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公开(公告)号：US20180134411A1
公开(公告)日：2018-05-17
申请号：US15349571
申请日：2016-11-11
Applicant: Bell Helicopter Textron Inc.
Inventor： Brian Lafon , Ricky Jenkins , Sean Morgan , William P. Sumner , William L. Neal
Abstract: A detachable cargo mirror assembly for use on a rotorcraft surface that includes a bracket configured to mount to a surface on the rotorcraft, the bracket comprising a base portion and a retainer portion having a first pair of opposing holes, an elongated arm having two opposing ends, a first end for coupling with the bracket and a second end coupled to a mirror apparatus, the first end having a passage: and a releasable connector configured to engage with the first pair of opposing holes and the passage in the elongated arm when the elongated arm is in a first position to display a desired image on the mirror apparatus. The detachable cargo mirror assembly can be removed or in a stowed position when not in use.
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公开(公告)号：US10858091B2
公开(公告)日：2020-12-08
申请号：US16047907
申请日：2018-07-27
Applicant: Bell Helicopter Textron Inc.
Inventor： John C. Larkin, III , Emery N. Ward , William P. Sumner , Ricky Jenkins , Brian Lafon
Abstract: In a first aspect, there is a helicopter skid landing gear assembly including a front cross tube configured to interconnect two skid tubes; and a rear cross tube configured to interconnect two skid tubes; wherein at least one of the cross tubes comprises a monolithic metallic tube having a cross-section with a round exterior shape and an elliptical hollow portion therein. In a second aspect, there is a method for retrofitting a helicopter with a landing gear assembly; the method including providing a front cross tube and a rear cross tube, at least one of the front cross tube and the rear cross tube comprises a monolithic metallic tube having a cross-section with a substantially round exterior shape and an elliptical hollow portion therein; and connecting the front cross tube and rear cross tube to a fuselage.
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公开(公告)号：US09475577B2
公开(公告)日：2016-10-25
申请号：US14205886
申请日：2014-03-12
Applicant: Bell Helicopter Textron Inc.
Inventor： Patricia Wills , Brian Lafon , Ricky Jenkins
Abstract: One example of a retention system for a rotorcraft pedal assembly includes an insertion member, an axial retention member, and a transverse retention member. The insertion member, which is inserted through a side of a pedal assembly, includes a spring compressible against the side of the pedal assembly in response to the insertion member being inserted through the side. The axial retention member receives and retains the insertion member on an opposing side of the pedal assembly. The transverse retention member is inserted through a passage formed in the axial retention member to secure the axial retention member against the side of the pedal assembly.
Abstract translation: 用于旋翼飞机踏板组件的保持系统的一个示例包括插入构件，轴向保持构件和横向保持构件。 通过踏板组件侧插入的插入构件包括响应于插入构件插入通过侧面而抵靠踏板组件侧面的弹簧可压缩。 轴向保持构件将插入构件接收并保持在踏板组件的相对侧上。 横向保持构件通过形成在轴向保持构件中的通道插入，以将轴向保持构件固定在踏板组件的侧面上。
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Patent Agency Ranking
公开(公告)号：US20150259065A1
公开(公告)日：2015-09-17
申请号：US14205886
申请日：2014-03-12
Applicant: Bell Helicopter Textron Inc.
Inventor： Patricia Wills , Brian Lafon , Ricky Jenkins
Abstract: One example of a retention system for a rotorcraft pedal assembly includes an insertion member, an axial retention member, and a transverse retention member. The insertion member, which is inserted through a side of a pedal assembly, includes a spring compressible against the side of the pedal assembly in response to the insertion member being inserted through the side. The axial retention member receives and retains the insertion member on an opposing side of the pedal assembly. The transverse retention member is inserted through a passage formed in the axial retention member to secure the axial retention member against the side of the pedal assembly.
Abstract translation: 用于旋翼飞机踏板组件的保持系统的一个示例包括插入构件，轴向保持构件和横向保持构件。 通过踏板组件侧插入的插入构件包括响应于插入构件插入通过侧面而抵靠踏板组件侧面的弹簧可压缩。 轴向保持构件将插入构件接收并保持在踏板组件的相对侧上。 横向保持构件通过形成在轴向保持构件中的通道插入，以将轴向保持构件固定在踏板组件的侧面上。
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公开(公告)号：US20190047687A1
公开(公告)日：2019-02-14
申请号：US16047907
申请日：2018-07-27
Applicant: Bell Helicopter Textron Inc.
Inventor： John C. Larkin, III , Emery N. Ward , William P. Sumner , Ricky Jenkins , Brian Lafon
IPC: B64C25/52
Abstract: In a first aspect, there is a helicopter skid landing gear assembly including a front cross tube configured to interconnect two skid tubes; and a rear cross tube configured to interconnect two skid tubes; wherein at least one of the cross tubes comprises a monolithic metallic tube having a cross-section with a round exterior shape and an elliptical hollow portion therein. In a second aspect, there is a method for retrofitting a helicopter with a landing gear assembly; the method including providing a front cross tube and a rear cross tube, at least one of the front cross tube and the rear cross tube comprises a monolithic metallic tube having a cross-section with a substantially round exterior shape and an elliptical hollow portion therein; and connecting the front cross tube and rear cross tube to a fuselage.
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公开(公告)号：US09989098B2
公开(公告)日：2018-06-05
申请号：US15440044
申请日：2017-02-23
Applicant: Bell Helicopter Textron Inc.
Inventor： Ricky Jenkins , Robert Matson , William Sumner , Brian Lafon
CPC classification number: F16D1/12 , B25J1/04 , B64C27/04 , B64C27/28 , B64C27/50 , F16C11/06 , F16C11/0619 , F16C2326/43
Abstract: In one aspect, there is provided a rotary blade movement system including a retaining member configured to receive a rotor blade, a graspable arm, and a coupling mechanism operable to removably couple the retaining member to the graspable arm. The rotor blade movement system is configured to enable a user to adjust the position of the rotor blade by moving the graspable arm. The coupling mechanism can be a ball and socket joint. In one aspect, there is a method of rotating a rotor blade using a rotary blade movement system.
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公开(公告)号：US10745147B2
公开(公告)日：2020-08-18
申请号：US15349571
申请日：2016-11-11
Applicant: Bell Helicopter Textron Inc.
Inventor： Brian Lafon , Ricky Jenkins , Sean Morgan , William P. Sumner , William L. Neal
Abstract: A detachable cargo mirror assembly for use on a rotorcraft surface that includes a bracket configured to mount to a surface on the rotorcraft, the bracket comprising a base portion and a retainer portion having a first pair of opposing holes, an elongated arm having two opposing ends, a first end for coupling with the bracket and a second end coupled to a mirror apparatus, the first end having a passage: and a releasable connector configured to engage with the first pair of opposing holes and the passage in the elongated arm when the elongated arm is in a first position to display a desired image on the mirror apparatus. The detachable cargo mirror assembly can be removed or in a stowed position when not in use.
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公开(公告)号：US20170241474A1
公开(公告)日：2017-08-24
申请号：US15440044
申请日：2017-02-23
Applicant: Bell Helicopter Textron Inc.
Inventor： Ricky Jenkins , Robert Matson , William Sumner , Brian Lafon
IPC: F16C11/06
CPC classification number: F16D1/12 , B25J1/04 , B64C27/04 , B64C27/28 , B64C27/50 , F16C11/06 , F16C11/0619 , F16C2326/43
Abstract: In one aspect, there is provided a rotary blade movement system including a retaining member configured to receive a rotor blade, a graspable arm, and a coupling mechanism operable to removably couple the retaining member to the graspable arm. The rotor blade movement system is configured to enable a user to adjust the position of the rotor blade by moving the graspable arm. The coupling mechanism can be a ball and socket joint. In one aspect, there is a method of rotating a rotor blade using a rotary blade movement system.
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