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:
Aug. 22, 2023

Filed:

May. 22, 2020
Applicant:

Aerostar International, Llc, Columbia, MD (US);

Inventors:

Aaron Fan, Redwood City, CA (US);

David Solum, Sunnyvale, CA (US);

Carey Hijmans, Morgan Hill, CA (US);

Jonathan Nutzmann, Redwood City, CA (US);

Assignee:

Aerostar International, LLC, Sioux Falls, SD (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64B 1/40 (2006.01); F16D 55/22 (2006.01); F03D 13/20 (2016.01); F16D 43/18 (2006.01); B64D 31/06 (2006.01); F16D 65/16 (2006.01); F16D 55/02 (2006.01); F04D 27/00 (2006.01); B64D 45/00 (2006.01); F04D 19/00 (2006.01); F16D 121/22 (2012.01);
U.S. Cl.
CPC ...
B64D 31/06 (2013.01); B64B 1/40 (2013.01); B64D 45/00 (2013.01); F04D 27/00 (2013.01); F16D 55/02 (2013.01); F16D 65/16 (2013.01); B64D 2045/0085 (2013.01); F04D 19/002 (2013.01); F16D 2121/22 (2013.01);
Abstract

Aspects of the technology relate to a braking assembly for a lateral propulsion system of a high altitude platform (HAP) configured to operate in the stratosphere. Power is supplied to a propeller assembly as needed during lateral propulsion so that the HAP can move to a desired location or remain on station. When lateral propulsion is not needed, power is no longer supplied to the propeller assembly and it may slowly cease rotating. However, in certain situations, it may be necessary to cause the propeller assembly to stop rotating as soon as possible. This can include an unplanned descent. Rapid braking can avoid the propeller blades from entangling in the envelope, parachute or other parts of the HAP. A reusable brake is employed to prevent uncontrolled rotation of the propeller on descent, or otherwise to prevent the propeller from spinning freely when not being used to propel the HAP laterally.


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