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Buoyancy-assisted UAV having electric-field actuated generator for powering electrical load within vicinity of powerlines

a technology of electric field and assisted uav, which is applied in the direction of charging stations, instruments, transportation and packaging, etc., can solve the problems of complex electric field topography in the vicinity of powerlines, failure to recognize and appreciate electric field strengths and interactions, and limited range and usefulness of uavs, so as to improve the performance of powering electrical loads

Active Publication Date: 2019-12-12
NXP AERONAUTICS RES LLC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

Enables extended range and utility of UAVs by directly harnessing electric field differentials, allowing for flight along powerlines and efficient power generation for various electrical loads, improving performance and reducing reliance on traditional power sources.

Problems solved by technology

Chen acknowledges that in such known arrangements the range and usefulness of the UAV are limited by the amount of energy available from the battery.
Consequently, it is believed that a significant shortcoming of Chen is a failure to recognize and appreciate electric field strengths and interactions within the vicinity of powerlines.
Indeed, electric field topography in the vicinity of powerlines is complex and depends on a number of factors, including the number of conducting lines and their arrangement.
Electric field strengths within the vicinity of the powerlines of the exemplary towers are complex.

Method used

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  • Buoyancy-assisted UAV having electric-field actuated generator for powering electrical load within vicinity of powerlines
  • Buoyancy-assisted UAV having electric-field actuated generator for powering electrical load within vicinity of powerlines
  • Buoyancy-assisted UAV having electric-field actuated generator for powering electrical load within vicinity of powerlines

Examples

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Embodiment Construction

[0391]As a preliminary matter, it will readily be understood by one having ordinary skill in the relevant art (“Ordinary Artisan”) that the invention has broad utility and application. Furthermore, any embodiment discussed and identified as being “preferred” is considered to be part of a best mode contemplated for carrying out the invention. Other embodiments also may be discussed for additional illustrative purposes in providing a full and enabling disclosure of the invention. Furthermore, an embodiment of the invention may incorporate only one or a plurality of the aspects of the invention disclosed herein; only one or a plurality of the features disclosed herein; or combination thereof. As such, many embodiments are implicitly disclosed herein and fall within the scope of what is regarded as the invention.

[0392]Accordingly, while the invention is described herein in detail in relation to one or more embodiments, it is to be understood that this disclosure is illustrative and exem...

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PUM

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Abstract

A UAV in which electric power is generated for an electric load from differentials in electric field strengths within a vicinity of powerlines includes: a plurality of electrodes separated and electrically insulated from one another for enabling differentials in voltage resulting from differentials in electric field strength experienced thereat; and electrical components electrically connected therewith and configurable to establish one or more electric circuits whereby voltage differentials causes a current to flow through the established electric circuit for powering an electric load. Preferably, the UAV includes a control assembly having one or more voltage-detector components configured to detect relative voltages of the electrodes; and a processor enabled to configure—based on the detected voltages and based on voltage and electric current specifications for powering the electric load—one or more of the electrical components to establish an electric circuit for powering the electric load.

Description

CROSS-REFERENCE TO RELATED APPLICATION[0001]The present application is a continuation of, and claims priority under 35 U.S.C. § 120 to, U.S. patent application Ser. No. 16 / 162,681, incorporated herein by reference, which '681 application is a continuation-in-part of, and claims priority under § 120 to, U.S. patent application Ser. No. 16 / 136,226, incorporated herein by reference, which '226 application is a continuation-in-part of, and claims priority under § 120 to, U.S. patent application Ser. No. 16 / 134,909, incorporated herein by reference. Each of the present application, the '681 application, the '226 application, and the '909 application is a nonprovisional application of, and claims priority under 35 U.S.C. § 119(e) to, each of the following provisional U.S. patent applications: 62 / 682,841; 62 / 682,842; 62 / 682,843; 62 / 682,845; 62 / 682,846; and 62 / 682,931. Each of the foregoing provisional U.S. patent applications is incorporated herein by reference. Any patent application publ...

Claims

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Application Information

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Patent Type & Authority Applications(United States)
IPC IPC(8): B64C39/02H02J7/00B64C25/10
CPCB64C39/024B64C2201/042H02J7/0068B64C25/10B64C2201/066H02G1/02B60L2200/10B60L53/12B60L5/005H02J50/001H02J50/05H02J7/0044Y02T90/16Y02T10/70Y02T10/7072Y02T90/14Y02T90/12B64U50/34B64U30/20B64U50/37B64U50/19B64U10/10B64U50/30B64U60/50B64U10/25B64U30/297B64U10/14B64U2101/30B60M3/00B60L53/14B60L53/30B64C39/04B64C39/08H02J50/10H04W4/029G01C9/005B60L53/60B60L53/38H04L67/12H04W4/025B64U2201/202B64U2101/10
Inventor SYRACUSE, STEVEN J.TILLMAN, CHAD D.
Owner NXP AERONAUTICS RES LLC
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