بازدیدکننده گرامی این صفحه در حال بروزرسانی و بازطراحی میباشد لذا ممکن است در حال حاضر برخی از مطالب قابل رویت نباشند
- RPM sensor and digital display to indicate real-time angular velocity, as well as switches for changing the direction of rotor spin and gimbal rotary system
- Rotor with proper motor and precise driver to increase motor revolutions to 3500rpm
- A volume control to increase and/or decrease the rotor or gimbal rotary angular speed
- Revolutions and rotors speed are controlled by closed loop control
- Low friction gimbal hinge and leveling mechanism to level the rotor prior to applying balance weights
- A bifilar system to obtain the actual value of moment of inertia in the motor’s coil and accessories
- A transparent plastic protection shield, resistant to impact, enabling the operator to have clear vision and easy control on the experiment
- A balance piece to make balance the rotor weight prior to applying the test weights
- Easy and safe operation
Machine is used to obtain the gyroscopic couple, review the dynamics of a gyroscope under rotor moment of inertia, as well as gimbal and rotor angular velocity. To carry out the experiment more easily, buttons and control volumes are intended to adjust the angular velocity and their directions. Moment of inertia is obtained via bifilar method. For this purpose, first we should fasten the rotor coil and the accessories (which are the same as the rotor) to the bifilar hanger by means of two wires and two bolts; then the bifilar assembly is deviated round the axis between the two hangers for few degrees and released to get oscillation. Once the time for the complete oscillations (usually 50 oscillations) is recorded, the period of oscillation can be calculated. Next, we displace the counterbalance to the extent that the arm assumes the balance position. In order to measure the gyroscopic couple, the test weights should be screwed into their place, and then we should increase the speed of gimbal and rotor to the extent that the gyroscopic couple lifts up the test weight and keep it balanced. Upon the obtained results and by drawing graphs, the linearity of the equations can be studied; graphs are plotted in terms of rotor-couple velocity, gimbal-couple velocity, and rotor-gimbal velocity. A transparent protective shield is mounted on the machine to prevent throwing pieces, and a micro switch is intended to stop the machine from running if the shield is not secured properly.
The machine is designed to test generated couples in a gyroscope and provides the possibility of analogy between theoretic values with experimental ones. On the other hand, upon the obtained results, the effect of rotation direction, gimbal rotary speed, rotor angular velocity and moment of inertia can be can be studied against the gyroscopic couple.
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سازنده:
شرکت طراحی مهندسی سنتام
استعلام قیمت
درخواست مشاوره
دانلود کاتالوگ
شرایط تحویل حضوری
شرایط تحویل کالا در محل کارخانه
جزییات بیشتر
شرایط ارسال دستگاه
شرایط ارسال دستگاه و حمل آن
جزییات بیشتر
متن آزمایشی
متن آزمایشی
جزییات بیشتر
گارانتی دستگاه
شرایط خدمات پس از فروش
جزییات بیشتر
جزییات بیشتر
- RPM sensor and digital display to indicate real-time angular velocity, as well as switches for changing the direction of rotor spin and gimbal rotary system
- Rotor with proper motor and precise driver to increase motor revolutions to 3500rpm
- A volume control to increase and/or decrease the rotor or gimbal rotary angular speed
- Revolutions and rotors speed are controlled by closed loop control
- Low friction gimbal hinge and leveling mechanism to level the rotor prior to applying balance weights
- A bifilar system to obtain the actual value of moment of inertia in the motor’s coil and accessories
- A transparent plastic protection shield, resistant to impact, enabling the operator to have clear vision and easy control on the experiment
- A balance piece to make balance the rotor weight prior to applying the test weights
- Easy and safe operation
Machine is used to obtain the gyroscopic couple, review the dynamics of a gyroscope under rotor moment of inertia, as well as gimbal and rotor angular velocity. To carry out the experiment more easily, buttons and control volumes are intended to adjust the angular velocity and their directions. Moment of inertia is obtained via bifilar method. For this purpose, first we should fasten the rotor coil and the accessories (which are the same as the rotor) to the bifilar hanger by means of two wires and two bolts; then the bifilar assembly is deviated round the axis between the two hangers for few degrees and released to get oscillation. Once the time for the complete oscillations (usually 50 oscillations) is recorded, the period of oscillation can be calculated. Next, we displace the counterbalance to the extent that the arm assumes the balance position. In order to measure the gyroscopic couple, the test weights should be screwed into their place, and then we should increase the speed of gimbal and rotor to the extent that the gyroscopic couple lifts up the test weight and keep it balanced. Upon the obtained results and by drawing graphs, the linearity of the equations can be studied; graphs are plotted in terms of rotor-couple velocity, gimbal-couple velocity, and rotor-gimbal velocity. A transparent protective shield is mounted on the machine to prevent throwing pieces, and a micro switch is intended to stop the machine from running if the shield is not secured properly.


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