Tilt rotor aircraft
Latest Bell Helicopter Textron Inc. Patents:
Description
FIG. 1 is a left side view of the tilt rotor aircraft;
FIG. 2 is a right side view thereof;
FIG. 3 is a front view thereof;
FIG. 4 is a rear view thereof;
FIG. 5 is a top view thereof; and,
FIG. 6 is a bottom view thereof.
Referenced Cited
U.S. Patent Documents
D226826 | May 1973 | Wernicke |
D323315 | January 21, 1992 | Haga |
D332079 | December 29, 1992 | Haga et al. |
3059876 | October 1962 | Platt |
3073547 | January 1963 | Fischer |
3107881 | October 1963 | Stuart, III |
3136499 | June 1964 | Kessler |
3166271 | January 1965 | Zuck |
3231221 | January 1966 | Platt |
5096140 | March 17, 1992 | Dornier, Jr. |
5236149 | August 17, 1993 | Mackay |
5352090 | October 4, 1994 | Churchill et al. |
5381985 | January 17, 1995 | Wechsler et al. |
Patent History
Patent number: D394422
Type: Grant
Filed: May 13, 1996
Date of Patent: May 19, 1998
Assignee: Bell Helicopter Textron Inc. (Fort Worth, TX)
Inventor: John Patrick Magee (Arlington, TX)
Primary Examiner: Kay H. Chin
Attorney: Melvin A. Hunn
Application Number: 0/54,353
Type: Grant
Filed: May 13, 1996
Date of Patent: May 19, 1998
Assignee: Bell Helicopter Textron Inc. (Fort Worth, TX)
Inventor: John Patrick Magee (Arlington, TX)
Primary Examiner: Kay H. Chin
Attorney: Melvin A. Hunn
Application Number: 0/54,353
Classifications
Current U.S. Class:
Plural Horizontal Rotors (D12/328);
Vertical Takeoff Type (D12/326);
Canard Configuration Or With Plural Distinct Wings (D12/331);
T-tail Empennage, I.e., Stabilizer Mounted At Top Of Rudder Or Vertical Fin (D12/337)
International Classification: 1207;
International Classification: 1207;