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Helicopter brake starting control circuit, brake starting system and control method

A start-up control and start-up system technology, applied to motor vehicles, machines/engines, rotorcraft, etc., can solve problems such as limiting the use and maintenance of helicopters and the ability to perform tasks, and achieve the effect of avoiding safety risks

Active Publication Date: 2020-04-07
CHINA HELICOPTER RES & DEV INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

thereby limiting the helicopter's ability to use maintenance and perform missions in such scenarios

Method used

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  • Helicopter brake starting control circuit, brake starting system and control method
  • Helicopter brake starting control circuit, brake starting system and control method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0032] figure 2 It is the schematic diagram of the helicopter brake start control circuit, combined with figure 2 As shown, the helicopter braking and starting control circuit of the present embodiment 1 includes an engine electronic controller circuit, a helicopter power supply, a first switch, a second switch, a brake interlock circuit and an engine starter,

[0033] The helicopter power supply, the first switch, the second switch and the engine starter are sequentially connected in series; the brake interlock circuit controls the on-off of the first switch;

[0034] The engine electronic controller circuit includes an engine electronic controller and a starting relay, the engine electronic controller is electrically connected to the starting relay, and controls the operation of the starting relay, and the starting relay controls the on-off of the second switch;

[0035] When both the first switch and the second switch are closed, the engine starter works.

[0036] Furth...

Embodiment 2

[0039] figure 1 The schematic diagram of the rotor brake starting system is combined with figure 1 and figure 2 Shown, a kind of helicopter brake start system, described brake start system comprises brake start control circuit,

[0040] The rotor brake annunciator is signal-connected to the engine electronic controller, and is used to feed back to the engine electronic controller whether the brake stop mechanism has stopped the helicopter rotor;

[0041] After the engine electronic controller receives the start signal, the brake interlock circuit and the engine electronic controller circuit respectively control the on-off of the first switch and the second switch to control the engine starter Starting: the engine electronic controller controls the starting mode and working state of the engine according to the signal fed back by the rotor brake device.

[0042] Further, the starting mode includes a first starting mode and a second starting mode,

[0043] The first start mo...

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PUM

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Abstract

The invention belongs to the field of helicopter engine starting and provides a helicopter brake starting control circuit, a helicopter brake starting system and a control method of the helicopter brake starting system. With the helicopter brake starting control circuit, the helicopter brake starting system and the control method of the helicopter brake starting system adopted, the use, maintenance and task execution requirements of a helicopter under special conditions can be satisfied. The helicopter brake starting system mainly comprises a rotor wing brake device, an engine electronic controller, an engine starting switch and a brake interlocking switch. The system acts on an engine, a transmission system and a rotor wing to achieve a helicopter brake starting function.

Description

technical field [0001] The invention belongs to the field of starting a helicopter engine, and in particular relates to a braking and starting system and a control method for a helicopter turboshaft engine. Background technique [0002] The helicopter relies on the output shaft power of the turboshaft engine to drive the rotor and tail rotor through the transmission system to provide the lift and anti-torque required for flight. The turbine of an aviation turboshaft engine consists of two parts: a gas turbine and a power turbine. The front-end gas turbine drives the compressor to work together to form the rotor of the engine gas generator; the rear-end power turbine is connected to the transmission system through the output shaft to drive the rotor and tail rotor to do work. The gas turbine and the power turbine are not mechanically connected to each other. Under normal circumstances, during the starting process of the turboshaft engine, the high-temperature gas drives the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02C7/268B64C27/12
CPCB64C27/12F02C7/268
Inventor 杨波谌昱王智张宇沛窦志伟田野
Owner CHINA HELICOPTER RES & DEV INST