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公开(公告)号:US11753998B2
公开(公告)日:2023-09-12
申请号:US16914664
申请日:2020-06-29
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Shawn Alstad , Tomasz Dobosz , Rocio Chavez Felix
CPC classification number: F02C7/32 , F01D25/162 , F16H1/222 , F16H55/20 , F05D2230/644 , F05D2240/50 , F05D2250/312 , F05D2250/313 , F05D2250/314 , F05D2260/4031 , F05D2260/532
Abstract: An accessory system for a gas turbine engine having a drive shaft with an axis of rotation is provided. Also provided is a bearing housing assembly for coupling the drive shaft of an accessory having a first gear to a gear associated with the accessory system. The bearing housing assembly includes a mount including an interface to be coupled to the accessory and defining a central bore, and a lock cylinder configured to receive the drive shaft. The lock cylinder is movable relative to the central bore and the drive shaft to adjust a contact pattern between the first gear of the drive shaft and the gear of the accessory system.
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公开(公告)号:US20210087975A1
公开(公告)日:2021-03-25
申请号:US16914664
申请日:2020-06-29
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Shawn Alstad , Tomasz Dobosz , Rocio Chavez Felix
Abstract: An accessory system for a gas turbine engine having a drive shaft with an axis of rotation is provided. Also provided is a bearing housing assembly for coupling the drive shaft of an accessory having a first gear to a gear associated with the accessory system. The bearing housing assembly includes a mount including an interface to be coupled to the accessory and defining a central bore, and a lock cylinder configured to receive the drive shaft. The lock cylinder is movable relative to the central bore and the drive shaft to adjust a contact pattern between the first gear of the drive shaft and the gear of the accessory system.
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公开(公告)号:US10731566B2
公开(公告)日:2020-08-04
申请号:US15786733
申请日:2017-10-18
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Shawn Alstad , Tomasz Dobosz , Rocio Chavez Felix
Abstract: An accessory system for a gas turbine engine having a driveshaft with an axis of rotation is provided. The system includes a towershaft coupled to the driveshaft and rotatable about a towershaft axis of rotation. The towershaft includes a towershaft bevel gear. The system includes a primary shaft including a first bevel gear and a second bevel gear that each revolve about a primary shaft axis of rotation. The first bevel gear is coupled to the towershaft bevel gear. The system includes a secondary shaft including a third bevel gear and a fourth bevel gear that each revolve about a secondary shaft axis of rotation. The third bevel gear is coupled to the second bevel gear. The system includes a tertiary shaft including a fifth bevel gear that revolves about a tertiary shaft axis of rotation. The fifth bevel gear is coupled to the fourth bevel gear.
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公开(公告)号:US20190112984A1
公开(公告)日:2019-04-18
申请号:US15786733
申请日:2017-10-18
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Shawn Alstad , Tomasz Dobosz , Rocio Chavez Felix
CPC classification number: F02C7/32 , F01D25/162 , F05D2230/644 , F05D2240/50 , F05D2250/312 , F05D2250/313 , F05D2250/314 , F05D2260/4031 , F05D2260/532 , F16H1/222 , F16H55/20
Abstract: An accessory system for a gas turbine engine having a driveshaft with an axis of rotation is provided. The system includes a towershaft coupled to the driveshaft and rotatable about a towershaft axis of rotation. The towershaft includes a towershaft bevel gear. The system includes a primary shaft including a first bevel gear and a second bevel gear that each revolve about a primary shaft axis of rotation. The first bevel gear is coupled to the towershaft bevel gear. The system includes a secondary shaft including a third bevel gear and a fourth bevel gear that each revolve about a secondary shaft axis of rotation. The third bevel gear is coupled to the second bevel gear. The system includes a tertiary shaft including a fifth bevel gear that revolves about a tertiary shaft axis of rotation. The fifth bevel gear is coupled to the fourth bevel gear.
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