FIELD: aircraft industry. SUBSTANCE: construction is loaded in chord area and linear displacements of two points are determined. Force-transmitting lever S is fixed to the construction and torsional vibrations are excited due to application of pair of forces P(t) with sign changing periodically to ends of the lever. Amplitudes a and b of vibrational displacements of the ends are measured. The point is determined according to the relation of a and b and known value of length lp of force-transmitting lever which corresponds to coordinate of projection of center of rigidity Ni of tested cross-section onto the surface of the construction from the relation given in the description of the invention. EFFECT: improved reliability; improved precision. 1 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF DETERMINING OBJECT CENTER-OF-MASS COORDINATE | 0 |
|
SU1820256A1 |
DEVICE DETERMINING MASS OF OBJECT | 1993 |
|
RU2075732C1 |
DEVICE FOR IMPARTING VIBRATIONS TO OBJECT UNDER INVESTIGATION | 1991 |
|
RU2030927C1 |
METHOD OF ESTIMATION OF TECHNICAL STATE OF FLYING VEHICLE RIGID CONTROL LINKAGE | 1994 |
|
RU2092387C1 |
STAND FOR VIBRATION TESTS OF DESIGN STRUCTURES | 1990 |
|
RU2017107C1 |
METHOD FOR DETERMINING POSITION OF OBJECT CENTER OF MASS | 0 |
|
SU1795317A1 |
DEVICE FOR DETERMINATION OF MATERIAL STRENGTH CHARACTERISTICS | 1991 |
|
RU2017114C1 |
VIBRATION PUMP | 1993 |
|
RU2066794C1 |
METHOD DETERMINING POSITION OF CENTER OF MASS OF ARTICLE | 1993 |
|
RU2089865C1 |
DEVICE FOR DETERMINATION MASS CENTER OF OBJECT | 0 |
|
SU1820255A1 |
Authors
Dates
1994-12-15—Published
1992-01-15—Filed