Academic literature on the topic 'Curve blade'

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Journal articles on the topic "Curve blade"

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Tao, Wang, Ding Huapeng, Wang Hao, and Tang Jie. "Virtual remanufacturing: Cross-section curve reconstruction for repairing a tip-defective blade." Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science 229, no. 17 (2015): 3141–52. http://dx.doi.org/10.1177/0954406214567135.

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Remanufacturing of damaged blades has been widely discussed in the field related with aero maintenance. Cross-section curve is the key factor for rebuilding 3D airfoil of a damaged blade. This paper focuses on how to reconstruct the cross-section curves of a tip-defective blade. The difficulty in the reconstruction of the cross-section curve is in broken region, where some data points are absent. In this paper, a method for reconstructing the cross-section curve in small-scale broken region of the blade tip is proposed. This method involves 3D noncontact digitization, methodology of obtaining
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Oyewola, Olanrewaju Miracle, Patrick Mark Singh, Ademola Samuel Akinwonmi, Olusegun Olufemi Ajide, and Tajudeen Abiola Ogunniyi Salau. "Thermal characterization of straight and curve edge blade liquid fuel swirl burner." EUREKA: Physics and Engineering, no. 3 (May 31, 2022): 11–19. http://dx.doi.org/10.21303/2461-4262.2022.002157.

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Accurate monitoring and controlling of the temperature in the combustion chamber can raise the burner efficiency, combustion intensity, fuel consumption and reduce pollutant emission. However, except combustion is accurately monitored and controlled, high concentration of pollutant gases and products like carbon monoxide (CO) and soot can form in the combustion chamber. This paper compares the combustion thermal profiles in a liquid fuel swirl burner using developed straight edge and curve edge blade swirlers at (20, 30, 40, 50 and 60)° for 6, 8, 10 and 12 number of blades in order to optimize
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Oyewola, Olanrewaju Miracle, Patrick Mark Singh, Ademola Samuel Akinwonmi, Olusegun Olufemi Ajide, and Tajudeen Abiola Ogunniyi Salau. "Thermal characterization of straight and curve edge blade liquid fuel swirl burner." EUREKA: Physics and Engineering, no. 3 (May 31, 2022): 11–19. https://doi.org/10.21303/2461-4262.2022.002157.

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Accurate monitoring and controlling of the temperature in the combustion chamber can raise the burner efficiency, combustion intensity, fuel consumption and reduce pollutant emission. However, except combustion is accurately monitored and controlled, high concentration of pollutant gases and products like carbon monoxide (CO) and soot can form in the combustion chamber. This paper compares the combustion thermal profiles in a liquid fuel swirl burner using developed straight edge and curve edge blade swirlers at (20, 30, 40, 50 and 60)° for 6, 8, 10 and 12 number of blades in order to optimize
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Irfan Ullah and Aamer Sharif. "Novel Blade Design and Performance Evaluation of a Single-Stage Savanious Horizontal Water Turbine." Journal of Technology Innovations and Energy 1, no. 4 (2022): 32–40. http://dx.doi.org/10.56556/jtie.v1i4.394.

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A type of micro-hydropower turbine known Savanious horizontal water turbine operates in freely flowing water of streams, canal, rivers etc. In a current study, blade shape and flow rates were used as the basis for an experimental assessment of a single- stage savanious horizontal water turbine. Numerical, experimental and statistical methods have used to examine the impact of blade shape and flow rates on performance metrics like rotational speed, torque and efficiency. The finding indicates that round curved blades performed better than semicircular and straight curved in terms of overall per
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Yang, Ke, Zhaoyang Yu, Weiwen Luo, et al. "Experiment and Study of Garlic Root Cutting Based on Continuous Force Feedback." Agronomy 13, no. 3 (2023): 835. http://dx.doi.org/10.3390/agronomy13030835.

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In this study, we quantified and analyzed the root-cutting process of garlic with a test bench with pressure sensors on the basis of the comparative analysis of various information perception methods. On the basis of the output value of the pressure sensor, the force curve of garlic roots was plotted, and the double round blade cutting module is optimized on the basis of the force curve diagram. The innovative proposal of slotted round blades for garlic root cutting is presented here. The round blade diameter is 110 mm, the center distance is 100 mm, the blade thickness is 1 mm, and the blade
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Nejad, J., A. Riasi, and A. Nourbakhsh. "Efficiency improvement of regenerative pump using blade profile modification: Experimental study." Proceedings of the Institution of Mechanical Engineers, Part E: Journal of Process Mechanical Engineering 233, no. 3 (2018): 448–55. http://dx.doi.org/10.1177/0954408918763554.

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Regenerative flow pump is a kind of turbomachine with the ability to generate high heads at relatively low flow rates. Despite having low hydraulic efficiency, regenerative pumps have found many applications in industries due to their simplicity, compact size, low manufacturing costs, and low specific speed. In this paper, an experimental study has been carried out to investigate the influence of impeller blade change on the performance of regenerative pump. To this end, the straight radial blades were changed to curved blades with the same inlet/outlet angles. Three forward curved blade impel
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Gao, Shimin, Yanrong Wang, Zhiwei Sun, and Siyuan Chen. "A Prediction Method with Altering Equivalent Stiffness for Damping Evaluation of Shrouded Bladed Disk Dynamic Systems." Symmetry 13, no. 3 (2021): 413. http://dx.doi.org/10.3390/sym13030413.

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In turbomachinery bladed disks are typical cyclic symmetric structures where high-cycle fatigue of the blades can easily occur. Increasing the shroud structure is an effective blade vibration reduction method using the dry friction of the shroud contact surface to dissipate vibration energy. During one vibration cycle of the blade, the contact surface of the shroud may have one or several states of stick, slip, and separation due to the different amplitude of blade, which affects not only the damping, but also the stiffness of the system. This paper proposes a method to analyze the damping cha
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Wang, Tao, Yi Liu Liu, Jie Tang, Hao Wang, and Li Wen Wang. "Study on the Curve Reconstructing in the Process of Blade Repairing." Advanced Materials Research 819 (September 2013): 86–90. http://dx.doi.org/10.4028/www.scientific.net/amr.819.86.

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the aero-blades are often easy to be damaged because of the severe working conditions, and the invading of out objects. Repairing is preferred to replacing with a new one due to the very high expense. The mathematical model of cross section curve is very important to the process of repairing the blade and to the analysis for the working performance of repaired blade. The method of remodeling the curve of cross section is studied including scanning the broken blade, denoising the data points, analyzing the points of cross section and dividing them into four assembles, and fitting them with adap
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Singh, Shambhu, S. V. Jogdand, R. K. Naik, A. K. Dave, and V. M. Victor. "Interaction Effect of Operating Parameters of Blade on Vermicompost Quality under Drum Condition." Current Journal of Applied Science and Technology 42, no. 16 (2023): 45–53. http://dx.doi.org/10.9734/cjast/2023/v42i164129.

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The curve blade, operational parameters and vermicompost physical properties are the key parameters come to pronouncement for breaking, churning and mixing clods condition. C, L and J curve blades was tested in the churning machine under drum condition for large, medium and small textured clods at vermicompost physical properties namely moisture content (15.24-35.48 % db.), bulk density (646 -732kg m-3) and crushing force (30 N). The performance results were analyzed in terms of mean mass diameter of vermicompost with the effects of three operating parameters namely moisture content % db, blad
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Zhao, Zhengcai, Junming Hou, and Yucan Fu. "Measurement-Based Modal Analysis and Stability Prediction on Turn-Milling of Hollow Turbine Blade." Shock and Vibration 2020 (September 24, 2020): 1–9. http://dx.doi.org/10.1155/2020/8861373.

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Hollow blades with honeycomb structures are increasingly used in the turbine engines for reducing weight and saving costs. The hollow blade is a typical thin-walled structural part with low stiffness, the machining system of which is often unstable and likely to chatter. The most effective solution to avoid the machining chatter is to guide the hollow blade to be machined in a stable machining zone. This paper proposes a measurement-based approach for modal analysis and stability prediction of turn-milling hollow blade. The impact test was carried out to achieve the FRF curves on the hollow bl
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Dissertations / Theses on the topic "Curve blade"

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Мілтих, Вікторія Станіславівна, Виктория Станиславовна Милтых та Viktoriia Stanislavivna Miltykh. "Підвищення енергоефективності насосної станції з насосами типу д впливом геометричних параметрів їх робочих коліс на форму напірної характеристики". Thesis, Сумський державний університет, 2016. http://essuir.sumdu.edu.ua/handle/123456789/46028.

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Робота спрямована на подальший розвиток науково-методичного забезпечення розв’язання задачі підвищення енергетичної ефективності роботи насосної станції з насосами типу Д шляхом заміни їх робочих коліс на нові, спроектовані з наперед визначеною крутизною напірної характеристики. За результатами огляду науково-технічної інформації визначена та обґрунтована актуальність теми дисертаційної роботи, сформульовані її мета і задачі. Поставлену наукову задачу вирішено шляхом впливу на крутизну напірної характеристики насоса зміною ширини робочого колеса на виході. За результатами математичного моделю
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Angel, Geoffrey Dennis. "Optimisation and characterisation of a curved bimetallic blade and its performance within a thermal motor." Thesis, University of Hertfordshire, 2014. http://hdl.handle.net/2299/13908.

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In most flat bimetallic strip applications, the bending is employed in the transverse direction, that is, upon the application of uniform heating to the entire strip, the initially straight strip bends transversely up from the flat plane. This study is concerned with a pre-curved bimetallic strip that upon heating up from the ambient, straightens up along the chord line tending to become flatter. The initial ambient radius of curvature of the strip is smaller, and upon heating, the radius of curvature becomes larger. By mounting the curved bimetallic strip with a rotational degree of freedom a
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Canovas, Lotthagen Zandra. "Defining, analyzing and determining power losses - due to icing on wind turbine blades." Thesis, Mälardalens högskola, Akademin för ekonomi, samhälle och teknik, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-48251.

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The wind power industry is one of the fastest-growing renewable energy industries in the world. Since more energy can be extracted from wind when the density is higher, a lot of the investments made in the wind power industry are made in cold climates. But with cold climates come harsh weather conditions such as icing. The icing on wind power rotor blades causes the aerodynamic properties of the blade to shift and with further ice accretion, the wind power plant can come to a standstill causing a loss of power, until the ice is melted. How big these losses are, depend greatly on site-specific
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Read, Simon. "A theoretical and experimental study of the aerodynamics of the curved-bladed darrieus vertical axis wind turbine." Thesis, Kingston University, 1986. http://eprints.kingston.ac.uk/20507/.

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The aerodynamic performance of the low solidity curved-bladed Darrieus vertical axis wind turbine has been studied both theoretically and experimentally. Initial studies showed the need for an engineering prediction scheme sufficiently accurate to give blade forces as functions of rotational position which did not require excessive computational time. The scheme proposed here develops a suggestion first made by Lapin in 1975, to treat the turbine as two actuator discs, one upwind and the other down-wind. This suggestion, combined with a multiple streamtube approach, the momentum equations in t
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Dickel, Jacob Allen. "Design Optimization of a Non-Axisymmetric Endwall Contour for a High-Lift Low Pressure Turbine Blade." Wright State University / OhioLINK, 2018. http://rave.ohiolink.edu/etdc/view?acc_num=wright1534980581177159.

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Darvish, Manoochehr [Verfasser], Christian Oliver [Akademischer Betreuer] Paschereit, and Stefan [Akademischer Betreuer] Frank. "Numerical and experimental investigations of the noise and performance characteristics of a radial fan with forward-curved blades / Manoochehr Darvish. Gutachter: Christian Oliver Paschereit ; Stefan Frank. Betreuer: Christian Oliver Paschereit ; Stefan Frank." Berlin : Technische Universität Berlin, 2015. http://d-nb.info/1070276693/34.

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CHIH, CHIOU FENG, and 邱峰志. "Influences of the Blade Thickness and Blade Number on the Performance Curve of Computer Centrifugal Fan." Thesis, 2011. http://ndltd.ncl.edu.tw/handle/87810803248078201730.

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碩士<br>國立高雄應用科技大學<br>應用工程科學研究所<br>99<br>This research aims to investigate the performance of the computer centfriugal fan under changing fan blade's thickness and blade's number. The computer centfriugal fan performance promotion method has been extensively studied, but little research was done on the fan blade thickness and leaf blade quantity. Therefore, this article will carry out the research gap on this subject. The research model uses 73.5x70x11mm mode for the high efficiency characteristic, with the wind entering upward and downward for the centfriugal fan. By reducing its fan blade thic
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Fang, Mei-Chih, and 方美智. "Simulation and analysis for the effect of axial fan blade angle on performance curve." Thesis, 2011. http://ndltd.ncl.edu.tw/handle/13056195277959121480.

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碩士<br>國立高雄應用科技大學<br>機械與精密工程研究所<br>99<br>Three axial-fan blade angles, i.e. fixed stagger angle, free stagger angle and horizontal inclination angle, are studied in this thesis by Taguchi Method. Influences of different fan angles on the performance, flow, pressure, torque, efficiency, noise and other characteristics of a fan are examined. In simulation, three axial-fan blade angles had used the Taguchi Method. Totally, 18 sets of simulation data are obtained. The data are analyzed through Signal-to-Noise Ratio (SNR) method, by using MINITAB software. For all of the control factors, set the qua
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Liu, Szu-hsien, and 劉思賢. "Computational and Experimental Investigations of a Forward-curved Blades Centrifugal Fan." Thesis, 2010. http://ndltd.ncl.edu.tw/handle/mgj569.

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博士<br>國立臺灣科技大學<br>機械工程系<br>99<br>The progress in the video related technologies fueled the projector industry to a flourish. However, heat dissipations from the optical engine became a design challenge. The fan selection for lamp cooling must be designed according to the interaction between fan performance curve and system impedance. Unfortunately, the existent simulation methods cannot predict the fan curve close to the measured results during the design stage. To improve the obvious defects of conventional methods, a newly developed computational approach by using the commercial code (STAR-C
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Chen, Hao-Ying, and 陳浩瑩. "An Investigation of the Influences of the Blade Curves on the Hydrodynamic Performance and Structure of Centrifugal Pump." Thesis, 2006. http://ndltd.ncl.edu.tw/handle/77377385517127459993.

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碩士<br>國立成功大學<br>機械工程學系碩博士班<br>94<br>A centrifugal pump impeller design covers many fields, including fluid dynamics, structural mechanics, vibration and manufacturing etc. In order to obtain blade shapes that could lead to good hydrodynamic performance and machined practicably, an impeller design approach combining five-axis manufacturing process and numerical curve is proposed in this research. The blade shapes are generated from the tool paths constructed ruled surface by the concept of generative machining method, and the cubic spline and the rational B-spline are used to compose the blade
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Books on the topic "Curve blade"

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United States. National Aeronautics and Space Administration., ed. On curve veering and flutter of rotating blades. National Aeronautics and Space Administration, 1993.

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United States. National Aeronautics and Space Administration., ed. On curve veering and flutter of rotating blades. National Aeronautics and Space Administration, 1993.

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Afolabi, Dare. Effects of mistuning and matrix structure on the topology of frequency response curves. Lewis Research Center, 1989.

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Center, Lewis Research, ed. Effects of mistuning and matrix structure on the topology of frequency response curves. Lewis Research Center, 1989.

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Schwartz, Steven A. The Big Book of Nintendo Games. Compute Books, 1991.

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Camilleri, I. C. Blake Curse. Pneuma Springs Publishing, 2012.

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Wells, Carolyn. Curved Blades. Creative Media Partners, LLC, 2023.

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Wells, Carolyn. Curved Blades. Creative Media Partners, LLC, 2023.

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Wells, Carolyn. Curved Blades. Lulu Press, Inc., 2017.

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Wells, Carolyn. Curved Blades. Lulu Press, Inc., 2017.

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Book chapters on the topic "Curve blade"

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Wang, Qikun, and Kangmin Chen. "A Bowed Blade based on’ spline Curve’ and Investigations on Its Aerodynamic Performance." In Challenges of Power Engineering and Environment. Springer Berlin Heidelberg, 2007. http://dx.doi.org/10.1007/978-3-540-76694-0_77.

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Kim, Chul Su, Jung Kyu Kim, and Tae Seong Kim. "An Evaluation of Appropriate Probabilistic ­S-­N Curve for the Turbine Blade Steel in the Low Pressure Steam." In Key Engineering Materials. Trans Tech Publications Ltd., 2005. http://dx.doi.org/10.4028/0-87849-978-4.1751.

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Großmann, David, and Bert Jüttler. "Volumetric Geometry Reconstruction of Turbine Blades for Aircraft Engines." In Curves and Surfaces. Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-27413-8_18.

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Matthews, Susan. "Impurity of Diction: The ‘Harlots Curse’ and Dirty Words." In Blake and Conflict. Palgrave Macmillan UK, 2009. http://dx.doi.org/10.1057/9780230584280_5.

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Migliaccio, G., G. Ruta, S. Bennati, and R. Barsotti. "Curved and Twisted Beam Models for Aeroelastic Analysis of Wind Turbine Blades in Large Displacement." In Lecture Notes in Mechanical Engineering. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-41057-5_144.

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Yuan, Ke, and Weidong Zhu. "Modal Identification of a Turbine Blade with a Curved Surface Under Random Excitation by a 3D CSLDV System and the Extended Demodulation Method." In Computer Vision & Laser Vibrometry, Volume 6. Springer Nature Switzerland, 2023. http://dx.doi.org/10.1007/978-3-031-34910-2_16.

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Zhao, Xi. "A Genetic Algorithm-Based Method for Smooth Modeling of Blade Surfaces." In Advances in Transdisciplinary Engineering. IOS Press, 2023. http://dx.doi.org/10.3233/atde230134.

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To further optimize the quality of the blade surface model, a fairing modeling method of blade surface based on a genetic algorithm is proposed. According to the NURBS curve and surface modeling principle, the fairing criterion of minimum strain energy and curvature change rate is established. Then the spline interpolation value points are optimized by the genetic algorithm and compared with the B-spline curve. The value points are modeled by NX. The blade surface is smooth, the curve curvature changes evenly, the strain energy is small, and there are no singular points and redundant inflectio
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Wei, Rong, Wei Xu, and Tingfeng Ming. "Experimental and Computational Studies on Characteristics of Cavitation Flow in Centrifugal Pump." In Frontiers in Artificial Intelligence and Applications. IOS Press, 2024. http://dx.doi.org/10.3233/faia241224.

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The work presents the investigation of characteristics of the cavitation flow in a centrifugal pump using a combination of experimental and computational studies. In experimental studies, the head drop curve and pressure signals were dynamically measured. The numerical computations were implemented based on Zwart mass transfer cavitation model and a modified RNG k-ε turbulence model. The computational head drop curve showed good agreement with the experimental results. The computational results and experimental results revealed that the cavitation of a centrifugal pump could be divided into fo
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Prasad Maddula, Satya, Vasishta Bhargava Nukala, Swamy Naidu Neigapula Venkata, Chinmaya Prasad Padhy, and Rahul Samala. "Trailing Edge Bluntness Noise Characterization for Horizontal Axis Wind Turbines [HAWT] Blades." In Acoustic Emission - New Perspectives and Applications. IntechOpen, 2022. http://dx.doi.org/10.5772/intechopen.99880.

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Wind turbine noise is becoming a critical issue for many offshore and land-based wind projects. In this work, we analyzed trailing edge bluntness vortex shedding noise source for a land-based turbine of size 2 MW and blade span of 38 m using original Brooks Pope and Marcolini (BPM)and modified BPM noise model. A regression-based curve fitting approach has been implemented to predict the shape function in terms of thickness to chord ratio of aerofoils used for blade. For trailing edge height of 0.1% chord, computations for sound power level were done at wind speed of 8 m/s, 17 RPM. The results
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Boedeker Ben H., Bernhagen Mary, Miller David J., Nicholas IV Thomas A., Linnaus Andrew, and Murray W.B. "Improving Fiberoptic Intubation with a Novel Tongue Retraction Device." In Studies in Health Technology and Informatics. IOS Press, 2011. https://doi.org/10.3233/978-1-60750-706-2-68.

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This study examined the utility of a novel tongue retractor created with a wider working blade and a more ergonomic curve to provide jaw lift and tongue management with one hand during intubation. Anesthesia providers participated in simulated intubation of a difficult manikin using the novel tongue retractor with the Bonfils video fiberscope. Results show that the tongue retractor improved placement success and was well received by the study participants.
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Conference papers on the topic "Curve blade"

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Yang, Sungho, Sanghun Kim, Hyosung Kim, and Junsu Park. "Rejuvenation and Life Assessment of IN 738 Blades after Long-Term Service." In AM-EPRI 2024. ASM International, 2024. http://dx.doi.org/10.31399/asm.cp.am-epri-2024p1269.

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Abstract Gas turbine blades are operated in a high temperature and a high pressure. In order to cope with that harsh condition, the blades are made of Nickel based superalloys which show excellent performance in such environment. Manufacturers of the blades usually provide the standards for the blade inspection and replacement. According to their guide, the blades are replaced after 3 times of operations and 2 times of refurbishments. Howsoever, purchase the new blades is always costly and burdensome to the power plant owners hence, the assessment of the blade lifespan and the rejuvenation of
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Rusk, David, Robert Taylor, Bruce Pregger, and Luis Sanchez. "Very-High Cycle Fatigue Testing Under Spectrum Loading for Endurance Limit Structural Design." In Vertical Flight Society 72nd Annual Forum & Technology Display. The Vertical Flight Society, 2016. http://dx.doi.org/10.4050/f-0072-2016-11543.

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A program has recently concluded that generated fatigue test data for the influence of a rotorcraft main rotor blade root bending spectrum (Helix) on the crack nucleation mechanisms in 7075-T651 aluminum. High frequency tests were performed that generated spectrum fatigue failures out to nearly 10⁹ cycles. Fractographic examination showed a distinct change in crack nucleation from slip initiated to inclusion initiated cracking as the spectrum peak stress level was increased. Spectrum life predictions were made using three different baseline constant-amplitude S-N curves, one using a traditiona
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Liu, Yuan-Peng, Song Zhao, and Xiao-Yan Dong. "Constructing section profile curve of turbine blade." In 2010 International Conference on Wavelet Analysis and Pattern Recognition (ICWAPR). IEEE, 2010. http://dx.doi.org/10.1109/icwapr.2010.5576329.

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Kianifar, Ali, Morteza Anbarsooz, and Mohammad Javadi. "Blade Curve Influences on Performance of Savonius Rotors: Experimental and Numerical." In ASME 2010 3rd Joint US-European Fluids Engineering Summer Meeting collocated with 8th International Conference on Nanochannels, Microchannels, and Minichannels. ASMEDC, 2010. http://dx.doi.org/10.1115/fedsm-icnmm2010-30919.

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In this study, the effect of blade curve on the power coefficient of a Savonius rotor is investigated by means of numerical simulation and wind tunnel tests. The tests were conducted on six rotors with identical dimensions but different blade curves, and the influences of blade curve and Reynolds number were studied. Followed by a simulation of the flow field around rotors with identical semi-circular curves and different overlaps, torque was calculated using pressure distribution on the blade surface, and the effect of Reynolds number and blade curve were studied on torque as well. Results in
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"Bezier Curve Fitting of Blade Profile considering Curvature Variation." In 3rd International Conference on Scientific and Academic Research ICSAR 2023. All Sciences Academy, 2023. http://dx.doi.org/10.59287/as-proceedings.746.

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Kammerer, Albert, and Reza S. Abhari. "Experimental Study on Impeller Blade Vibration During Resonance: Part 2—Blade Damping." In ASME Turbo Expo 2008: Power for Land, Sea, and Air. ASMEDC, 2008. http://dx.doi.org/10.1115/gt2008-50467.

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Forming the second part of a two-part paper, the estimation of damping is presented here. Part 1 discusses the experimental approach and the results on blade resonant response measurements. In the study of forced response damping is a crucial parameter which is measured to quantify the ability of a vibrating system to dissipate vibratory energy in response to a given excitation source. The blading of turbomachinery components is particularly prone to forced response excitation which is one of the major causes of high cycle fatigue failure during operation. In turbocharging applications forced
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Jujukin, Nikolai. "GEOMETRY OF KERF WHEN CURVE SAWING WITH A CIRCULAR RIP-SAW." In Modern machines, equipment and IT solutions for industrial complex: theory and practice. FSBE Institution of Higher Education Voronezh State University of Forestry and Technologies named after G.F. Morozov, 2021. http://dx.doi.org/10.34220/mmeitsic2021_224-227.

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Rip-sawing following the curvature of a crooked log means advantages for yield. However, the possibility to saw in a narrow curve with a circular saw blade is limited because of the inherently flat geometry of circular saw blades. For a double arbour circular saw the situation is even more problematic because the two blades have a certain overlap and thus, the two arbours are not positioned in the same horizontal position. In this study, a theoretical geometrical study of the creation of a kerf with a single circular saw blade and with a double arbour circular saw with two saw blades was exami
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Kooijman, Adrie, and Johan Broek. "Improving minimum strain energy curve calculations for flexible blade cutting." In 2006 7th International Conference on Computer-Aided Industrial Design and Conceptual Design. IEEE, 2006. http://dx.doi.org/10.1109/caidcd.2006.329367.

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Lee, Joshua, Arun Prabhakar, and Kathy Johnson. "Numerical Investigations Into the Oil Capture Efficiency of a Curve-Bladed Scoop System." In ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2020. http://dx.doi.org/10.1115/gt2020-15257.

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Abstract In civil aero-engines, the shafts are supported by oil-lubricated bearings. These bearings require sufficient lubrication to provide cooling and ensure the reliability of the engine. In some engine configurations, it is not possible to supply oil to the bearings via the traditional direct jet injection method. An oil scoop delivery system is one of the solutions proposed to solve this problem by directing oil from a nozzle towards a rotating plurality of scoops that have internal conduits to direct the captured oil to an under-race location. The performance of an oil scoop can be quan
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Ling, Jing, Xin Du, Songtao Wang, and Zhongqi Wang. "Relationship Between Optimum Curved Blade Generate Line and Cascade Parameters in Subsonic Axial Compressor." In ASME Turbo Expo 2014: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/gt2014-25799.

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Curved blade has been widely used to reduce the endwall loss, but there is no criterion for curved blade design. Relationship of the optimum curved blade generate line (stack line) and the inlet Mach number, solidity, aspect ratio and camber angle in a linear compressor cascade were researched by optimization method in present paper. The stack line is vertically symmetrical, composed of two third-order Bezier curves and a straight line. The results show that total pressure loss coefficient decreases with the curved height increasing in the present calculate conditions at the same curved angle,
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Reports on the topic "Curve blade"

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ZUTECK, MICHAEL. Adaptive Blade Concept Assessment: Curved Platform Induced Twist Investigation. Office of Scientific and Technical Information (OSTI), 2002. http://dx.doi.org/10.2172/803289.

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