The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Dec. 06, 2016

Filed:

Oct. 12, 2011
Applicant:

Niklas Bennstedt, Svärdsjö, SE;

Inventor:

Niklas Bennstedt, Svärdsjö, SE;

Assignee:

AUTOINVENT TRANSIP AB, Svardsjo, SE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F16H 57/021 (2012.01); F16H 1/20 (2006.01); F16H 1/22 (2006.01); F03D 15/00 (2016.01); F16H 57/02 (2012.01);
U.S. Cl.
CPC ...
F16H 1/20 (2013.01); F03D 15/00 (2016.05); F16H 57/021 (2013.01); F05B 2260/4031 (2013.01); F16H 2057/02078 (2013.01); Y02E 10/722 (2013.01); Y10T 74/19651 (2015.01);
Abstract

A method of stepping up the speed of a rotary motion from a first speed, supplied to an input shaft (), to a second speed delivered by an output shaft (), comprises transmitting said rotary motion from said input shaft (), via a drive gear () of said input shaft (), the drive gear () being helical and having a first helix angle (ψ), to a layshaft arrangement, so as to generate a first axial thrust (F) of the input shaft () in a first axial direction; transmitting said rotary motion from said layshaft arrangement, via a driven gear () of said output shaft (), said driven gear () being helical and having a second helix angle (ψ) that is larger than said first helix angle (ψ), to said output shaft (), so as to generate a second axial thrust (F) of the output shaft () in a second direction, said second direction being substantially opposite to said first direction; and applying said first axial thrust (F) and said second axial thrust (F) to the same location of an axially rigid support structure (), such that said first and second axial thrusts (F, F) counter-act and at least partly cancel out in said support structure ().


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