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This report details the methodology and findings of the helicopter vibration analysis, focusing on the vibrations caused by damage to the main rotor blades. It includes a computer program designed
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How to fill out Helicopter Forced Response Vibration Analysis Method RTVIB20

01
Gather necessary data and specifications of the helicopter.
02
Prepare the required equipment and tools for vibration analysis.
03
Follow the standard procedure for setting up the helicopter in a controlled environment.
04
Collect baseline vibration data from the helicopter before any modifications.
05
Perform forced response testing under specific flight conditions.
06
Analyze the collected data using appropriate software to identify vibration patterns.
07
Cross-reference the results with established benchmarks or standards.
08
Document findings and provide recommendations for addressing any identified issues.

Who needs Helicopter Forced Response Vibration Analysis Method RTVIB20?

01
Helicopter maintenance engineers.
02
Aerospace reliability and safety analysts.
03
Helicopter manufacturers and designers.
04
Regulatory bodies for aviation safety.
05
Helicopter operators seeking to improve performance and reliability.
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There are two primary types of vibration that affect rotors: vertical and lateral. Vertical vibration often happens when the rotor blades are unable to provide equal lift. Lateral vibration can be caused by unbalanced mass distribution or misalignment of the rotor system.
The vibration level in helicopters is of the order of 0.05 to 0.25g, which is about five times the vibration levels encountered in fixed wing aircraft. This high vibration is due to the very construction and aerodynamics of highly varying velocity fields.
High frequency vibrations are associated with the engine bearings, cooling blower fan blades, the tail rotor driveshaft, or any other component spinning at high revolutionary speeds. Main rotors rotate at close to 360 revolutions per minutes (r.p.m.), with tail rotors generally spinning six times faster than that.
Frequency vibrations — which can be rated as low-, medium-, or high-frequency — are caused by specific kinds of equipment adjustments or malfunctions.
Lateral Low Frequency Vibration are caused by the rotor system being out of balance due to differences in blade weights, incorrect rotor hub grip spacing or trunnion centring, rotor hub internal grease leaks, an out of balance stabilizer bar or a faulty damper.
The effects due to the disadvantages of vibration are believed to be reduced by the employment of a twist morphing technology on the helicopter blades. Active twist rotor method is used to reduce vibration under aerodynamic loads using piezoelectric actuators.
Frequency vibrations — which can be rated as low-, medium-, or high-frequency — are caused by specific kinds of equipment adjustments or malfunctions.
Main rotors typically spin faster than 250 revolutions per minute, meaning a 4/rev vibration would have a frequency above 4*250/60, or 17 Hz. That's 17 vibrations per second, almost like a buzzing. As you might imagine, the strength of these N per rev vibrations varies with speed.

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Helicopter Forced Response Vibration Analysis Method RTVIB20 is a standardized approach used to analyze the vibration response of helicopters to forced excitations, aiming to assess and mitigate potential risks associated with vibration-related issues.
Operators and maintenance organizations that oversee helicopter operations and maintenance programs are required to file Helicopter Forced Response Vibration Analysis Method RTVIB20, especially those where vibration issues could impact safety and performance.
To fill out the RTVIB20 form, the filer must provide detailed information regarding the helicopter's model, vibration measurement data, operating conditions, and any inspections or corrective actions taken, adhering to the guidelines specified in the form.
The purpose of RTVIB20 is to systematically evaluate vibration data to identify any anomalies or trends that could indicate mechanical issues, thereby ensuring the safety and reliability of helicopter operations.
The information that must be reported includes helicopter identification details, vibration data, operational conditions during measurements, any past vibration-related issues, and corrective actions taken to address identified problems.
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