Measuring and testing – Volume or rate of flow – Using differential pressure
Reexamination Certificate
2005-06-07
2005-06-07
Patel, Harshad (Department: 2855)
Measuring and testing
Volume or rate of flow
Using differential pressure
C073S170020
Reexamination Certificate
active
06901814
ABSTRACT:
Since, as a rule, there are several such PSTs on an aircraft, this results in a marked reduction in weight and aerodynamic drag, and savings in the required electric power in conjunction with a simultaneous increase in the accuracy of measurement of the angle of attack. All this permits a substantial increase in the competitiveness of the proposed fuselage Pitot-static tube.
REFERENCES:
patent: 3329016 (1967-07-01), Leavens et al.
patent: 4240598 (1980-12-01), Vinas Espin et al.
patent: 4718273 (1988-01-01), McCormack
patent: 4920808 (1990-05-01), Sommer
patent: 5024396 (1991-06-01), Guevel et al.
patent: 5337602 (1994-08-01), Gibson
patent: 5601254 (1997-02-01), Ortiz et al.
patent: 5628565 (1997-05-01), Hagen et al.
Efremov Andrei Aleksandrovich
Golovkin Mikhail Alekseevich
Golovkin Vladimir Alekseevich
Guskov Valentin Ivanovich
Kohler Heinz-Gerhard
Harter Secrest & Emery LLP
Nord-Micro Elektronik Feinmechanik
Patel Harshad
Salai Esq. Stephen B.
Shaw Esq. Brian B.
LandOfFree
Fuselage pitot-static tube does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Fuselage pitot-static tube, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Fuselage pitot-static tube will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-3521113