Aircraft selectively engageable electric taxi system
US-9290264-B2 · Mar 22, 2016 · US
US9650131B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9650131-B2 |
| Application number | US-201514817295-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 4, 2015 |
| Priority date | Aug 5, 2014 |
| Publication date | May 16, 2017 |
| Grant date | May 16, 2017 |
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.
A method for rotationally driving an aircraft wheel, the wheel being equipped with a rim comprising two half-rims assembled by bolts ( 5 ). According to the method, a drive member for generating a torque for driving the wheel is controlled. The transfer of the drive torque to the wheel is accomplished via the rim assembly bolts.
Opening claim text (preview).
The invention claimed is: 1. A method for rotationally driving an aircraft wheel, the wheel being equipped with a rim comprising two half-rims assembled by bolts ( 5 ), comprising: controlling a drive member for generating a torque for driving the wheel, and transferring the drive torque to the wheel via the rim assembly bolts by means of a drive member which comprises a motor ( 10 ) having an output member ( 15 ) forming part of a rotor of the motor ( 10 ) mounted coaxially to the wheel, the output member being connected to the rim assembly bolts ( 5 ) by an interfacing member ( 20 ; 120 ), wherein the interfacing member ( 20 ) comprises two coaxial rings ( 21 ) connected to one another by crossmembers ( 22 ), each ring comprising sleeves for receiving ends of the rim assembly bolts ( 5 ) and ends of tie rods secured to the output member ( 15 ). 2. A method for rotationally driving an aircraft wheel, the wheel being equipped with a rim comprising two half-rims assembled by bolts ( 5 ), comprising: controlling a drive member for generating a torque for driving the wheel, and transferring the drive torque to the wheel via the rim assembly bolts by means of a drive member which comprises a motor ( 10 ) having an output member ( 15 ) forming part of a rotor of the motor ( 10 ) mounted coaxially to the wheel, the output member being connected to the rim assembly bolts ( 5 ) by an interfacing member ( 20 ; 120 ), wherein the interfacing member ( 120 ) comprises a plurality of stirrups ( 121 ) comprising two arms ( 123 ) connected by a bridge ( 122 ) and terminated by lugs ( 124 ), the bridge of each stirrup being fixed to the one of the output member or rim, the lugs being fixed to the other of the output member or rim.
Energy efficient operational measures, e.g. ground operations or mission management · CPC title
the wheels being individually rotatable around the axles · CPC title
Powered wheels, e.g. for taxing · CPC title
one rim part comprising the wheel disc · CPC title
with disc body formed by two or more axially spaced discs {(comprising rail-engaging elements formed by two or more axially spaced discs B60B17/0013)} · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.