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Unknown BrandSKU: 60862
Aviation piston engine with electronic fuel injection x400
Two-stroke horizontally opposed 4-cylinder piston aircraft engine.
$8,081.40
USD · Оптовые цены
В наличииДостаточно на складе
Категории:
1
Сертификаты
CEFCCRoHS
Доставка 7-14 дней
DHL/FedEx/UPS/авиа/море
Оригинал гарантирован
Официальные поставщики
Полный пакет документов
ECCN, CO, CI, PL, EUS docs
Поддержка 24/7
До и после продажи
Экспортный контроль
9A012Код ECCN9A012
КлассификацияБеспилотные летательные аппараты
Основания
NSMTRS
РегионыВесь мир кроме эмбарго/санкций
Уровень клиентаПроверенный B2B (KYC + заявление конечного пользователя)
ЛицензияТребуется лицензия
AI уверенность 75% · Лицензия требуется для некоторых направлений. Для союзников могут применяться исключения GBS/CIV.
Программа лояльности
Бронза
3%
$0k+
Серебро
6%
$10k+
Золото
10%
$50k+
Бриллиант
15%
$200k+
Скидка по уровню суммируется с оптовыми ценами
I. Main characteristics
- Model: x400 EFI
- Type: two-stroke horizontally opposed 4-cylinder piston aircraft engine
- Cooling method: air
- Lubrication method: oil mist (mixed lubrication system)
- Working volume (cubic capacity): 400 cc cm (400 cc)
- Minimum stable speed: ≤ 1200 rpm
- Maximum power: 48 hp / 35 kW at 6400 rpm
- Specific fuel consumption:
- 1) Cruise mode: ≤ 380 g/(kWh)
- 2) Maximum power mode: ≤ 480 g/(kWh)
- Fuel: gasoline with an octane rating of 92 and higher (mixture ratio with oil for two-stroke engines 50:1)
- Resource (Service life):
- 1) Time to first overhaul (TBO): ≥ 250 h
- 2) Total resource: ≥ 500 h
II. Weight and dimensions
- Engine net weight: 15 kg (including engine block, intake and exhaust components, electronic injection control unit)
- Dimensions (L×W×H): 370 × 320 × 280 mm
III. Fuel supply and control
- Fuel supply system: electronic fuel injection (EFI)
- Control method: capable of receiving commands from the control computer (or integrated on-board computer) and adjusting engine speed accordingly; capable of transmitting to the control computer parameters of throttle position, speed, intake temperature, cylinder temperature, exhaust gas temperature, etc..
IV. Startup and power generation
- The engine has an electric start function:
- 1) Number of starting attempts: the engine must start successfully within 3 attempts.
- 2) Low Temperature Starting: The engine can be started in low temperature conditions down to -40°C (use of the included preheating equipment is acceptable).
- Generation power: ≥ 2 kW.
V. Environmental Conditions (Adaptability)
- Operating temperature: -50°C to +55°C (start at -40°C, auxiliary heating possible).
- Storage temperature: -50°C to +65°C.
- Relative Humidity: (95±5)% (at 30°C ~ 60°C).
- Vibration: ≥ 2g (15Hz ~ 500Hz ~ 15Hz).
- Shock loads: vertically ≥ 20g, along the transverse and longitudinal axes ≥ 15g.
- Low pressure: Capable of withstanding low pressure conditions equivalent to an altitude of 7000 m.
- Salt fog: is resistant to salt spray.
- Mold: is resistant to mold fungi.
- Rain: Provides protection from moderate rain.
- Application altitude: capable of starting and operating normally in high mountain conditions at an altitude of up to 5000 meters.
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