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:
Jan. 18, 2011

Filed:

Mar. 02, 2007
Applicants:

Anatoly Gosis, Palatine, IL (US);

Scott Takayuki Koizumi, Fairfield, CA (US);

Folkert Fred Koch, San Ramon, CA (US);

Frank Otte, Mt. Prospect, IL (US);

Dennis Bednarz, Des Plaines, IL (US);

Inventors:

Anatoly Gosis, Palatine, IL (US);

Scott Takayuki Koizumi, Fairfield, CA (US);

Folkert Fred Koch, San Ramon, CA (US);

Frank Otte, Mt. Prospect, IL (US);

Dennis Bednarz, Des Plaines, IL (US);

Assignee:

Illinois Tool Works Inc., Glenview, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H01R 13/15 (2006.01);
U.S. Cl.
CPC ...
Abstract

A new and improved aircraft power connector, for electrical connection to an aircraft electrical connector, has incorporated thereon a dual-position mechanism which can effectively alter the engagement force level defined between the electrical connector contact pins of the aircraft power connector and the aircraft electrical connector. When the mechanism is disposed at a first position, the force level is relatively low so as to easily permit connection and disconnection, whereas when the mechanism is disposed at a second position, the force level is relatively high so as to ensure the connection of the aircraft power connector to the aircraft electrical connector and thereby prevent the inadvertent disconnection of the aircraft power connector from the aircraft electrical connector.


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