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:
Apr. 11, 2023

Filed:

Sep. 16, 2020
Applicant:

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

Inventors:

John Cromie, Menlo Park, CA (US);

Carey Hijmans, Morgan Hill, CA (US);

Assignee:

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

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/02 (2006.01); F01D 5/14 (2006.01); F01D 5/28 (2006.01); F01D 5/30 (2006.01); B64B 1/58 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64B 1/58 (2013.01); B64D 27/02 (2013.01); F01D 5/02 (2013.01); F01D 5/147 (2013.01); F01D 5/282 (2013.01); F01D 5/30 (2013.01);
Abstract

Aspects of the technology relate to a propeller blade assembly that is used in lateral propulsion systems for lighter-than-air high altitude platforms designed to operate, e.g., in the stratosphere. During operation, the propeller of the assembly is pointed along a specified heading and rotates at a selected velocity (e.g., hundreds or thousands of revolutions per minute). Power is supplied to the propeller as needed during lateral propulsion to move the platform along a particular trajectory or to remain on station over a given geographic location. In certain circumstances, the propeller may become damaged. This can include one or more blades breaking or shattering, which can result in failure of the propeller and potentially the entire LTA platform. The technology provides blades that are sufficiently flexible to avoid breakage or shattering due to debris impact or envelope entanglement, or otherwise shed a load. This can avoid catastrophic failure during stratospheric operation.


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