Журнал Российского общества по неразрушающему контролю и технической диагностике
The journal of the Russian society for non-destructive testing and technical diagnostic
 
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Главная Archive
18 | 11 | 2024
2019, 10 October

DOI: 10.14489/td.2019.10.pp.058-063

 

Osadchy N. V., Zubov S. S., Shepel V. T.
VIBRATION STRENGTH MONITORING OF THE AVIATION GTE ACOUSTIC PANELS
(pp. 58-63)

Abstract. The vibration strength check of the acoustic panels installed inside the gas-air duct of the aviation engine was performed by computation of frequencies and natural modes of vibration, endurance strength and the amplification factor. The amplification factor characterizing the dynamic properties of vibration transmission was calculated in the laboratory conditions as a ratio of the vibration level on the examined panel installed on the vibration test rig similar to  attachment on the engine to the vibration level on the vibration rig table. The natural frequency search was performed with the help of the ping-test and vibration mapping of the acoustic panels. Identification of the resonance frequencies was performed by means of strain-gaging. The amplification factor and the vibration acceleration on the engine casing enable to assess vibration acceleration of the panel under the resonant conditions during the panel operation on the engine. The panel performance under resonance was assessed by comparison of the actual vibration acceleration of the panel with the limit value obtained based on 107 cycles. In the process of design-experimental work the proposed approach enabled bringing the acoustic panels of the fifth-generation aircraft engine to compliance with the airworthiness requirements.

Keywords: acoustic panel, amplification factor, resonance, ping-test, vibration mapping, vibration acceleration, endurance strength.

 

N. V. Osadchy, S. S. Zubov, V. T. Shepel (PJSC UEC-Saturn, Rybinsk, Russia) E-mail: Данный адрес e-mail защищен от спам-ботов, Вам необходимо включить Javascript для его просмотра. , Данный адрес e-mail защищен от спам-ботов, Вам необходимо включить Javascript для его просмотра. , Данный адрес e-mail защищен от спам-ботов, Вам необходимо включить Javascript для его просмотра.  

 

 

1. Grigor'ev V. A., Kuznetsov S. P., Shepel' V. T. (2017). The basics of fine-tuning aviation gas turbine engines. Moscow: Innovatsionnoe mashinostroenie. [in Russian language]
2. Osadchiy N. V., Sergeev A. A., Shepel' V. T. (2013). Providing certification requirements for the turbojet engine fan casing. Aviatsionno-kosmicheskaya tekhnika i tekhnologiya, 104(7), pp. 197 – 200. [in Russian language]
3. Carrera E. (2002). Theories and Finite Elements for Multi-layered, Anisotropic, Composite Plates and Shells. Archives of Computational Methods Engineering, Vol. 9, (2), pp. 87 – 140.
4. Osadchiy N. V., Malyshev V. A., Shepel' V. T. (2018). Review of analytical methods for calculating the static strength of multilayer structures with honeycomb core. Materials of reports of the international scientific and technical conference "Problems and Prospects for the Development of Engine Engineering", pp. 144 – 147. Samara. [in Russian language]
5. Osadchiy N. V., Okrugin A. A., Shepel' V. T. (2016). Device for static testing of open shells for strength. Patent No. Ru 166440 U1. [in Russian language]
6. Osadchiy N. V., Shepel' V. T. (2015). Evaluation of the mechanical properties of the honeycomb core using the finite element method. Vestnik RGATU im. P. A. Solov'eva, 32(1), pp. 129 – 135. [in Russian language]
7. Osadchiy N. V., Malyshev V. A., Shepel' V. T. (2017). Methods for choosing the density and type of finite elements in the problems of the static strength of multilayer structures. Deformatsiya i razrushenie materialov, (1), pp. 10 – 17. [in Russian language]
8. Youzera H., Meftah S. A., Challamel N., Tounsi A. (2012). Nonlinear damping and forced vibration analysis of laminated composite beams. Composites. Part B. Engineering, Vol. 43, pp. 1147 – 1154.
9. Iurlaro L., Ascione A., Gherlone M. et al. (2015). Free vibration analysis of sandwich beams using the refined zigzag theory: an experimental assessment. Mechanics, Vol. 50, (10), pp. 2525 – 2535.

 

 

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