High Hardness and Toughness Alumina Ceramic Components for Drone Motor

• Application: Heat Exchanger, Refractory Lining, Thermal Insulation
• Material: Alumina Ceramic
• Shape: Rod
• Flexural Strength: 300MPa
• Max Use Temperature: 1600°c
• Color: White
• Processing Service: Welding, Moulding
• Material Option: 96%, 99%, 99.7% Alumina
• Type: Ceramic Plates
• Transport Package: Standard Safety Cartons with Plastic Foams
• Specification: Customized
• Trademark: INNOVACERA
• Origin: Fujian, China
• Production Capacity: 100000 Piece/Pieces Per Month

Product Description

 

According to different UAV design and performance requirements of drone, drone requests different components make by ceramic components. Different ceramic components play different role in the UAV and improve the drone overall performance. Such as zirconia ceramic axles for ultra mini motor driver , 99 alumina ceramic passive rotor and silicon carbide ceramic sleeve as wear resistance sleeve for the drone motor.These ceramic components already widely used for famous drone and play a very important roles in the drone rotating blade motor components.

 

Ceramic components for drone advantage

>Good heat resistance
> Good thermal conductivity

>High hardness and toughness

>High resistivity and dielectric constant

> Low dielectric loss and coefficient of thermal expansion

>Good wear resistance and extend the service life.

>Low density to reduce the overall weight of the UAV motor

More ceramic components will be used for drone motor and let's explore it together, welcome to send your customized design ceramic parts inquiry to research together.

 

Alumina Ceramic Property
Property		Unit	92% Alumina Ceramic	95% Alumina Ceramic	99% Alumina Ceramic
Density		g/cm3	≥3.63	≥3.68	≥3.83
Water absorption		%	O	O	O
Sintering temperature		°C	1500-1700	1600-1800	1700-1800
Hardness		HV	≥1400	≥1500	≥1650
Flexural strength		Kgf/cm2	3000	3000	3000
Compressive strength		Kgf/cm2	24000	25000	26000
Fracture toughness		Map.m3/2	3~4	3~4	4~5
Maximum temperature		°C	1600	1700	1800
Coefficient of thermal expansion		/°C	8*10-6	8*10-6	8*10-6
Heat shock		T(°C)	220	220	220
Thermal conductivity		W/m.k(25-300°C)	25 14	25 14	25 14
	20°C		>1012	>1012	>1012