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EVALUATION OF A LOW-NOISE FORMATE SPIRAL-BEVEL GEAR SET

机译:低噪音型螺旋锥齿轮组的评价

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Studies to evaluate low-noise Formate spiral-bevel gears were performed. Experimental tests were performed on the OH-58D helicopter main-rotor transmission in the NASA Glenn 500-hp Helicopter Transmission Test Stand. Low-noise Formate spiral-bevel gears were compared to the baseline OH-58D spiral-bevel gear design, a high-strength design, and previously tested low-noise designs (including an original low-noise design and an improved-bearing-contact low-noise design). Noise, vibration, and tooth strain tests were performed. The Formate design showed a decrease in noise and vibration compared to the baseline OH-58D design, and was similar to that of the previously tested improved-bearing contact low-noise design. The pinion tooth stresses for the Formate design significantly decreased in comparison to the baseline OH-58D design. Also similar to that of the improved-bearing-contact low-noise design, the maximum stresses of the Formate design shifted toward the heel, compared to the center of the face width for the baseline, high-strength, and previously tested low-noise designs.
机译:进行评估低噪音鳞状螺旋锥齿轮的研究。在NASA Glenn 500-HP直升机传动试验台上对OH-58D直升机主转子传输进行了实验测试。与基线OH-58D螺旋锥齿轮设计,高强度设计和先前测试的低噪声设计(包括原始低噪音设计和改进的轴承接触)进行比较低噪音型螺旋锥齿轮低噪音设计)。进行噪音,振动和牙齿应变试验。与基线OH-58D设计相比,甲板设计表现出噪声和振动的降低,并且类似于先前测试的轴承接触低噪声设计的噪音和振动。与基线OH-58D设计相比,甲板设计的小齿轮齿应力显着降低。还类似于改进的轴承接触低噪声设计,格式设计的最大应力朝向脚跟移动,与面部宽度的中心为基线,高强度和先前测试的低噪声相比设计。

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