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公开(公告)号:US10533603B2
公开(公告)日:2020-01-14
申请号:US15448415
申请日:2017-03-02
Applicant: Bell Helicopter Textron Inc.
Inventor: Nick Pravanh , Michael E. Rinehart , Bart Shafer , Clegg Smith , Bruce B. Bacon
Abstract: A door track assembly for cooperation with a door roller mechanism, including a housing having a longitudinal channel along a length of the housing, wherein the channel descends at an end of the housing to form a stowage recess for the door roller mechanism, and a first track and a second track that are disposed on the housing along a length of the channel and that descend into the stowage recess and along which the door roller mechanism traverses.
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公开(公告)号:US20180251227A1
公开(公告)日:2018-09-06
申请号:US15661129
申请日:2017-07-27
Applicant: Bell Helicopter Textron Inc.
Inventor: Brent C. Ross , Michael E. Rinehart , Jeffrey M. Williams , Clegg Smith , Nick Pravanh
CPC classification number: B64D29/06 , B64C7/02 , B64C29/0033 , B64D29/02
Abstract: An aircraft including a nacelle disposed at a fixed location relative a wing member; a proprotor housing coupled to the nacelle, the proprotor housing configured to selectively rotate between a horizontal orientation and a non-horizontal orientation; a door pivotably coupled to the proprotor housing; and a linkage to connect the door and the nacelle, the linkage configured to move with the door from a closed position when the proprotor housing is in a horizontal orientation to an open position when the proprotor housing is in a non-horizontal orientation. In some embodiments, there can be a hinge member for hingedly coupling the door to the proprotor and/or nacelle. In other embodiments, the door includes a flexure portion. In some embodiments, the nacelle includes a plurality of doors. In other embodiments, proprotor includes a forward portion and a stationary aft portion; wherein the forward portion is configured to selectively pivot.
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公开(公告)号:US11046446B2
公开(公告)日:2021-06-29
申请号:US15661129
申请日:2017-07-27
Applicant: Bell Helicopter Textron Inc.
Inventor: Brent C. Ross , Michael E. Rinehart , Jeffrey M. Williams , Clegg Smith , Nick Pravanh
Abstract: An aircraft including a nacelle disposed at a fixed location relative a wing member; a proprotor housing coupled to the nacelle, the proprotor housing configured to selectively rotate between a horizontal orientation and a non-horizontal orientation; a door pivotably coupled to the proprotor housing; and a linkage to connect the door and the nacelle, the linkage configured to move with the door from a closed position when the proprotor housing is in a horizontal orientation to an open position when the proprotor housing is in a non-horizontal orientation. In some embodiments, there can be a hinge member for hingedly coupling the door to the proprotor and/or nacelle. In other embodiments, the door includes a flexure portion. In some embodiments, the nacelle includes a plurality of doors. In other embodiments, proprotor includes a forward portion and a stationary aft portion; wherein the forward portion is configured to selectively pivot.
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公开(公告)号:USD909949S1
公开(公告)日:2021-02-09
申请号:US29670350
申请日:2018-11-15
Applicant: Bell Helicopter Textron Inc.
Designer: Jeffrey M. Williams , James E. Kooiman , Clegg Smith , Lynn F. Eschete , Jason P. Winter , Michael E. Rinehart , Troy T. Bushmire
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公开(公告)号:US20190389571A1
公开(公告)日:2019-12-26
申请号:US16014441
申请日:2018-06-21
Applicant: Bell Helicopter Textron Inc.
Inventor: Colton Gilliland , Jeffrey Williams , Michael E. Rinehart , James Kooiman , Mark Przybyla , Clegg Smith , Eric Stephen Olson , George Ryan Decker , David Russell Bockmiller
Abstract: A tiltrotor aircraft includes a propulsion system with a fixed engine and a rotatable proprotor. The engine is located below the wing of the tiltrotor aircraft, and the rotatable proprotor assembly is mounted on the top surface of the wing. The engine and proprotor assembly are connected via a series of one or more gearboxes that route the engine output from the engine to the proprotor.
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公开(公告)号:USD909278S1
公开(公告)日:2021-02-02
申请号:US29670337
申请日:2018-11-15
Applicant: Bell Helicopter Textron Inc.
Designer: Jeffrey M. Williams , James E. Kooiman , Clegg Smith , Lynn F. Eschete , Jason P. Winter , Michael E. Rinehart , Troy T. Bushmire
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公开(公告)号:US20180252264A1
公开(公告)日:2018-09-06
申请号:US15448136
申请日:2017-03-02
Applicant: Bell Helicopter Textron Inc.
Inventor: Nick Pravanh , Michael E. Rinehart , Bart Shafer , Clegg Smith , Jeffrey M. Williams
CPC classification number: F16C29/008 , B64C1/14 , B64C7/02 , B64C29/0033 , B64C29/0091 , B64D29/02 , B64D29/06 , E05D15/0686 , E05Y2201/64 , E05Y2800/422 , E05Y2900/502 , F01D15/02 , F01D15/12 , F05D2220/90 , F05D2260/40311 , F05D2260/53 , F16C29/002 , F16C29/007 , F16C2204/20 , F16C2204/72 , F16C2208/82 , F16C2326/43
Abstract: A door roller mechanism for cooperation with a roller track including a carriage member having a door attachment feature; at least one roller disposed for rotation on a first side of the carriage member when the carriage member moves in the rolling direction; at least one roller disposed for rotation on an opposite second side of the carriage member when the carriage member moves in the rolling direction; a first rub member disposed on the first side of the carriage; a second rub member disposed on the second side of the carriage; and at least one biasing element disposed on the carriage member for resiliently biasing the first rub member and the second rub member in opposite lateral directions so as to contact a respective first track surface and a second track surface in a manner to dampen lateral vibration of a door connected to the roller mechanism.
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公开(公告)号:US20180252263A1
公开(公告)日:2018-09-06
申请号:US15448415
申请日:2017-03-02
Applicant: Bell Helicopter Textron Inc.
Inventor: Nick Pravanh , Michael E. Rinehart , Bart Shafer , Clegg Smith , Bruce B. Bacon
CPC classification number: F16C29/005 , B64C1/14 , B64C7/02 , B64C29/0033 , B64C29/0091 , B64D29/02 , B64D29/06 , E05D15/0665 , E05D15/0686 , E05D2015/1055 , E05Y2900/502 , F01D15/02 , F01D15/12 , F05D2220/90 , F05D2260/40311 , F05D2260/53 , F16C29/002 , F16C29/007 , F16C2204/20 , F16C2204/72 , F16C2208/82 , F16C2326/43
Abstract: A door track assembly for cooperation with a door roller mechanism, including a housing having a longitudinal channel along a length of the housing, wherein the channel descends at an end of the housing to form a stowage recess for the door roller mechanism, and a first track and a second track that are disposed on the housing along a length of the channel and that descend into the stowage recess and along which the door roller mechanism traverses.
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公开(公告)号:US10539180B2
公开(公告)日:2020-01-21
申请号:US15448136
申请日:2017-03-02
Applicant: Bell Helicopter Textron Inc.
Inventor: Nick Pravanh , Michael E. Rinehart , Bart Shafer , Clegg Smith , Jeffrey M. Williams
Abstract: A door roller mechanism for cooperation with a roller track including a carriage member having a door attachment feature; at least one roller disposed for rotation on a first side of the carriage member when the carriage member moves in the rolling direction; at least one roller disposed for rotation on an opposite second side of the carriage member when the carriage member moves in the rolling direction; a first rub member disposed on the first side of the carriage; a second rub member disposed on the second side of the carriage; and at least one biasing element disposed on the carriage member for resiliently biasing the first rub member and the second rub member in opposite lateral directions so as to contact a respective first track surface and a second track surface in a manner to dampen lateral vibration of a door connected to the roller mechanism.
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公开(公告)号:US20190389572A1
公开(公告)日:2019-12-26
申请号:US16015760
申请日:2018-06-22
Applicant: Bell Helicopter Textron Inc.
Inventor: Colton Gilliland , Jeffrey Williams , Michael E. Rinehart , James Kooiman , Mark Przybyla , Clegg Smith , Eric Stephen Olson , George Ryan Decker , David Russell Bockmiller
Abstract: A tiltrotor aircraft includes a propulsion system with a fixed engine and a rotatable proprotor. The engine is located on the top surface of the wing of the tiltrotor aircraft, and the rotatable proprotor assembly is also mounted on the top surface of the wing. The engine and proprotor assembly are connected via a series of one or more gearboxes that route the engine output from the engine to the proprotor.
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