Long-endurance oil-electric hybrid unmanned aerial vehicle
By designing a hybrid electric drone, the rotor system is directly driven by a fuel engine. Combined with the transmission system and clutch differential rotor technology, the problem of insufficient range of existing drones is solved, and a longer flight time is achieved.
CN224529040UActive Publication Date: 2026-07-21李宏利
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Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- 李宏利
- Filing Date
- 2025-09-16
- Publication Date
- 2026-07-21
AI Technical Summary
Technical Problem
The short flight range of existing drones is due to the fact that the mechanical energy output by the fuel engine needs to be converted into electrical energy to drive the motor, resulting in significant energy conversion losses.
Method used
The drone adopts a hybrid electric design, which directly drives the rotor system through a fuel engine, using fuel to provide the main energy. The battery module assists in controlling the drone's attitude and balance. The transmission system enables synchronous operation of multiple rotors, and the rotor differential speed is achieved through a clutch and a secondary drive unit to reduce energy conversion losses.
Benefits of technology
This improved the drone's range, reduced energy conversion losses, and enabled longer flight times.
✦ Generated by Eureka AI based on patent content.
Smart Images
Figure CN224529040U_ABST
Abstract
The utility model relates to an unmanned plane technical field discloses a long endurance oil electricity hybrid unmanned plane, including frame, energy system, rotor system, energy system and rotor system transmission connection, still include: transmission system for transmitting the power output of energy system to the rotor system on, the rotor system includes the installation shell, installs the upper wing unit, lower wing unit, auxiliary drive unit on the installation shell, transmission system drives the upper wing unit, lower wing unit simultaneously, auxiliary drive unit is used for adjusting the rotating speed of lower wing unit, the utility model discloses a fuel provides main energy, directly the mechanical energy of fuel engine generates transmission to the rotor, makes unmanned plane lift off, avoids the mechanical energy conversion into electric energy, then electric energy is converted into mechanical energy, has reduced energy conversion loss, with the battery module energy as the auxiliary, controls unmanned plane to turn to and keeps fuselage balance, that is through the mode of oil as the main, electricity as the auxiliary, compared with prior art can obtain longer endurance mileage.
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