Ducted tail rotor for rotary wing aircraft providing torque reaction and yaw attitude control
A Standard patent application filed on 31 July 1992 credited to McCardle, Francis H ; Desjardins, Rene A

Details

Application number :

25517  

Application type :

Standard  

Application status :

LAPSED  

Under opposition :

No  

Proceeding type :

 

Invention title :

Ducted tail rotor for rotary wing aircraft providing torque reaction and yaw attitude control  

Inventor :

McCardle, Francis H ; Desjardins, Rene A  

Agent name :

 

Address for service :

 

Filing date :

31 July 1992  

Associated companies :

 

Applicant name :

Boeing Company, The  

Applicant address :

 

Old name :

 

Original Source :

Go  

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