Real-time detection device for turbojet power of a vertical aircraft

By installing a force sensor on the output shaft of a turbojet engine and combining it with a modular structure, the mechanical loss and response delay problems of turbojet engine power detection in existing technologies have been solved, enabling real-time and accurate thrust detection, improving the stability and control accuracy of the aircraft, and reducing maintenance costs.

CN224286383UActive Publication Date: 2026-05-26天津璐珩智能科技有限公司

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
天津璐珩智能科技有限公司
Filing Date
2025-08-12
Publication Date
2026-05-26

AI Technical Summary

Technical Problem

Existing turbojet engine power detection technologies suffer from mechanical losses, slow dynamic response speed, response delay, and insufficient applicability. They cannot accurately detect engine power output in real time, especially when the engine is accelerating or experiencing sudden load changes, the detected data deviates significantly from the true value.

Method used

The modular vertical takeoff and landing vehicle turbojet power real-time detection device directly collects thrust data by installing a force gauge at the output axis of the turbojet engine. Combined with components such as guide rails, sliders, and clamps, it ensures a stable connection between the force gauge and the engine, achieving real-time and accurate detection.

Benefits of technology

It significantly improves the dynamic response capability and data accuracy of detection, supports the synchronous detection and dynamic balance monitoring of multiple engines, improves the attitude stability and control accuracy of the aircraft, reduces maintenance costs, adapts to extreme working conditions, and facilitates installation and maintenance.

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Abstract

This utility model discloses a real-time detection device for the turbojet power of a vertical takeoff and landing vehicle, relating to the technical field of detection devices. The real-time detection device uses a fixed frame connected to a clamp via a guide rail and a slider structure to fix the turbojet engine. The clamp is connected to the fixed frame via a force gauge set on the axis of the turbojet engine. It can collect thrust data in real time, avoiding the data delay and distortion problems caused by response lag and indirect calculation in traditional dynamometer methods, and significantly improving the dynamic response capability and data accuracy of the detection.
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