2011
DOI: 10.1115/1.4004458
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High-Pressure Angle Gears: Comparison to Typical Gear Designs

Abstract: A preliminary study has been completed to determine the feasibility of using high-pressure angle gears in aeronautic and space applications. Tests were conducted in the NASA GRC Spur Gear Test Facility at speeds up to 10,000 rpm and 73 N m (648 in. lb) for 3.18, 2.12, and 1.59 module gears (8, 12, and 16 diametral pitch gears), all designed to operate in the same test facility. The 3.18 module (8-diametral pitch), 28 tooth, 20 deg pressure angle gears are the NASA GRC baseline test specimen. Also, 2.12 module … Show more

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Cited by 11 publications
(5 citation statements)
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“…The value of this angle influences the generated internal stresses [18]. Gears with a large pressure angle are used in the aerospace industry [19] and show high bending strength of the tooth at the base. Gears with a small pressure angle are characterized by a quiet operation and a high contact ratio [20].…”
Section: Figurementioning
confidence: 99%
“…The value of this angle influences the generated internal stresses [18]. Gears with a large pressure angle are used in the aerospace industry [19] and show high bending strength of the tooth at the base. Gears with a small pressure angle are characterized by a quiet operation and a high contact ratio [20].…”
Section: Figurementioning
confidence: 99%
“…If speed ratio is not specified, the lowest speed ratio is advisable to reduce the maximum fillet stress. Robert F. Handschuh et, al., [19] examined high-pressure angle gearing for possible use in space mechanism applications. Tests were conducted in the NASA GRC Spur Gear Test Facility for 3.18 module (8-diametral pitch), 28 tooth, 20-degree pressure angle gear, 2.12 module (12-diametral pitch), 42 tooth, 25-degree pressure and 1.59 module (16diametral pitch), 56 tooth, 35-degree pressure angle gears were tested.…”
Section: Literature Reviewmentioning
confidence: 99%
“…The first trend refers to the optimization around the involute curve focusing on the selection of its optimal parameters or the introduction of optimal profile modifications (i.e., tip and root reliefs). The main objectives of the optimization are the minimization of the weight and the volume of the gears [6][7][8], the increase of their efficiency and load capacity [9][10][11] and the improvement of their dynamic and NVH characteristics (mainly through optimal profile modifications) [12][13][14].…”
Section: Introductionmentioning
confidence: 99%