SYSTEMS AND METHODS FOR DELIVERING CLIMATE CONTROLLED PRODUCT

In some embodiments, apparatuses and methods are provided herein useful to delivering climate controlled product. In some embodiments, there is provided a system for delivering climate controlled product via at least one autonomous unmanned aircraft system (UAS) that self-evaluates power sufficiency...

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Bibliographische Detailangaben
1. Verfasser:	Winkle, David C
Format:	Patent
Sprache:	eng
Schlagworte:	ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR AEROPLANES AIRCRAFT AVIATION CALCULATING COMPUTING CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS,e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES,DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS CONVEYING COSMONAUTICS COUNTING DATA PROCESSING SYSTEMS OR METHODS, SPECIALLY ADAPTED FORADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORYOR FORECASTING PURPOSES HANDLING THIN OR FILAMENTARY MATERIAL HELICOPTERS PACKAGES PACKAGING ELEMENTS PACKING PERFORMING OPERATIONS PHYSICS STORING SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE,COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORY OR FORECASTINGPURPOSES, NOT OTHERWISE PROVIDED FOR TRANSPORTING
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Beschreibung
Zusammenfassung:	In some embodiments, apparatuses and methods are provided herein useful to delivering climate controlled product. In some embodiments, there is provided a system for delivering climate controlled product via at least one autonomous unmanned aircraft system (UAS) that self-evaluates power sufficiency based on temperature tolerance of at least one product including: an autonomous UAS and at least one climate controlled product chamber. The UAS comprising: a control circuit, at least one rotor; a power supply, and a package coupler. The product chamber comprising: a chamber, at least one product reader, and a temperature control mechanism. The control circuit configured to: receive product identifier data; determine at least one climate threshold value; determine a confidence value of sufficient power remaining; compare whether the confidence value is within a risk threshold probability that a first mission will be completed; and initiate supply of power to the at least one rotor.