Systems and methods for in-flight operational assessment
US-2020277080-A1 · Sep 3, 2020 · US
US2020009989A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2020009989-A1 |
| Application number | US-201916460456-A |
| Country | US |
| Kind code | A1 |
| Filing date | Jul 2, 2019 |
| Priority date | Jul 4, 2018 |
| Publication date | Jan 9, 2020 |
| Grant date | — |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
An aircraft includes a first battery, provisions for transport that are powered by a second battery, and a management system for transferring energy between the first battery and the second battery.
Opening claim text (preview).
What is claimed is: 1 . An aircraft comprising: a first battery, at least one means of transport for short distances having a second battery; and a management system for transferring energy between the first battery and the second battery. 2 . The aircraft as claimed in claim 1 , further comprising an electrical or electronic connection between the first battery and the second battery. 3 . The aircraft as claimed in claim 1 , wherein the management system is configured so as to distribute the energy between the first and second batteries on the way to a predefined destination depending on a distance to the destination. 4 . The aircraft as claimed in claim 1 , wherein the aircraft has a fully electric drive. 5 . The aircraft as claimed in claim 1 , wherein the aircraft comprises bent or bendable wings. 6 . The aircraft as claimed in claim 1 , wherein the aircraft comprises a fast-charging battery system. 7 . The aircraft as claimed in claim 1 , wherein the means of transport comprises horizontally fixed ducted fans for take-off and landing. 8 . The aircraft as claimed in claim 7 , wherein the aircraft has louvers and the horizontal ducted fans are configured to be selectively covered by way of the louvers. 9 . The aircraft as claimed in claim 1 , wherein the means of transport comprises vertically fixed ducted fans for generating a propulsion. 10 . The aircraft as claimed in claim 1 , wherein the aircraft is configured to be selectively controlled in a fully autonomous manner. 11 . The aircraft as claimed in claim 1 further comprising a propulsion means powered by the first battery.
using steam or spring force (jet aircraft B64D27/16) · CPC title
Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft · CPC title
Air crafts · CPC title
having different nominal voltages · CPC title
Accessories not provided for elsewhere · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.