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:
Jun. 24, 2025

Filed:

Jun. 18, 2024
Applicant:

Vetco Gray Scandinavia As, Sandvika, NO;

Inventors:

Giacomo Landi, Oslo, NO;

Vittorio Michelassi, Florence, IT;

Matteo Dozzini, Florence, IT;

Francesco Cangioli, Florence, IT;

Massimiliano Borghetti, Florence, IT;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F04D 17/12 (2006.01); F04D 13/06 (2006.01); F04D 19/02 (2006.01); F04D 25/02 (2006.01); F04D 25/06 (2006.01); F04D 29/58 (2006.01); H02K 1/12 (2006.01); H02K 1/16 (2006.01); H02K 1/22 (2006.01); H02K 3/46 (2006.01); H02K 7/14 (2006.01); H02K 16/00 (2006.01); H02K 21/14 (2006.01); H02K 21/22 (2006.01);
U.S. Cl.
CPC ...
F04D 17/12 (2013.01); F04D 13/06 (2013.01); F04D 19/02 (2013.01); F04D 19/022 (2013.01); F04D 19/024 (2013.01); F04D 19/026 (2013.01); F04D 25/02 (2013.01); F04D 25/0606 (2013.01); F04D 29/588 (2013.01); H02K 1/12 (2013.01); H02K 1/16 (2013.01); H02K 1/22 (2013.01); H02K 3/46 (2013.01); H02K 7/14 (2013.01); H02K 16/00 (2013.01); H02K 21/14 (2013.01); H02K 21/22 (2013.01);
Abstract

A compressor or pump stage is provided. The compressor or pump stage at least comprising a central shaft and at least one rotor, wherein an axis of rotation of the at least one rotor is the central shaft, wherein at least two axial thrust bearings are arranged axially remote from each other and being associated with each of the at least one rotor and at least two radial bearings arranged between the at least two axial thrust bearings and the at least one rotor comprises a number, n, of rows of impellers arranged at an outer perimeter of the at least one rotor with an axial distance between neighbouring rows of impellers, where n={2, 3, 4 . . . }


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