• Ana Sayfa
  • Firma Profili
  • Ürünler
  • Referanslar
  • İletişim
Ürünler
Havacılık Eğitim Sistemleri
Güç Sistemleri
         Pistonlu Motor Modeli
         Pistonlu Motor Kesiti
         Turboşaft Allison 250 Motor Modeli
         Turboşaft Motor Kesiti
         Turbofan Motor Modeli
         Turbojet Motor Modeli
         JT8D Turbofan Motor Kesiti
         CF700 Turbofan Motor Kesiti
         PT6A Motor Modeli
         PT6A Turboprop Motor Kesiti
         Motor Sökme & Takma Eğitim Seti
         Türbin Motor Eğitim Seti–Konfigürasyon 1
Türbin Motor Eğitim Seti–Konfigürasyon 2
         Thrust Reverser Eğitim Seti
         Uçak Yedek Güç Ünitesi (APU) Eğitim Seti
         Çalıştırılabilir (APU)
         Pistonlu Motor Eğitim Seti
         Pistonlu Motor Veri Toplama Sistemi
         Turboprop Motor Eğitim Seti
         Turboşaft Motor Eğitim Seti
         Türbin Motor Eğitim Seti
         Uçak Yakıt Sistemi Eğitim Seti
         TCM Yakıt Enjeksiyon Sistemi Eğitim Seti
         Sabit Hızlı Pervane Eğitim Seti
         Uçak Pervane Sistemi Eğitim Seti
Gövde Sistemleri
Aviyonik Sistemler
Bilgisayar Tabanlı Eğitim Yazılımları
Türbin Motor Eğitim Seti - Konfigürasyon 2
The Model AE-11-2 Turbine Engine Training System is a functional, scaled down turbine engine ideally suited for training applications. The engine is a small compact free turbine engine. The built-in safety features of this engine test stand make it suitable for educational use. The turbine engine comprises of a gas generator that incorporates a centrifugal compressor, an axial flow turbine rotating unit and an ignition and combustion system. The AE-11 is a self contained unit mounted on a sturdy steel frame, with caster wheels for easy mobility. The engine RPM and thrust are controlled by a mechanical throttle. The control panel contains


electrical circuit breaker and switches that are similar to the ones found in aircraft. The control panel also has engine instruments resembling aircraft installation, comprising of an EGT indicator, Oil Pressure indicator, Fuel Pressure gauge, Engine Thrust (in %), Tach indicator, Oil Temperature gauge, and Inlet Air Temperature gauge.


Engine Specifications:
Thrust: Up to 300 lbs
Fuel: Jet A-1 (can also be operated on K-1 Kerosene)
Combustion Chamber: Reverse Flow Annular
Ignition System: One, high voltage ignitor
Compressor Type: Single stage centrifugal
Turbine Type: Single stage axial flow
Engine RPM: 45,000 rpm


Instrumentation:
Sensors are installed to measure the indicated parameters to acquire and to store the engine run-up data into the computer through a data acquisition hardware module. The data is represented in instrument display form as well as in a graphical form. This facilitates the instructor to explain engine operating parameters and the interdependence of variables.

Training Materials:
The Training system is provided with user manual, and extensive educational materials. A computer based training package (CBT) may be ordered as an optional item.
Tüm Hakları Saklıdır © 2013 KONTEK Mühendislik Otomasyon Danışmanlık San. ve Tic. Ltd. Şti. | Tasarım: QDajans.com
Scroll