ChinaDrone.Request a quote ↗
COMPONENT

BE-15C

By Jining Yunbao Technology Co,Ltd ↗

A carbureted engine for UAV applications.

Request a quote ↗
Jining Yunbao Technology Co,Ltd BE-15C Engine
Jining Yunbao Technology Co,Ltd BE-15C Engine

Product overview

The engine uses a twin-cylinder, single-intake design.

Equipped with a diaphragm carburetor, the engine supports 360° mounting orientations.

It runs on ordinary automotive gasoline.

The front shaft supports a propeller or reduction gearbox, while the rear shaft supports a starter-generator or coupling.

A built-in throttle servo bracket facilitates installation and maintenance.

Optional generators can supply continuous electrical power to the system.

Specifications

SpecificationValue & conditions
Mounting orientation360°For the engine equipped with the described diaphragm carburetor.
SOURCE WITH CHINADRONE

Request a quote for BE-15C

Send your application, destination country and expected quantity to the ChinaDrone team. We can discuss product selection, configuration and sourcing from China.

Submit your procurement requirements ↗

No account needed. A model number is optional. Your enquiry is handled by ChinaDrone.

KEEP EXPLORING

Similar products

Browse all products ↗
Motors & ESCs

T-MOTOR Air Gear 355 (Quick-Release Version)

By T-MOTOR

The T-MOTOR Air Gear 355 (Quick-Release Version) is a multirotor propulsion combo comprising AIR2213/KV1000 motors, MF9545 quick-release propellers and an AIR 20A four-in-one ESC. It supports recommended 3~4S LiPo operation and several multirotor layouts, with defined aircraft weight ranges, propeller operating limits and a 25% loss allowance for coaxial configurations.

EMAX E3 2814 brushless motor with threaded shaft and black wires
Motors & ESCs

EMAX E3 2814 Brushless Motor

By EMAX

The EMAX E3 2814 Brushless Motor is a propulsion component for 8-10 inch FPV aircraft used for long-range, cinematic and high-load flying. Available in 850KV and 1100KV configurations for 3-6S systems, it combines a metal housing and outer-rotor architecture with defined mounting, wiring and propeller interfaces for aircraft integration.