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. 17, 2019

Filed:

Aug. 27, 2018
Applicant:

Space Systems/loral, Llc, Palo Alto, CA (US);

Inventors:

Seyed Tabatabaei, Mountain View, CA (US);

Jim Sowers, Sunnyvale, CA (US);

Ghislain Turgeon, San Jose, CA (US);

Assignee:

Space Systems/Loral, LLC, Palo Alto, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H04B 7/185 (2006.01); H04B 1/04 (2006.01); H04B 1/18 (2006.01); H03F 1/02 (2006.01); H03F 3/24 (2006.01); H03F 3/195 (2006.01); H01Q 1/28 (2006.01);
U.S. Cl.
CPC ...
H04B 7/18515 (2013.01); H01Q 1/288 (2013.01); H03F 1/0288 (2013.01); H03F 3/195 (2013.01); H03F 3/245 (2013.01); H04B 1/04 (2013.01); H04B 1/0458 (2013.01); H04B 1/0483 (2013.01); H04B 1/18 (2013.01); H03F 2200/451 (2013.01); H04B 2001/045 (2013.01);
Abstract

A solid state power amplifier uses a Doherty power amplifier that can be implemented as a monolithic microwave integrated circuit. By adjusting the DC bias of the amplifying stages in each branch of the Doherty amplifier, the output power, linearity, and DC power can be adjusted to provide a specified output, where the specification for the output can include the maintaining of desired DC power and linearity. The Doherty power amplifier can be used in a satellite payload or other application utilizing solid state power amplifiers, while providing the proper amount of RF output power and DC power. A single amplifier can have its bias levels adjusted for different output levels, helping to minimize the number of designs that are required for a given satellite payload, reducing the variety of parts in a satellite payload.


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