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. 08, 2010

Filed:

Sep. 28, 2004
Applicants:

Dudley E. Smith, Arlington, TX (US);

Walter C. Joiner, Arlington, TX (US);

Paul J. Madej, Grand Prairie, TX (US);

Charles L. Hollimon, North Richland Hills, TX (US);

Daniel B. Robertson, Southlake, TX (US);

Inventors:

Dudley E. Smith, Arlington, TX (US);

Walter C. Joiner, Arlington, TX (US);

Paul J. Madej, Grand Prairie, TX (US);

Charles L. Hollimon, North Richland Hills, TX (US);

Daniel B. Robertson, Southlake, TX (US);

Assignee:

Bell Helicopter Textron Inc., Fort Worth, TX (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/82 (2006.01);
U.S. Cl.
CPC ...
Abstract

A rotorcraft having an enhanced configuration in which a simple wing and a propulsive anti-torque system are combined is disclosed. The propulsive anti-torque system includes an anti-torque thruster system in which a variable pitch fan is installed internal to the tail boom of the rotorcraft and an anti-torque thruster nozzle is mounted at the extremity of the tail boom. The fan is driven directly from the main rotor drive. The configuration and location of the fan allows the primary exhaust from the engine to be mixed with the compressed air flow from the fan. The mixed air flow from the fan and the engine passes through the tail boom and out the thruster nozzle.


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