving an unmanned vehicle, wherein the landing area includes a predetermined charging region; a first charging plate; a second charging plate, wherein the first charging plate and the second charging plate are positioned in the predetermined charging region; an electrical energy storage device for connecting electrically with the first charging plate and with the second charging plate; and an unmanned vehicle alignment mechanism configured to move the unmanned vehicle into the predetermined charging region; wherein the unmanned vehicle alignment mechanism includes a first beam, a second beam, a third beam, a fourth beam, and an actuation device for actuating at least two of the first beam, the second beam, the third beam, and the fourth beam to push the unmanned vehicle into the charging region.

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Singapore, Singapore

Harshavardhan Thakar