公开(公告)号：US20230072207A1

公开(公告)日：2023-03-09

申请号：US17900770

申请日：2022-08-31

Applicant: Khalifa University of Science and Technology

Inventor： Rajkumar MUTHUSAMY ,  Huda Alyammahi ,  Muhammad Umer Hameed Shah ,  Omar Fuad Faris ,  Irfan Hussain ,  Yahya Hashem Zweiri ,  Dongming Gan ,  Seneviratne Mudigansalage Seneviratne

IPC: B25J19/02 ,  B25J13/08

Abstract: A robotic manipulator is described. The robotic manipulator includes a rigid or semi-rigid end effector that engages with objects and a sensor that detects data associated with the object. For example, the sensor can include an optical sensor or a vision-based tactile sensor that detects data associated with the object.

公开(公告)号：US12280495B2

公开(公告)日：2025-04-22

申请号：US17900770

申请日：2022-08-31

Applicant: Khalifa University of Science and Technology

Inventor： Rajkumar Muthusamy ,  Huda Alyammahi ,  Muhammad Umer Hameed Shah ,  Omar Fuad Faris ,  Irfan Hussain ,  Yahya Hashem Zweiri ,  Dongming Gan ,  Seneviratne Mudigansalage Seneviratne

IPC: B25J19/02 ,  B25J13/08

Abstract: A robotic manipulator is described. The robotic manipulator includes a rigid or semi-rigid end effector that engages with objects and a sensor that detects data associated with the object. For example, the sensor can include an optical sensor or a vision-based tactile sensor that detects data associated with the object.

公开(公告)号：US12037095B2

公开(公告)日：2024-07-16

申请号：US17430174

申请日：2020-02-10

Applicant: Khalifa University of Science and Technology

Inventor： Yahya Hashem Zweiri ,  Yahya Taha Al-Majali

IPC: B63G8/18 ,  B64C15/12 ,  B64C29/00 ,  B64C29/02 ,  B64U30/20 ,  B63G8/00 ,  B64U10/25 ,  B64U50/13

CPC classification number: B63G8/18 ,  B64C15/12 ,  B64C29/0033 ,  B64C29/02 ,  B63G2008/004 ,  B64U10/25 ,  B64U30/20 ,  B64U50/13

Abstract: The invention provides for a hybrid unmanned aerial and submersible vehicle (UASV) (100) comprising a fuselage (102), at least one wing structure (104, 106), a propulsion system (116, 118) and an empennage. The said vehicle is capable of operating in air, on water and underwater via its wing tilting mechanism wherein the transition of the vehicle between different mediums is seamless. Further, the wing structures (104, 106) are connected on either side of the fuselage (102), such that each wing (104, 106) tilts about a common lateral axis (360° of freedom), and wherein said tilting depends on the mode of operation of the UASV (100). The vehicle of the present invention further includes a propeller protection system, a landing system, control surfaces, and sensors. The present invention also discloses methods for operating the UASV (100) in multiple mediums.