Academic Journal
Engine/Airframe/Drive Train Dynamic Interface Documentation
| العنوان: | Engine/Airframe/Drive Train Dynamic Interface Documentation |
|---|---|
| المؤلفون: | Needham, James F., Banerjee, Debashis |
| المساهمون: | SUMMA CORP CULVER CITY CA HUGHES HELICOPTERS DIV |
| المصدر: | DTIC AND NTIS |
| سنة النشر: | 1978 |
| المجموعة: | Defense Technical Information Center: DTIC Technical Reports database |
| مصطلحات موضوعية: | Helicopters, Jet and Gas Turbine Engines, HELICOPTER ROTORS, HELICOPTERS, HELICOPTER ENGINES, TRANSMISSIONS(MECHANICAL), STABILITY, VIBRATION, DRIVES, TORSION, DYNAMIC LOADS, AIRFRAMES, TURBOSHAFT ENGINES, INTERFACES, T-63 ENGINES, T-63-A-5A ENGINES, H-6 AIRCRAFT, OH-6A AIRCRAFT, H- 64 AIRCRAFT, YAH-64 AIRCRAFT, T-700 ENGINES, T-700-GE-700 ENGINES, PE62209A, WU201 |
| الوصف: | This report pertains to engine/airframe/drive train dynamic interface problems experienced by helicopters and the methodology used to avoid dynamic interface problems. The problem of low torsional frequency of the engine/ airframe/drive train dynamic system that results from the design philosophy of using a stationary main rotor mast enclosing a separate 'floating' torque drive shaft is addressed. The use of supercritical shafts and vibration isolators are described and mobility methods to preclude engine/airframe vibration problems are discussed. |
| نوع الوثيقة: | text |
| وصف الملف: | text/html |
| اللغة: | English |
| Relation: | http://www.dtic.mil/docs/citations/ADA056956 |
| الاتاحة: | http://www.dtic.mil/docs/citations/ADA056956 http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADA056956 |
| Rights: | Approved for public release; distribution is unlimited. |
| رقم الانضمام: | edsbas.9EE30900 |
| قاعدة البيانات: | BASE |
| الوصف غير متاح. |