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Main data and specifications of the air source unit

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Air Source Unit Technical Specifications

1.1.1 Dimensions

Overall length of the machine (mm): L = 7150

Overall width of the machine (mm): W = 2260

Overall height of the machine (mm): H = 3000

1.1.2 Main Technical Parameters of the Air Source Unit

● Supply pressure: Startup supply: 35 (0.241 MPa) - 42 (0.29 MPa) psi, adjustable (factory set at 38 psi) Auxiliary supply: 25 - 32 psi, adjustable (factory set at 28 psi)

● Supply flow rate: 300 ppm = 2.267 kg/s

● Supply temperature: ≤ 220℃

● Minimum turning radius: ≤ 15m

● Minimum ground clearance: ≥ 190mm

1.1.3 Main Configuration of the Air Source Unit

● Vehicle chassis

Model: Qingling 700P (QL1080A8KAY)

Axle spacing: 3815mm

Wheel spacing: Front wheels 1680mm; Rear wheels 1650mm

Manufacturer: Chongqing Qingling Automobile Company

● Engine

Model: TCD2015V08

Type: Inline, 8-cylinder, turbocharged (air-to-air) water-cooled, multi-function electronic fuel injection diesel engine

Compression ratio: 20.8:1

Displacement: 15.87L

Cylinder diameter: 132mm

Stroke: 145mm

Rated/Maximum power: 440/520 kW

Rated/Maximum speed: 1900/2100 rpm

Fuel consumption rate: 211g/kWh

Electricity: 24V

Manufacturer: DAIKIN Engine Co., Ltd. Compressor

Model: GHH CD42S

Type: Air-cooled, oil-free, double-screw rotary compressor

Flow rate: 290 lbs/min (131.5 kg/min)

(Compressor inlet temperature 20℃, inlet pressure 1 bar absolute, relative humidity ≤ 80%) Engine speed during startup of supply air: 2100 rpm

Manufacturer: Germany GHH

1.2 Product Standards

TYAS290 aircraft starting air supply vehicle complies with the following standard requirements:

IATA AHM976 aircraft air supply vehicle functional indicators

IATA AHM905 reference materials for civil aircraft ground support equipment

IATA AHM910 basic requirements for aircraft ground support equipment

IATA AHM913 basic safety requirements for aircraft ground support equipment

IATA AHM916 basic requirements for towing interfaces of apron equipment

ISO2026: 1974 aircraft engine starting air supply interface

SAE RP 4087 position and type standards for aircraft ground service interfaces

Q/TYT 001-2018 enterprise standard for aircraft starting air supply vehicle

1.3 Operating Conditions

Altitude does not exceed 4000 m;

Environmental temperature: -40 ℃ to +50 ℃;

Air relative humidity: ≤ 95%. 1.4 Applicable Aircraft Models

Boeing 707, 717, 727, 737 series, 757, 767, 747 series, some B777, DC8, DC9, DC10, MD80 series, MD90, MD11, Airbus A320 series, A340 series, A300, A310, A330, that is, all aircraft models except those using GE90 engines.

Aircraft Air Start Unit


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Jiangsu Tianyi Aviation Industry Co., Ltd.
 
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