-
公开(公告)号:US11142433B2
公开(公告)日:2021-10-12
申请号:US17105380
申请日:2020-11-25
Applicant: Vita Inclinata Technologies, Inc.
Inventor: Derek Sikora , Logan Goodrich
Abstract: A bidirectional thrust assembly comprises a motor, a selective power transfer mechanism, and a plurality of fans; wherein a change in direction of rotation of the motor causes the selective power transfer mechanism to change a torque transfer among the plurality of fans, wherein the fans may be opposing, and wherein the fans may be unidirectional. The bidirectional thrust assembly may be used in or by a plurality of craft or with respect to other objects which may need to be maneuvered, included suspended load control systems, vertical takeoff and landing craft, watercraft.
-
公开(公告)号:US10479503B2
公开(公告)日:2019-11-19
申请号:US16247791
申请日:2019-01-15
Applicant: Vita Inclinata Technologies, Inc.
Inventor: Derek Sikora , Caleb B. Carr , Logan Goodrich
Abstract: Load stability systems and methods for stabilizing swinging motions of suspended loads. The load stability systems include a fully automated, self-powered device that employs thrust to counteract and control lateral and rotational motion of an external load. The device is a temporary installment on the load, cable, or boom, and is agnostic to the platform from which it is suspended.
-
公开(公告)号:US20220371736A1
公开(公告)日:2022-11-24
申请号:US17875873
申请日:2022-07-28
Applicant: Vita Inclinata Technologies, Inc.
Inventor: Derek Sikora , Logan Goodrich , Caleb B. Carr
Abstract: Disclosed are systems, apparatuses, and methods to enhance control of a drone-load system, including through drone thrusters or load thrusters.
-
公开(公告)号:US20220274696A1
公开(公告)日:2022-09-01
申请号:US17750015
申请日:2022-05-20
Applicant: Vita Inclinata Technologies, Inc.
Inventor: Derek Sikora , Logan Goodrich
Abstract: A bidirectional thrust assembly comprises a motor, a selective power transfer mechanism, and a plurality of fans; wherein a change in direction of rotation of the motor causes the selective power transfer mechanism to change a torque transfer among the plurality of fans, wherein the fans may be opposing, and wherein the fans may be unidirectional. The bidirectional thrust assembly may be used in or by a plurality of craft or with respect to other objects which may need to be maneuvered, included suspended load control systems, vertical takeoff and landing craft, watercraft.
-
公开(公告)号:US20220135378A1
公开(公告)日:2022-05-05
申请号:US17581709
申请日:2022-01-21
Applicant: VITA INCLINATA TECHNOLOGIES, INC.
Inventor: Derek Sikora , Logan Goodrich , Daniel Stehling , Jonathan Zeller Oster , Caleb B. Carr , Patrick Carr
Abstract: Disclosed are systems, apparatuses, and methods to deploy and stow a deployable equipment to and from a hoist, to control a load on a suspension without transfer of torque to the suspension cable, for the deployable equipment to obtain data and electrical services from a dock of a carrier, and for the deployable equipment to control the hoist, such as a reel of a hoist, to control a z-axis of a terminal end of the suspension cable. Control of the z-axis may be, for example, to control an elevation of a load, such as relative to carrier, ground, or an objective or target, to control a tension on or of suspension cable. Control of the z-axis may be, for example, to control a rate of ascent or descent of a terminal end of suspension cable.
-
公开(公告)号:US20210078837A1
公开(公告)日:2021-03-18
申请号:US17105380
申请日:2020-11-25
Applicant: Vita Inclinata Technologies, Inc.
Inventor: Derek Sikora , Logan Goodrich
Abstract: A bidirectional thrust assembly comprises a motor, a selective power transfer mechanism, and a plurality of fans; wherein a change in direction of rotation of the motor causes the selective power transfer mechanism to change a torque transfer among the plurality of fans, wherein the fans may be opposing, and wherein the fans may be unidirectional. The bidirectional thrust assembly may be used in or by a plurality of craft or with respect to other objects which may need to be maneuvered, included suspended load control systems, vertical takeoff and landing craft, watercraft.
-
公开(公告)号:US20200271270A1
公开(公告)日:2020-08-27
申请号:US16802368
申请日:2020-02-26
Applicant: Vita Inclinata Technologies, Inc.
Inventor: Derek Sikora , Caleb B. Carr , Logan Goodrich
Abstract: Disclosed are systems, apparatuses, and methods to deploy a suspended load control apparatus onto a suspension cable and optionally allowing the suspended load control system to rotate about the suspension cable without imparting a significant rotational force on the suspension cable from rotation of the suspended load control system.
-
公开(公告)号:US20230249820A1
公开(公告)日:2023-08-10
申请号:US18135070
申请日:2023-04-14
Applicant: Vita Inclinata Technologies, Inc.
Inventor: Derek Sikora , Logan Goodrich , Caleb B. Carr
CPC classification number: B64C39/024 , B64D1/08 , B64D9/00 , B64D1/22 , B64U10/13
Abstract: Disclosed are systems, apparatuses, and methods to enhance control of a drone-load system, including through drone thrusters or load thrusters.
-
公开(公告)号:US11339034B2
公开(公告)日:2022-05-24
申请号:US17431019
申请日:2020-11-25
Applicant: Vita Inclinata Technologies, Inc
Inventor: Derek Sikora , Logan Goodrich
Abstract: Systems, apparatuses, and methods for a load control system for use on or with respect to a main load bearing line, carrier hook, and or head block of a crane, wherein the load control system may maintain tension on the load via a winch control line and a winch, wherein the tension may allow improved control over the load by the load control system.
-
公开(公告)号:US10940061B2
公开(公告)日:2021-03-09
申请号:US16788275
申请日:2020-02-11
Applicant: Vita Inclinata Technologies, Inc.
Inventor: Derek Sikora , Caleb B. Carr , Adam L. K. Philipp
Abstract: Load control apparatuses, systems and methods to control a location, orientation, or rotation of a suspended load by imparting thrust vectors to the suspended load or to a structure that holds the load. The load control apparatuses, systems and method may be integrated into a structure that holds a load, such as a rescue litter. The load control apparatuses, systems, and methods may be modular. The modular load control apparatuses, systems, and methods may be secured to a load or to a structure that holds the load.
-
-
-
-
-
-
-
-
-