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The paper explains how information stored in on-board recorders of flight parameters can be used for acceptance tests, also referred to as qualification tests. The disclosed example refers to the An-28 ‘Bryza’ aircraft where an old airscrew was substituted with the new generation Hartzell airscrew of the HC-B5 MP-3D type. The airscrew is an integral part of the driving system for the airscrew propelled aircraft that is provided with the TWD-10B engine. After revamping of the airscrew, the aircraft was named as TWD-10B/PZL-10S. The follow-up investigations were carried out with the aim to find out how much the airscrew substitution affected the alteration of key performance characteristics achieved by the driving unit of the aircraft. The investigations comprised both ground and in-flight tests and have led to determination of the essential characteristics for the engine operation as well as variations of the operational parameters in time. In some cases also so called phase portraits were found out for parameters of the engine operation so that to reflect dynamic properties of the engines. Such investigations are indispensable since the aircrafts are subject to operational limitations and technical conditions that must be mandatory fulfilled due to requirements of flight safety. The paper demonstrates that the data stored in on-board recorders of flight parameters can be really useful for execution of such acceptance (qualification) tests.
Wydawca
Czasopismo
Rocznik
Tom
Strony
201--206
Opis fizyczny
Bibliogr. 5 poz., rys.
Twórcy
autor
- Air Force Institute of Technology Księcia Bolesława Street 6, 01-494 Warsaw, Poland tel.: +48 22 6851101, fax: +48 22 8364471
Bibliografia
- [1] Kowalski, M., Szymczak, J., Raport z uzupełniających badań kwalifikacyjnych samolotu An-28 w wersji Bryza-1R z pięciołopatowymi śmigłami firmy Hartzell. (The Report on Supplementary Qualification Investigations Carried Out for the An-28 Aircraft of Bryza-1R Make Furnished with Five-Bladed Airscrews from Hartzell), Mielec 2000.
- [2] Kowalski, M., Zagadnienia diagnozowania turbinowych silników lotniczych z wykorzystaniem danych z pokładowych rejestratorów lotu, Zeszyt naukowy ITWL, Nr 31, Warszawa 2013. (Issues Related to Diagnostic of Turbojet Engines with Use of Data From On-Board Recorders of Flight Parameters, ITWL Scientific Journal, Vol. 31, Warsaw 2013).
- [3] Tymczasowa instrukcja użytkowania w locie samolotu Bryza-1R, sygn. PBD-1/8/2000, alb. 31, (Temporary Manual for In-Flight Use of Bryza-R1 Aircraft, sign. PBD-1/8/2000, Vol. 31), Mielec 2000.
- [4] Opis techniczny samolotu Bryza-1R, cz.1. Płatowiec i silnik, sygn. PBD-1/5/2000, alb. 6, (Technical Description of Bryza-R1 Aircraft, Part 1: Airframe and Engine, sign. PBD-1/5/2000, Vol. 6), Mielec 2000.
- [5] Instrukcja eksploatacji technicznej silnika turbośmigłowego TWD-10B nr 10.0.646/10B.00.030 i załącznik do tej instrukcji dotyczący Eksploatacji silnika TWD-10B (PZL-10S) ze śmigłem pięciołopatowym firmy Hartzell, nr dok. 10.0.684, 1999. (Technical Operation Manual of the TWD-10B Turbo-Propeller Engine No. 10.0.646/10B.00.030 with the Annex to that Manual Operation of the TWD-10B (PZL-10S) Engine Furnished with the Five-Bladed Airscrew from Hartzell, Doc. No. 10.0.684, 1999).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-d5b82515-8cff-4743-a708-f30d29034188