| 摘要 |
The invention relates to a fuselage Pitot-static tube comprising three groups of orifices for determining the total pressure (2), static pressure (3) and angle of attack (6, 7), and an axisymmetric body (1) and strut (5) for mounting an anti-icing system having, arranged between them, airways (10) and electric heating elements (8). The orifices for determining the angle of attack are arranged on the strut, whose cross section is constructed in the form of a subsonic aerodynamic profile with a rounded-off nose or a tapered nose, and are arranged between the nose of the profile and the position of its maximum thickness. |
| 申请人 |
PROFESSOR N.E. ZHUKOVSKY CENTRAL AEROHYDRODYNAMIC INSTITUTE;AEROPRIBOR VOSKHOD OJSC;NORD-MICRO ELEKTRONIK FEINMECHANIK AG;VOZHDAEV, YEVGENY SEMENOVICH;KOEHLER, HEINZ-GERHARD;GOLOVKIN, MIKHAIL ALEKSEEVICH;GOLOVKIN, VLADIMIR ALEKSEEVICH;NIKOLSKY, ALEKSANDR ALEKSANDROVICH;EFREMOV, ANDREI ALEKSANDROVICH;GUSKOV, VALENTIN IVANOVICH |
发明人 |
VOZHDAEV, YEVGENY SEMENOVICH;KOEHLER, HEINZ-GERHARD;GOLOVKIN, MIKHAIL ALEKSEEVICH;GOLOVKIN, VLADIMIR ALEKSEEVICH;NIKOLSKY, ALEKSANDR ALEKSANDROVICH;EFREMOV, ANDREI ALEKSANDROVICH;GUSKOV, VALENTIN IVANOVICH |
