Airplane hydraulic system layout based on hydraulic and power-by-wire boosting and energy storing devices

A booster energy storage device and aircraft hydraulic technology, applied in the field of hydraulic systems, can solve problems such as thick parts and increased aircraft weight

Inactive Publication Date: 2016-06-01
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0013] EDP ​​and pipelines need to withstand high pressure, re...

Method used

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  • Airplane hydraulic system layout based on hydraulic and power-by-wire boosting and energy storing devices
  • Airplane hydraulic system layout based on hydraulic and power-by-wire boosting and energy storing devices
  • Airplane hydraulic system layout based on hydraulic and power-by-wire boosting and energy storing devices

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Embodiment Construction

[0027] Embodiments of the present application are described below with reference to the drawings. Elements and features described in one drawing or one embodiment of the present application may be combined with elements and features shown in one or more other drawings or embodiments. It should be noted that representation and description of components and processes that are not relevant to the present application and known to those of ordinary skill in the art are omitted from the drawings and descriptions for the purpose of clarity.

[0028] see figure 1 Shown is a structural diagram 100 of an embodiment of the layout of an aircraft hydraulic system based on a hydraulic pressure and a power-by-wire boost energy storage device of the present application.

[0029] In this embodiment, the layout of the aircraft hydraulic system based on hydraulic pressure and power electric boost energy storage device includes:

[0030] The spoiler aileron accumulator 110 is used to drive the ...

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Abstract

The invention relates to an airplane hydraulic system layout based on hydraulic and power-by-wire boosting and energy storing devices. The airplane hydraulic system layout based on the hydraulic and power-by-wire boosting and energy storing devices comprises a spoiler and aileron energy storing device, a cabin door energy storing device and an empennage energy storing device, wherein the spoiler and aileron energy storing device is used for driving a spoiler steering engine and an aileron steering engine; the cabin door energy storing device is used for driving a cabin door actuator; the empennage energy storing device is used for respectively driving a rudder steering engine and an elevator steering engine; the spoiler and aileron energy storing device and the cabin door energy storing device are connected with an engine driving pump, and are used for receiving oil pressure input from the engine driving pump; and the empennage energy storing device is connected with a power-by-wire control system of an airplane, and is used for storing energy or actuating on the basis of an output instruction of the power-by-wire control system. By the airplane hydraulic system layout based on the hydraulic and power-by-wire boosting and energy storing devices, installed power of the airplane can be reduced.

Description

technical field [0001] The present application relates to the field of hydraulic systems, in particular to an aircraft hydraulic system layout based on hydraulic pressure and power transmission boost energy storage devices. Background technique [0002] The aircraft hydraulic system is one of the main onboard systems of the aircraft. The control and actuators of the main control system and auxiliary control system of modern aircraft use hydraulic pressure as the energy source, and hydraulic actuators or hydraulic motors as the actuators. The aircraft hydraulic system refers to the complete set of devices on the aircraft that use oil as the working medium and rely on oil pressure to drive the actuator to complete specific manipulation actions. In order to ensure the reliability of the hydraulic system, especially to improve the reliability of the hydraulic power source of the flight control system, most modern aircraft are equipped with two (or more) independent hydraulic sy...

Claims

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Application Information

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IPC IPC(8): B64C13/40F15B1/02
CPCB64C13/40F15B1/02
Inventor 焦宗夏刘晓超尚耀星李兴鲁
Owner BEIHANG UNIV
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