Device and method for checking the balance of rotor blades relative to each other

DE102025101425A1Undetermined Publication Date: 2026-07-16ELBE FLUGZEUGWERKE GMBH
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Patent Information

Application Number
DE102025101425
Authority / Receiving Office
DE · DE
Patent Type
Applications
Current Assignee / Owner
Filing Date
2025-01-16
Publication Date
2026-07-16

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Abstract

A device (1) and a method (200) for checking the actual state of a rotating component (100) are provided. The device (1) comprises a frame (2), an elongated receiving beam (3), a receptacle (4), a first torque-generating element (5), and a reading device (7). The receiving beam (3) is connected to the frame (2) via a pivot axis (8). The first torque-generating element (5) is arranged on a first side (9) of the receiving beam (3) relative to the pivot axis (8). The receptacle (4) is arranged on a second side (10) of the receiving beam (3) relative to the pivot axis (8). The receptacle (4) is configured to connect the rotating component (100) to the receiving beam (3). The first torque-generating element (5) is adjustable so that a first torque (11) acting from the first side (9) on the axis of rotation (8) can be adjusted.The receiver (4) is configured to transmit a second torque (12) generated by the rotational component (100) from the second side (10) to the axis of rotation (8). The reading device (7) is configured to display a reading associated with the first torque (11), which is associated with the current state of the rotational component.
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Citation Information

Patent Citations

  • DEVICE FOR BALANCING MODEL HELICOPTER ROTOR BLADES

    DE8503412U1

  • Method of assembling a balanced rotor

    US2060901A

  • Testing device

    US2186831A