FIELD: mechanical engineering. SUBSTANCE: tested member is anchored on vibrator and loaded with mass which form together oscillatory system. For increase of accuracy of determination of characteristics of deformed member inertial properties end elastic-dissipative characteristic of deformed member are found by value of effort in point of anchoring of deformed member and vibrator is excited by random vibration. EFFECT: increased accuracy of determination of characteristics of deformed member. 1 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF ESTIMATING EFFICIENCY OF VIBRATION PROTECTION OF EQUIPMENT | 1989 |
|
RU2011173C1 |
METHOD DETERMINING AMPLITUDE-FREQUENCY CHARACTERISTICS OF MULTIDIMENSIONAL ELASTIC SYSTEM WITH MULTICHANNEL INPUT | 1993 |
|
RU2114408C1 |
METHOD OF DYNAMIC TESTING OF DEFORMABLE ELEMENTS | 0 |
|
SU699386A1 |
ACCELEROMETER | 1994 |
|
RU2091797C1 |
AERODYNAMIC EXCITER OF VIBRATION OF AIRCRAFT WING | 1996 |
|
RU2144657C1 |
AIRFIELD LIGHTING SYSTEM MODEL FOR LANDING TRAINING | 1992 |
|
RU2042981C1 |
METHOD OF IDENTIFICATION OF AERODYNAMIC CHARACTERISTICS OF AUTOMATICALLY CONTROLLED FLIGHT VEHICLES | 1994 |
|
RU2124711C1 |
METHOD OF MEASUREMENT OF RANDOM VIBRATION LOADS ON ENGINES OF AIRCRAFT POWER PLANT | 1992 |
|
RU2036450C1 |
0 |
|
SU1779968A1 | |
METHOD OF DYNAMIC BALANCING OF AIR-PROPELLER SET OF POWER UNIT ON AIRCRAFT | 1992 |
|
RU2039958C1 |
Authors
Dates
1997-07-27—Published
1991-04-09—Filed