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Aeroengine nozzle side fault-tolerant generator

A technology for aero-engines and generators, applied in electromechanical devices, electrical components, electric components, etc., can solve the problems of few patent applications and weak foundation of aero-generators, and achieve high back EMF, high motor power, and small internal resistance Effect

Active Publication Date: 2019-11-05
徐州博云航空科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] At present, my country's foundation in the field of aviation generators is relatively weak, and there are few patent applications in this field

Method used

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  • Aeroengine nozzle side fault-tolerant generator
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  • Aeroengine nozzle side fault-tolerant generator

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Embodiment Construction

[0026] The present invention provides a five-phase permanent magnet motor for an extended-range electric vehicle. In order to make the technical solution and effect of the present invention clearer and clearer, the present invention is further described in detail with reference to the accompanying drawings and examples. It should be understood that the specific implementations described here are only used to explain the present invention, not to limit the present invention.

[0027] figure 1 It is a cross-sectional view of a fault-tolerant generator device on the nozzle side of an aero-engine, including an excitation winding, an excitation core, a rotor core, an armature winding and an armature core, and is characterized in that: the rotor core is fixed on the nozzle side of the low-pressure shaft of the aero-engine; The disc-shaped field core, rotor core and armature core are coaxially arranged sequentially, and the field core and armature core are fixed on the aircraft engin...

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Abstract

The invention relates to a fault tolerant generator at the nozzle side of an aerial engine, and belongs to the field of aircraft engineering. The fault tolerant generator comprises an excitation coil,an excitation iron core, a rotor iron core, an armature coil and an armature iron core; the rotor iron core is fixed at one side of the nozzle of the low-pressure shaft of the aerial engine; the excitation iron core and the armature iron core are separately positioned at two axial sides of the rotor iron core; 12 fan-shaped through holes are uniformly distributed on the circumference of the rotoriron core; 10 fan-shaped protruding excitation poles are at one side of the excitation iron core towards the rotor iron core; 10 fan-shaped protruding armature poles are at one side of the armature iron core towards the rotor iron core; a centralized excitation coil is wound on each excitation pole; and a centralized armature coil is wound on each armature pole. According to the fault tolerant generator disclosed by the invention, the rotational inertia of the rotor iron core is low; therefore, the rotor iron core can rotate at high speed; and thus, the rotor iron core is particularly suitable for the fault tolerant generator at the nozzle side of the aerial engine.

Description

technical field [0001] The invention relates to a fault-tolerant generator at the nozzle side of an aero-engine, belonging to the field of aeronautical electrical engineering. Background technique [0002] More electric aircraft and all-electric aircraft are the inevitable trend of modern aircraft development. Having a starter generator is an important feature of a multi-electric aircraft. On the basis of the traditional aviation gas turbine engine, the magnetic suspension bearing for the built-in starter generator to support the engine rotor is installed inside the aircraft engine, eliminating the need for a transmission mechanism and running at a high speed. Provide sufficient power to supply components such as distributed electronic control systems, electric fuel pumps and electric actuators. [0003] With the development of science and technology, motors have been more and more widely used in military and civilian fields. However, aerospace and other fields that have hi...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H02K1/14H02K3/28H02K3/18H02K1/22
CPCH02K1/146H02K1/22H02K3/18H02K3/28
Inventor 史立伟周波侯振煜倪广阔王浩男化思展孙彦章
Owner 徐州博云航空科技有限公司
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