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公开(公告)号：US09463541B2
公开(公告)日：2016-10-11
申请号：US13791208
申请日：2013-03-08
Applicant: Bell Helicopter Textron Inc.
Inventor： Paul Sherrill , Ned Hanisko
Abstract: A clamp has a base and a first selectively compliant component carried by the base, the first selectively compliant component being selectively operable between a substantially compliant state and a substantially rigid state.
Abstract translation: 夹具具有底座和由基座承载的第一选择性顺应部件，第一选择性顺应部件可在基本顺从的状态和基本刚性状态之间选择性地操作。
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公开(公告)号：US10981647B2
公开(公告)日：2021-04-20
申请号：US15666654
申请日：2017-08-02
Applicant: Bell Helicopter Textron Inc.
Inventor： Robert Self , Nathan P. Green , John R. McCullough , Russell Cole , Paul Sherrill , Robert Wardlaw
Abstract: The present invention includes a rotor-blade span-balancing system, including a span-balance pocket in a surface of a rotor blade; a cover operably configured to cover the span-balance pocket, wherein the cover is operably configured to be substantially flush with the surface of the rotor blade surface when covering the span-balance pocket, and wherein the cover includes a cover boss for reacting centrifugal force of the cover into the rotor blade; and one or more span-balance weights attached to the cover to span-balance the rotor blade.
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公开(公告)号：US10723448B2
公开(公告)日：2020-07-28
申请号：US15350338
申请日：2016-11-14
Applicant: Bell Helicopter Textron, Inc.
Inventor： Jared Mark Paulson , Bryan Marshall , Paul Sherrill , Bryan Judd
Abstract: A weight system for a rotor blade includes a weight box open in an outboard direction, a weight guide rod connected to the weight box, the weight guide rod extending in a spanwise direction through an interior of the weight box, and a span balance weight disposed within the weight box, the span balance weight being captured between the weight guide rod and the weight box.
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公开(公告)号：US20190039726A1
公开(公告)日：2019-02-07
申请号：US15666654
申请日：2017-08-02
Applicant: Bell Helicopter Textron Inc.
Inventor： Robert Self , Nathan P. Green , John R. McCullough , Russell Cole , Paul Sherrill , Robert Wardlaw
Abstract: The present invention includes a rotor-blade span-balancing system, including a span-balance pocket in a surface of a rotor blade; a cover operably configured to cover the span-balance pocket, wherein the cover is operably configured to be substantially flush with the surface of the rotor blade surface when covering the span-balance pocket, and wherein the cover includes a cover boss for reacting centrifugal force of the cover into the rotor blade; and one or more span-balance weights attached to the cover to span-balance the rotor blade.
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公开(公告)号：US20140250675A1
公开(公告)日：2014-09-11
申请号：US13791208
申请日：2013-03-08
Applicant: BELL HELICOPTER TEXTRON INC.
Inventor： Paul Sherrill , Ned Hanisko
Abstract: A clamp has a base and a first selectively compliant component carried by the base, the first selectively compliant component being selectively operable between a substantially compliant state and a substantially rigid state.
Abstract translation: 夹具具有底座和由基座承载的第一选择性顺应部件，第一选择性顺应部件可在基本顺从的状态和基本刚性状态之间选择性地操作。
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Patent Agency Ranking
公开(公告)号：US10227132B2
公开(公告)日：2019-03-12
申请号：US14817442
申请日：2015-08-04
Applicant: Bell Helicopter Textron Inc.
Inventor： Drew Sutton , Paul K. Oldroyd , James Braswell, Jr. , Scott Wolthuis , Paul Sherrill
IPC: B64C27/473
Abstract: A rotorcraft rotor blade assembly includes an upper skin portion extending substantially a full span of the rotor blade assembly and a lower skin portion extending substantially the full span of the rotor blade assembly. Each of the upper skin portion and the lower skin portion is configured to carry at least substantially 30% of rotor blade assembly loads.
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公开(公告)号：US20180264755A1
公开(公告)日：2018-09-20
申请号：US15989839
申请日：2018-05-25
Applicant: Bell Helicopter Textron Inc.
Inventor： Ronald Measom , James R. Stamper, JR. , Robert Self , Paul Sherrill , Paul K. Oldroyd , Neil Edward Morrow , Russell Cole
IPC: B29C70/34 , B23P15/04 , B29C70/46 , B29C70/54 , B64C27/473 , B64F5/10 , B29K63/00 , B29K307/04 , B29L31/08 , B29K105/08
CPC classification number: B29C70/342 , B23P15/04 , B29C70/46 , B29C70/541 , B29K2063/00 , B29K2105/0881 , B29K2307/04 , B29L2031/082 , B64C27/473 , B64C2027/4736 , B64F5/10 , F01D5/282 , Y10T29/49337
Abstract: A method of constructing a cured composite assembly includes positioning a composite assembly within a bonding tool, wherein the composite assembly comprises an uncured composite spar and a skin and performing a curing cycle on the composite assembly to simultaneously cure the uncured composite spar and bond the skin to the cured composite spar.
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公开(公告)号：US20170217109A1
公开(公告)日：2017-08-03
申请号：US15492274
申请日：2017-04-20
Applicant: Bell Helicopter Textron Inc.
Inventor： Ronald J. Measom , James R. Stamper , Robert Self , Paul Sherrill , Paul K. Oldroyd , Neil Edward Morrow , Russell Cole
CPC classification number: B29C70/342 , B23P15/04 , B29C70/46 , B29C70/541 , B29K2063/00 , B29K2105/0881 , B29K2307/04 , B29L2031/082 , B64C27/473 , B64C2027/4736 , B64F5/10 , F01D5/282 , Y10T29/49337
Abstract: A method of constructing a cured composite assembly includes positioning a composite assembly within a bonding tool, wherein the composite assembly comprises an uncured composite spar and a skin and performing a curing cycle on the composite assembly to simultaneously cure the uncured composite spar and bond the skin to the cured composite spar.
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公开(公告)号：US12240189B2
公开(公告)日：2025-03-04
申请号：US15937009
申请日：2018-03-27
Applicant: Bell Helicopter Textron Inc.
Inventor： Michael Dean Dearman , Jared Mark Paulson , Paul K. Oldroyd , Paul Sherrill
Abstract: A method for forming composite components includes disposing composite laminate over a mandrel. The method further includes infusing the composite laminate with a resin. A gelation of the infused resin is caused by applying a first environmental condition to the composite laminate and mandrel. At least a portion of the mandrel is deformed by applying a second environmental condition to the composite laminate and mandrel. The method further includes forming a composite structure by curing the composite laminate infused with resin. The deformed mandrel is removed from the composite structure after forming the composite structure.
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10.发明授权公开(公告)号：US10569866B2
公开(公告)日：2020-02-25
申请号：US16024986
申请日：2018-07-02
Applicant: Bell Helicopter Textron Inc.
Inventor： Kyle Thomas Cravener , Paul Sherrill
Abstract: The aircraft includes a rotor. The rotor includes a plurality of rotor blades. The aircraft further includes a non-rotating aircraft component. A proximity sensor is disposed with at least one of the non-rotating aircraft component and the rotor blades. A flight control computer is electrically coupled to the proximity sensor.
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