公开(公告)号：US07182297B2

公开(公告)日：2007-02-27

申请号：US10758294

申请日：2004-01-15

Applicant: Clifford Jackson

Inventor： Clifford Jackson

IPC: B64C13/28

CPC classification number: B64C39/024 ,  B64C2201/028 ,  B64C2201/104 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/165

Abstract: Methods and apparatuses for supporting aircraft components, including actuators are disclosed. An apparatus in accordance with one embodiment of the invention includes an actuator housing having an actuator receptacle that securely yet releasably receives an actuator. The actuator receptacle can include conformal walls that conform at least in part to the shape of the actuator and can accordingly squeeze the actuator and properly align the actuator. At least one of the actuator walls can further include a projection that is releasably received in a corresponding recess of the actuator. One of both of these features can releasably secure the actuator relative to the aircraft, reducing and/or eliminating the likelihood that the actuator will be misaligned and/or mispositioned relative to the aircraft during installation and/or replacement.

Abstract translation: 公开了用于支持飞机部件（包括致动器）的方法和装置。 根据本发明的一个实施例的装置包括具有可靠地可释放地接收致动器的致动器插座的致动器壳体。 致动器容器可以包括至少部分地符合致动器的形状的适形壁，并且可以相应地挤压致动器并且正确对准致动器。 致动器壁中的至少一个还可以包括可释放地容纳在致动器的相应凹部中的突起。 这两个特征之一可以相对于飞行器可释放地固定致动器，减少和/或消除在安装和/或更换期间致动器相对于飞行器不对准和/或错位的可能性。

公开(公告)号：US06264140B1

公开(公告)日：2001-07-24

申请号：US09426042

申请日：1999-10-25

Applicant: Brian T. McGeer ,  Andreas H. von Flotow ,  Cory Roeseler ,  Clifford Jackson

Inventor： Brian T. McGeer ,  Andreas H. von Flotow ,  Cory Roeseler ,  Clifford Jackson

IPC: B64C2568

CPC classification number: B64C39/024 ,  B64C25/68 ,  B64C2201/104 ,  B64C2201/148 ,  B64C2201/182 ,  B64C2201/205 ,  B64F1/02

Abstract: A method and apparatus for retrieving an aircraft in a confined space involves hanging a cable, for example from a kite or mast, across the aircraft's flight path. The aircraft approaches the cable in steady forward flight, and may strike the cable at any point on the wing, fuselage, or other leading surface. The cable then slides along the airframe as the aircraft moves forward, until it is intercepted by a hook attached to the wing tip or other convenient location. The hook captures the cable, and prevents further sliding; the cable then pulls the aircraft to a stop. Compliance of the cable, optionally combined with compliance of the cable suspension, provides acceptably gradual deceleration. The aircraft is left suspended in mid-air, and is then winched or slid to the base of the cable or other convenient retrieval point. The cable suspension and other fixed objects can be kept well clear of the flight path, so that the aircraft can continue safely in the event that it misses the cable, and make another approach.

Abstract translation: 用于在密闭空间中检索飞行器的方法和装置涉及将诸如风筝或桅杆的电缆悬挂在飞机的飞行路径上。 飞机在稳定的前进飞行中接近电缆，并可能在机翼，机身或其他前导表面上的任何一点撞击电缆。 随着飞机向前移动，电缆随着机身滑动，直到被挂在翼尖或其他便利位置的钩子拦截。 钩子捕获电缆，并防止进一步滑动; 电缆然后拉飞机停下来。 电缆的符合性，可选地与电缆悬架的顺应性相结合，提供可接受的逐渐减速。 飞机悬挂在半空中，然后被绞盘或滑动到电缆的基座或其他方便的检索点。 电缆悬架和其他固定物体可以保持远离飞行路径，使飞机在错过电缆的情况下可以安全地继续，并进行另一种方法。

公开(公告)号：US20130045299A1

公开(公告)日：2013-02-21

申请号：US13584200

申请日：2012-08-13

Applicant: Paul Bright ,  Craig Baumer ,  William McKeown ,  Clifford Jackson

Inventor： Paul Bright ,  Craig Baumer ,  William McKeown ,  Clifford Jackson

IPC: A21D15/00 ,  A01N37/36 ,  A01P3/00 ,  A01N37/04

CPC classification number: A21D2/145 ,  A21D2/02 ,  A21D10/002 ,  A21D13/066 ,  A23L3/3508

Abstract: Disclosed herein are compositions containing natural acids and natural buffering agents useful for inhibiting mold growth and/or prolonging the shelf life of baked products, which do not require propionic acid, and may be in either a liquid or a dry form. Also disclosed are methods of using the disclosed compositions.

Abstract translation: 本文公开了含有天然酸和天然缓冲剂的组合物，其可用于抑制模具生长和/或延长不需要丙酸的烘焙产品的保质期，并且可以是液体或干燥形式。 还公开了使用所公开的组合物的方法。

公开(公告)号：US20100025528A1

公开(公告)日：2010-02-04

申请号：US11775600

申请日：2007-07-10

Applicant: Clifford Jackson

Inventor： Clifford Jackson

IPC: B64F1/02

CPC classification number: B64C39/024 ,  B64C2201/028 ,  B64C2201/086 ,  B64C2201/165 ,  B64C2201/182

Abstract: Systems and methods for capturing and controlling post-recovery motion of an unmanned aircraft are disclosed herein. An aircraft system in accordance with one embodiment of the invention, for example, can include a line capture assembly carried by an unmanned aircraft having a fuselage and a lifting surface. The line capture assembly can include a flexible support line having a first portion attached to an attachment point on the fuselage and a second portion extending from the attachment point spanwise along the lifting surface of the aircraft. The line capture assembly can also include an engagement device coupled to the second portion of the support line. The engagement device is releasably secured to the lifting surface.

Abstract translation: 本文公开了用于捕获和控制无人飞行器的恢复后运动的系统和方法。 例如，根据本发明的一个实施例的飞行器系统可以包括由具有机身和提升表面的无人飞行器承载的线捕获组件。 线捕获组件可以包括柔性支撑线，其具有附接到机身上的附接点的第一部分和从飞行器的提升表面沿着方向从附接点延伸的第二部分。 线捕获组件还可以包括联接到支撑线的第二部分的接合装置。 接合装置可释放地固定到提升表面。

公开(公告)号：US07121507B2

公开(公告)日：2006-10-17

申请号：US10758943

申请日：2004-01-16

Applicant: Brian D. Dennis ,  Clifford Jackson ,  Brian T. McGeer

Inventor： Brian D. Dennis ,  Clifford Jackson ,  Brian T. McGeer

IPC: B64F1/00

CPC classification number: B64C39/024 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/048 ,  B64C2201/084 ,  B64C2201/102 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/182 ,  B64C2201/201 ,  B64C2201/205 ,  B64F1/06

Abstract: Methods and apparatuses for capturing, recovering, disassembling, and storing unmanned aircraft and other flight devices or projectiles are described. In one embodiment, the boom can be extended to deploy a recovery line to capture the aircraft in flight, a process that can be aided by a line capture device having retainers in accordance with further aspects of the invention. The aircraft can then be returned to its launch platform, disassembled, and stored, again with little or no direct manual contact between the operator and the aircraft, for example, by capturing a first wing of the aircraft and securing a second wing before releasing the first.

Abstract translation: 描述了用于捕获，恢复，拆卸和存储无人驾驶飞机和其他飞行装置或射弹的方法和装置。 在一个实施例中，吊杆可以被延伸以部署回收线以在飞行中捕获飞行器，这是根据本发明的其它方面能够由具有保持器的线捕获装置辅助的过程。 然后，飞机然后可以返回到其发射平台，拆卸和存储，再次与操作者和飞机之间的很少或没有直接的手动接触，例如通过捕获飞行器的第一翼并且在释放之前固定第二翼 第一。

公开(公告)号：US20050230536A1

公开(公告)日：2005-10-20

申请号：US10758943

申请日：2004-01-16

Applicant: Brian Dennis ,  Clifford Jackson ,  Brian McGeer

Inventor： Brian Dennis ,  Clifford Jackson ,  Brian McGeer

IPC: B64C39/02 ,  B64F1/02 ,  B64F1/06

CPC classification number: B64C39/024 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/048 ,  B64C2201/084 ,  B64C2201/102 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/182 ,  B64C2201/201 ,  B64C2201/205 ,  B64F1/06

Abstract: Methods and apparatuses for capturing, recovering, disassembling, and storing unmanned aircraft and other flight devices or projectiles are described. In one embodiment, the boom can be extended to deploy a recovery line to capture the aircraft in flight, a process that can be aided by a line capture device having retainers in accordance with further aspects of the invention. The aircraft can then be returned to its launch platform, disassembled, and stored, again with little or no direct manual contact between the operator and the aircraft, for example, by capturing a first wing of the aircraft and securing a second wing before releasing the first.

Abstract translation: 描述了用于捕获，恢复，拆卸和存储无人驾驶飞机和其他飞行装置或射弹的方法和装置。 在一个实施例中，吊杆可以被延伸以部署回收线以在飞行中捕获飞行器，这是根据本发明的其它方面能够由具有保持器的线捕获装置辅助的过程。 然后，飞机然后可以返回到其发射平台，拆卸和存储，再次与操作者和飞机之间的很少或没有直接的手动接触，例如通过捕获飞行器的第一翼并且在释放之前固定第二翼 第一。

公开(公告)号：US4955162A

公开(公告)日：1990-09-11

申请号：US354630

申请日：1989-05-19

Applicant: Clifford Jackson

Inventor： Clifford Jackson

IPC: B24B9/16 ,  B24B23/00

CPC classification number: B24B23/00 ,  B24B9/16

Abstract: A gem faceting kit is disclosed which includes a portable carrying case that may be opened to a use position in which it constitutes a utility rack from which other items of the kit may be retrieved and conveniently used. The gem faceting kit includes a gem faceting machine that has a storage and a use position. Also included in the kit are various lap wheels, grinding compounds, a rinse dispenser, a catch basin, a lamp, a visor, and various other tools, chemicals, and compounds used in gem faceting. The entire kit is lightweight and portable.

Abstract translation: 公开了一种宝石刻面套件，其包括便携式手提箱，该便携式手提箱可以打开到使用位置，在该使用位置中，该便携式手提箱构成可用于取出并方便使用的该套件的其它物品的使用位置。 宝石刻面套件包括一个具有存储和使用位置的宝石刻面机。 套件中还包括各种轮圈，研磨组合物，冲洗分配器，集水盆，灯，遮阳板以及各种其他工具，化学品和用于宝石面板的化合物。 整个套件轻巧便携。

公开(公告)号：US08382027B2

公开(公告)日：2013-02-26

申请号：US13556931

申请日：2012-07-24

Applicant: Clifford Jackson

Inventor： Clifford Jackson

IPC: B64D45/00

CPC classification number: A63H27/02 ,  B64C39/024 ,  Y10T74/18568 ,  Y10T403/7033

Abstract: Adjustable servomechanism assemblies and associated systems and methods. An unmanned aircraft system in accordance with one embodiment of the disclosure includes a movable mechanism and a servomechanism assembly operably coupled to the movable mechanism. The system also includes an interface assembly operably coupled to an output shaft of the servo and the movable mechanism. The interface assembly includes an adapter portion carried by the output shaft and an output arm releasably engaged with the adapter portion. The adapter portion includes a first aperture having a non-round surface mated with a non-round surface of the output shaft, and a non-splined, engagement surface. The output arm includes a second aperture sized to receive at least a portion of the outer surface of the adapter portion. The second aperture includes a generally smooth inner surface in contact with and rotatable through 360 degrees relative to the engagement surface of the adapter portion.

Abstract translation: 可调节伺服机构组件及相关系统和方法。 根据本公开的一个实施例的无人飞行器系统包括可操作地联接到可移动机构的可移动机构和伺服机构组件。 该系统还包括可操作地联接到伺服机构的输出轴和可移动机构的接口组件。 接口组件包括由输出轴承载的适配器部分和可释放地与适配器部分接合的输出臂。 适配器部分包括具有与输出轴的非圆形表面配合的非圆形表面的第一孔和非花键接合表面。 输出臂包括尺寸适于接收适配器部分的外表面的至少一部分的第二孔。 第二孔包括与适配器部分的接合表面相接触并可360度旋转的大致平滑的内表面。

公开(公告)号：US08235327B2

公开(公告)日：2012-08-07

申请号：US12406908

申请日：2009-03-18

Applicant: Clifford Jackson

Inventor： Clifford Jackson

IPC: B64C13/20

CPC classification number: A63H27/02 ,  B64C39/024 ,  Y10T74/18568 ,  Y10T403/7033

Abstract: Adjustable servomechanism assemblies and associated systems and methods are disclosed herein. An unmanned aircraft system in accordance with one embodiment of the disclosure includes a movable mechanism and a servomechanism assembly operably coupled to the movable mechanism. The system also includes an interface assembly operably coupled to an output shaft of the servo and the movable mechanism. The interface assembly includes an adapter portion carried by the output shaft and an output arm releasably engaged with the adapter portion. The adapter portion includes a first aperture having a non-round surface mated with a non-round surface of the output shaft, and a generally smooth, non-splined, engagement surface. The output arm includes a second aperture sized to receive at least a portion of the outer surface of the adapter portion. The second aperture includes generally smooth inner surface in contact with and rotatable through 360 degrees relative to the engagement surface of the adapter portion.

Abstract translation: 本文公开了可调节伺服机构组件及相关系统和方法。 根据本公开的一个实施例的无人飞行器系统包括可操作地联接到可移动机构的可移动机构和伺服机构组件。 该系统还包括可操作地联接到伺服机构的输出轴和可移动机构的接口组件。 接口组件包括由输出轴承载的适配器部分和可释放地与适配器部分接合的输出臂。 适配器部分包括具有与输出轴的非圆形表面配合的非圆形表面的第一孔和大致光滑的非花键的接合表面。 输出臂包括尺寸适于接收适配器部分的外表面的至少一部分的第二孔。 第二孔包括与适配器部分的接合表面相接触并且可相对于适配器部分的接合表面360度旋转的大致平滑的内表面。

公开(公告)号：US07806366B2

公开(公告)日：2010-10-05

申请号：US11775600

申请日：2007-07-10

Applicant: Clifford Jackson

Inventor： Clifford Jackson

IPC: B64F1/02

CPC classification number: B64C39/024 ,  B64C2201/028 ,  B64C2201/086 ,  B64C2201/165 ,  B64C2201/182

Abstract: Systems and methods for capturing and controlling post-recovery motion of an unmanned aircraft are disclosed herein. An aircraft system in accordance with one embodiment of the invention, for example, can include a line capture assembly carried by an unmanned aircraft having a fuselage and a lifting surface. The line capture assembly can include a flexible support line having a first portion attached to an attachment point on the fuselage and a second portion extending from the attachment point spanwise along the lifting surface of the aircraft. The line capture assembly can also include an engagement device coupled to the second portion of the support line. The engagement device is releasably secured to the lifting surface.

Abstract translation: 本文公开了用于捕获和控制无人飞行器的恢复后运动的系统和方法。 例如，根据本发明的一个实施例的飞行器系统可以包括由具有机身和提升表面的无人飞行器承载的线捕获组件。 线捕获组件可以包括柔性支撑线，其具有附接到机身上的附接点的第一部分和从飞行器的提升表面沿着方向从附接点延伸的第二部分。 线捕获组件还可以包括联接到支撑线的第二部分的接合装置。 接合装置可释放地固定到提升表面。