Academic literature on the topic 'Hollow fan blade'

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Journal articles on the topic "Hollow fan blade"

1

Guo, Xiao, Qing Zhen Yang, and Yong Qiang Shi. "Vibration Characteristics Analysis of Wide-Chord Hollow Fan Blade." Applied Mechanics and Materials 482 (December 2013): 174–78. http://dx.doi.org/10.4028/www.scientific.net/amm.482.174.

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Wide-Chord Hollow Fan Blade is One of the New Technologies Used in Aircraft Engines. in this Paper, the Modal Analysis Method is Used to Analyze the Influence of the Rib Number and the Rib Thickness to Wide-Chord Hollow Fan Blade Vibration Characteristics. the Result Shows that the Wide-Chord Hollow Fan Blades Greatly Improves the First-Order Vibration Frequency Compared with the Solid Blades, and the First-Order Vibration Frequency of the Wide-Chord Hollow Fan Blades is Reduced with the Increasing Rib Number which is Not Good for Vibration Elimination. the Wide-Chord Hollow Fan Blades’ Vibrat
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2

Nikhamkin, M., and B. Bolotov. "Experimental and Finite Element Analysis of Natural Modes and Frequencies of Hollow Fan Blades." Applied Mechanics and Materials 467 (December 2013): 306–11. http://dx.doi.org/10.4028/www.scientific.net/amm.467.306.

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Natural modes and frequencies of gas turbine engine hollow fan blades were experimentally investigated. The blades were produced with the method of super-plastic molding and pressure welding combination. Two independent experimental methods were used: three-component scanning laser vibrometry and impact modal analysis. Natural frequencies and vibration modes of a hollow fan blade and stress fields corresponding to the natural modes were got. The finite element modal analysis was carried out. The hollow fan blade was stated to have particular natural vibration modes. The investigation results c
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3

Kielb, R. E. "Mass Balancing of Hollow Fan Blades." Journal of Engineering for Gas Turbines and Power 108, no. 4 (1986): 577–82. http://dx.doi.org/10.1115/1.3239950.

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This paper uses a typical section model to investigate analytically the effect of mass balancing as applied to hollow, supersonic fan blades. A procedure to determine the best configuration of an internal balancing mass to provide flutter alleviation is developed. This procedure is applied to a typical supersonic shroudless fan blade which is unstable both in the solid configuration and when it is hollow with no balancing mass. The addition of an optimized balancing mass is shown to stabilize the blade at the design condition.
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4

Sutliff, D. L., D. L. Tweedt, E. B. Fite, and E. Envia. "Low-Speed Fan Noise Reduction with Trailing EDGE Blowing." International Journal of Aeroacoustics 1, no. 3 (2002): 275–305. http://dx.doi.org/10.1260/147547202320962592.

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An experimental proof-of-concept test was conducted to demonstrate rotor-stator interaction tone noise reduction through rotor trailing edge blowing. The velocity deficit from the viscous wake of the rotor blades was reduced by injecting air into the wake from a trailing edge slot. Composite hollow rotor blades with internal flow passages were designed based on Computational Fluid Dynamics codes modeling the internal flow. The hollow blade with interior guide vanes creates flow channels through which externally supplied air flows from the root of the blade to the trailing edge. The impact of t
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5

Salnikov, Anton. "3D optimization of the hollow fan blade internal structure." Journal of Physics: Conference Series 1891, no. 1 (2021): 012015. http://dx.doi.org/10.1088/1742-6596/1891/1/012015.

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6

Chuan, Zeng, Jiang Xiang-hua, Chai Xiang-hai, and Shi Tong-cheng. "TC4 Hollow Fan Blade Structural Optimization Based on Bird-strike Analysis." Procedia Engineering 99 (2015): 1385–94. http://dx.doi.org/10.1016/j.proeng.2014.12.674.

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7

Kruglov, Alexey, Ramil Lutfullin, Radik Mulyukov, Minnaul Mukhametrakhimov, Oleg Rudenko, and Rinat Safiullin. "Promises of Low-Temperature Superplasticity for the Enhanced Production of Hollow Titanium Components." Materials Science Forum 838-839 (January 2016): 610–14. http://dx.doi.org/10.4028/www.scientific.net/msf.838-839.610.

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Application of the conventional superplasticity (SP) allows producing the unique hollow structures. One remarkable example is the hollow titanium blade of the air engine fan produced by Rolls-Royce. However, high temperature titanium alloys processing (~ 927 °С) limits wide industrial application of the conventional SP. The solution of the mentioned issue can be found through the application of low-temperature SP. Ti-6Al-4V alloy with ultrafine grain structure at the temperature range of 600 ­ 800 °С has enough ductility resources for the superplastic forming (SPF) of the parts with the compli
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8

Cosme, Nicolas, David Chevrolet, Jérôme Bonini, Bernard Peseux, and Patrice Cartraud. "Prediction of transient engine loads and damage due to hollow fan blade-off." Revue Européenne des Éléments Finis 11, no. 5 (2002): 651–66. http://dx.doi.org/10.3166/reef.11.651-666.

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9

Chai, Xianghai, Xiaoyun Zhang, Zhiqiang Wang, and Yesheng Liu. "Modeling of the Diffusion Bond for SPF/DB Titanium Hollow Structures." International Journal of Aerospace Engineering 2015 (2015): 1–9. http://dx.doi.org/10.1155/2015/694564.

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Diffusion-bonded titanium hollow warren structures have been successfully applied in aircraft engine components, such as fan blade, and OGV, while the optimal design of the hollow warren structure to improve its impact resistance, especially under bird-strike event, has been a challenge. In this work, a series of impact tests and numerical simulations are carried out to investigate the effect of key geometric features on the overall impact strength of a panel-shaped titanium hollow warren structure. Based on experimental and numerical studies, a quantitative relationship between diffusion bond
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10

Pereira, Michaël, Florent Ravelet, Kamel Azzouz, et al. "Improved Aerodynamics of a Hollow-Blade Axial Flow Fan by Controlling the Leakage Flow Rate by Air Injection at the Rotating Shroud." Entropy 23, no. 7 (2021): 877. http://dx.doi.org/10.3390/e23070877.

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Axial flow fans are used in many fields in order to ensure the mass and heat transfer from air, chiefly in the heating, ventilation and air conditioning industry (HVAC). A more proper understanding of the airflow behavior through the systems is necessary to manage and optimize the fan operation. Computational fluid dynamics (CFD) represents a real tool providing the ability to access flow structures in areas that measuring equipment cannot reach. Reducing the leakage flow rate, inherent in operation, by synthetic-jet techniques improves performance. This paper presents the CFD results performe
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