VEG, Aleksandar . An Advanced Balancing Methodology for the Propeller of a Wind-Tunnel Model. Strojniški vestnik - Journal of Mechanical Engineering, [S.l.], v. 53, n.5, p. 319-328, november 2017. ISSN 0039-2480. Available at: <https://www.sv-jme.eu/article/an-advanced-balancing-methodology-for-the-propeller-of-a-wind-tunnel-model/>. Date accessed: 24 dec. 2024. doi:http://dx.doi.org/.
Veg, A. (2007). An Advanced Balancing Methodology for the Propeller of a Wind-Tunnel Model. Strojniški vestnik - Journal of Mechanical Engineering, 53(5), 319-328. doi:http://dx.doi.org/
@article{.,
author = {Aleksandar Veg},
title = {An Advanced Balancing Methodology for the Propeller of a Wind-Tunnel Model},
journal = {Strojniški vestnik - Journal of Mechanical Engineering},
volume = {53},
number = {5},
year = {2007},
keywords = {wind-tunnels; airplane propellers; balancing contro; quality control; dynamic behaviour; },
abstract = {The focus of this paper is a versatile balancing procedure, developed to compensate for the asymmetries of a propeller blade's settable angle, in the range -5 to +35 . The standard balancing procedure (ISO 1940-1) was found to be inconsistent with the required quality grade, so a new balancing technique was created. A case study of propeller unbalance revealed a set of important details that must be uniquely assessed for such a complex balancing task. For the existing ISO notes, most of these details are descriptive rather than comprehensive. The new balancing concept defines the following: acceptable tolerances (shape, run-out and roughness), balancing order and priorities, a lower margin of residual unbalance, balancing accessories and regimes, unbalance correction and the verification of the results.},
issn = {0039-2480}, pages = {319-328}, doi = {},
url = {https://www.sv-jme.eu/article/an-advanced-balancing-methodology-for-the-propeller-of-a-wind-tunnel-model/}
}
Veg, A. 2007 November 53. An Advanced Balancing Methodology for the Propeller of a Wind-Tunnel Model. Strojniški vestnik - Journal of Mechanical Engineering. [Online] 53:5
%A Veg, Aleksandar %D 2007 %T An Advanced Balancing Methodology for the Propeller of a Wind-Tunnel Model %B 2007 %9 wind-tunnels; airplane propellers; balancing contro; quality control; dynamic behaviour; %! An Advanced Balancing Methodology for the Propeller of a Wind-Tunnel Model %K wind-tunnels; airplane propellers; balancing contro; quality control; dynamic behaviour; %X The focus of this paper is a versatile balancing procedure, developed to compensate for the asymmetries of a propeller blade's settable angle, in the range -5 to +35 . The standard balancing procedure (ISO 1940-1) was found to be inconsistent with the required quality grade, so a new balancing technique was created. A case study of propeller unbalance revealed a set of important details that must be uniquely assessed for such a complex balancing task. For the existing ISO notes, most of these details are descriptive rather than comprehensive. The new balancing concept defines the following: acceptable tolerances (shape, run-out and roughness), balancing order and priorities, a lower margin of residual unbalance, balancing accessories and regimes, unbalance correction and the verification of the results. %U https://www.sv-jme.eu/article/an-advanced-balancing-methodology-for-the-propeller-of-a-wind-tunnel-model/ %0 Journal Article %R %& 319 %P 10 %J Strojniški vestnik - Journal of Mechanical Engineering %V 53 %N 5 %@ 0039-2480 %8 2017-11-03 %7 2017-11-03
Veg, Aleksandar. "An Advanced Balancing Methodology for the Propeller of a Wind-Tunnel Model." Strojniški vestnik - Journal of Mechanical Engineering [Online], 53.5 (2007): 319-328. Web. 24 Dec. 2024
TY - JOUR AU - Veg, Aleksandar PY - 2007 TI - An Advanced Balancing Methodology for the Propeller of a Wind-Tunnel Model JF - Strojniški vestnik - Journal of Mechanical Engineering DO - KW - wind-tunnels; airplane propellers; balancing contro; quality control; dynamic behaviour; N2 - The focus of this paper is a versatile balancing procedure, developed to compensate for the asymmetries of a propeller blade's settable angle, in the range -5 to +35 . The standard balancing procedure (ISO 1940-1) was found to be inconsistent with the required quality grade, so a new balancing technique was created. A case study of propeller unbalance revealed a set of important details that must be uniquely assessed for such a complex balancing task. For the existing ISO notes, most of these details are descriptive rather than comprehensive. The new balancing concept defines the following: acceptable tolerances (shape, run-out and roughness), balancing order and priorities, a lower margin of residual unbalance, balancing accessories and regimes, unbalance correction and the verification of the results. UR - https://www.sv-jme.eu/article/an-advanced-balancing-methodology-for-the-propeller-of-a-wind-tunnel-model/
@article{{}{.},
author = {Veg, A.},
title = {An Advanced Balancing Methodology for the Propeller of a Wind-Tunnel Model},
journal = {Strojniški vestnik - Journal of Mechanical Engineering},
volume = {53},
number = {5},
year = {2007},
doi = {},
url = {https://www.sv-jme.eu/article/an-advanced-balancing-methodology-for-the-propeller-of-a-wind-tunnel-model/}
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TY - JOUR AU - Veg, Aleksandar PY - 2017/11/03 TI - An Advanced Balancing Methodology for the Propeller of a Wind-Tunnel Model JF - Strojniški vestnik - Journal of Mechanical Engineering; Vol 53, No 5 (2007): Strojniški vestnik - Journal of Mechanical Engineering DO - KW - wind-tunnels, airplane propellers, balancing contro, quality control, dynamic behaviour, N2 - The focus of this paper is a versatile balancing procedure, developed to compensate for the asymmetries of a propeller blade's settable angle, in the range -5 to +35 . The standard balancing procedure (ISO 1940-1) was found to be inconsistent with the required quality grade, so a new balancing technique was created. A case study of propeller unbalance revealed a set of important details that must be uniquely assessed for such a complex balancing task. For the existing ISO notes, most of these details are descriptive rather than comprehensive. The new balancing concept defines the following: acceptable tolerances (shape, run-out and roughness), balancing order and priorities, a lower margin of residual unbalance, balancing accessories and regimes, unbalance correction and the verification of the results. UR - https://www.sv-jme.eu/article/an-advanced-balancing-methodology-for-the-propeller-of-a-wind-tunnel-model/
Veg, Aleksandar"An Advanced Balancing Methodology for the Propeller of a Wind-Tunnel Model" Strojniški vestnik - Journal of Mechanical Engineering [Online], Volume 53 Number 5 (03 November 2017)
Strojniški vestnik - Journal of Mechanical Engineering 53(2007)5, 319-328
© The Authors, CC-BY 4.0 Int. Change in copyright policy from 2022, Jan 1st.
The focus of this paper is a versatile balancing procedure, developed to compensate for the asymmetries of a propeller blade's settable angle, in the range -5 to +35 . The standard balancing procedure (ISO 1940-1) was found to be inconsistent with the required quality grade, so a new balancing technique was created. A case study of propeller unbalance revealed a set of important details that must be uniquely assessed for such a complex balancing task. For the existing ISO notes, most of these details are descriptive rather than comprehensive. The new balancing concept defines the following: acceptable tolerances (shape, run-out and roughness), balancing order and priorities, a lower margin of residual unbalance, balancing accessories and regimes, unbalance correction and the verification of the results.