公开(公告)号：US20140110525A1

公开(公告)日：2014-04-24

申请号：US13659547

申请日：2012-10-24

Applicant: Brian S. Modrzejewski ,  Gary D. Hall ,  John R. McCullough ,  Farid Saiyed ,  Glenn A. Shimek ,  Danny A. Spivey ,  Tim Stark ,  Brian S. Vollmer

Inventor： Brian S. Modrzejewski ,  Gary D. Hall ,  John R. McCullough ,  Farid Saiyed ,  Glenn A. Shimek ,  Danny A. Spivey ,  Tim Stark ,  Brian S. Vollmer

IPC: B64C27/59

CPC classification number: B64C27/605 ,  Y10T29/49826

Abstract: In accordance with one embodiment of the present disclosure, a trunnion includes a first portion and a second portion. The first portion is capable of coupling directly to a drive tube of an aircraft, wherein the drive tube is capable of rotating around a first axis. The second portion is capable of coupling to a swash plate of the aircraft, wherein the swash plate is capable of causing the pitch of at least one of a plurality of aircraft blades to change.

Abstract translation: 根据本公开的一个实施例，耳轴包括第一部分和第二部分。 第一部分能够直接耦合到飞行器的驱动管，其中驱动管能够围绕第一轴旋转。 第二部分能够联接到飞行器的斜盘，其中斜盘能够导致多个飞行器叶片中的至少一个的桨距改变。

公开(公告)号：US20130105636A1

公开(公告)日：2013-05-02

申请号：US13286836

申请日：2011-11-01

Applicant: Clifton B. Day ,  Danny Spivey ,  Brian S.M. Modrzejewski ,  Tim Stark ,  Farid Saiyed

Inventor： Clifton B. Day ,  Danny Spivey ,  Brian S.M. Modrzejewski ,  Tim Stark ,  Farid Saiyed

IPC: B64C27/28 ,  B64C39/00 ,  B64C27/52

CPC classification number: B64C27/605

Abstract: A rotating control system includes a member having at least one clevis defined by a pair of clevis arms disposed in a clevis plane, the at least one clevis having an axis of symmetry disposed in the clevis plane midway between the pair of clevis arms, a shaft member pivotally coupled between the pair of clevis arms, the shaft member having a shaft axis, the shaft axis disposed axially along the shaft member, and an anti-rotation device for limiting a rotation of the shaft member about the shaft axis, the anti-rotation device having a plurality of flanges configured to couple to the clevis arms of the member, the flanges extending from a surface of a base member, the anti-rotation device having at least one restraining member that protrudes toward the shaft member for limiting the axial rotation of the shaft member.

Abstract translation: 旋转控制系统包括具有至少一个U形夹的构件，该至少一个U形夹由设置在U形夹平面中的一对U形臂限定，所述至少一个U形夹具有设置在所述一对U形臂之间中间的U形夹平面中的对称轴线; 所述轴构件枢转地联接在所述一对U形臂之间，所述轴构件具有轴轴线，所述轴线沿着所述轴构件轴向设置，以及用于限制所述轴构件围绕所述轴线的旋转的防旋转装置， 旋转装置具有多个凸缘，其被配置为联接到构件的U形夹臂，所述凸缘从基部构件的表面延伸，所述防旋转装置具有至少一个限制构件，所述限制构件朝向所述轴构件突出以限制轴向 轴构件的旋转。

公开(公告)号：US09193454B2

公开(公告)日：2015-11-24

申请号：US13659547

申请日：2012-10-24

Applicant: Brian S. Modrzejewski ,  Gary D. Hall ,  John R. McCullough ,  Farid Saiyed ,  Glenn A. Shimek ,  Danny A. Spivey ,  Tim Stark ,  Brian S. Vollmer

Inventor： Brian S. Modrzejewski ,  Gary D. Hall ,  John R. McCullough ,  Farid Saiyed ,  Glenn A. Shimek ,  Danny A. Spivey ,  Tim Stark ,  Brian S. Vollmer

IPC: B64C9/00 ,  B64C27/605

CPC classification number: B64C27/605 ,  Y10T29/49826

Abstract: In accordance with one embodiment of the present disclosure, a trunnion includes a first portion and a second portion. The first portion is capable of coupling directly to a drive tube of an aircraft, wherein the drive tube is capable of rotating around a first axis. The second portion is capable of coupling to a swash plate of the aircraft, wherein the swash plate is capable of causing the pitch of at least one of a plurality of aircraft blades to change.

Abstract translation: 根据本公开的一个实施例，耳轴包括第一部分和第二部分。 第一部分能够直接耦合到飞行器的驱动管，其中驱动管能够围绕第一轴旋转。 第二部分能够联接到飞行器的斜盘，其中斜盘能够导致多个飞行器叶片中的至少一个的桨距改变。

公开(公告)号：US09272781B2

公开(公告)日：2016-03-01

申请号：US13286836

申请日：2011-11-01

Applicant: Clifton B. Day ,  Danny Spivey ,  Brian S. M. Modrzejewski ,  Tim Stark ,  Farid Saiyed

Inventor： Clifton B. Day ,  Danny Spivey ,  Brian S. M. Modrzejewski ,  Tim Stark ,  Farid Saiyed

IPC: B64C27/32 ,  B64C27/605

CPC classification number: B64C27/605

Abstract: A rotating control system includes a member having at least one clevis defined by a pair of clevis arms disposed in a clevis plane, the at least one clevis having an axis of symmetry disposed in the clevis plane midway between the pair of clevis arms, a shaft member pivotally coupled between the pair of clevis arms, the shaft member having a shaft axis, the shaft axis disposed axially along the shaft member, and an anti-rotation device for limiting a rotation of the shaft member about the shaft axis, the anti-rotation device having a plurality of flanges configured to couple to the clevis arms of the member, the flanges extending from a surface of a base member, the anti-rotation device having at least one restraining member that protrudes toward the shaft member for limiting the axial rotation of the shaft member.

Abstract translation: 旋转控制系统包括具有至少一个U形夹的构件，该至少一个U形夹由设置在U形夹平面中的一对U形臂限定，所述至少一个U形夹具有设置在所述一对U形臂之间中间的U形夹平面中的对称轴线; 所述轴构件枢转地联接在所述一对U形臂之间，所述轴构件具有轴轴线，所述轴线沿着所述轴构件轴向设置，以及用于限制所述轴构件围绕所述轴线的旋转的防旋转装置， 旋转装置具有多个凸缘，其被配置为联接到构件的U形夹臂，所述凸缘从基部构件的表面延伸，所述防旋转装置具有至少一个限制构件，所述限制构件朝向所述轴构件突出以限制轴向 轴构件的旋转。