Product

Product

Product Introduction

AEC2.0L engine is self-developed by WDAE and has broken through a number of core technologies, among which, the engine electronic control system is the first set of electronic control system for civil aviation piston engine in China to complete the airworthiness validation process, realizing a zero breakthrough in the industry.  The engine has obtained the Type Certificate (TC) and Production Certificate (PC) issued by CAAC, and is qualified for large-scale production, which can provide safe and reliable flying power to the market and customers.

Product Parameters

Configuration

Inline Four-Cylinder Four-Stroke

Ignition Type

Compression

Cooling Method

Liquid Cooling

Displacement

2.0 L

MTOP

123.5 kW @ 3887 rpm

MCP

123.5 kW @ 3887 rpm

Altitud

5500 m

Fuel Type

Jet Fuel, Disel

Min. SFC

200 g/kW·h

Dry Weight

<180 kg

Dimension

767×854×575 mm

Min. Starting Ambient Temp.

-30℃ (-22℉)

Slide Oil Temp. (Normal Operation)

50℃-135℃ (122℉-275℉)

TBO

>1800 h

Application

DA42NG/CA42/DA40NG/UAV

Application Scenario

1. CA42 powered by AEC2.0L engine

2. HH-100 unmanned aircraft powered by AEC2.0L engine

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