CN103967535A - Refrigeration and electricitygeneration integrated device driven by air turbine - Google Patents
Refrigeration and electricitygeneration integrated device driven by air turbine Download PDFInfo
- Publication number
- CN103967535A CN103967535A CN201310041391.7A CN201310041391A CN103967535A CN 103967535 A CN103967535 A CN 103967535A CN 201310041391 A CN201310041391 A CN 201310041391A CN 103967535 A CN103967535 A CN 103967535A
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- air turbine
- refrigeration
- electricitygeneration
- air
- control system
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- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Abstract
The invention provides a refrigeration and electricitygeneration integrated device driven by an air turbine, relates to the field of aviation, and aims to solve the energy saving problem of the air turbine driving. The invention adopts the technical scheme as follows: the refrigeration and electricitygeneration integrated devicecomprises anair turbine component, wherein a generator rotor is arranged on the shaft of the air turbine component; a generator stator matched with the generator rotor is fixed to the housing of the air turbinecomponent. The device provided by theinvention has the advantages as follows: the energy of the air turbine component of an environmental control system in the rotating process is fully used, and the device is suitable for various air turbine drivingenvironments.
Description
Technical field
The present invention relates to aviation field, relate in particular to refrigeration and generating integration device that a kind of air turbine drives.
Background technique
No matter the driving power that current all aircraft environmental control system motor drive mechanisms use, all by aircraft task power-supply system, is that early stage Boeing-737, A320 or state-of-the-art Boeing 787 flies, A380 aircraft is all like this.Along with the development of environmental control system technology, the air turbine assembly that environmental control system uses by two-wheeled, three-wheel, develop into present four-wheel, bearing technology also has that early stage bearing oil is lubricated to be developed into the present air selflubricating stage.But before certain, do not find to adopt such technology to carry out the application case of coaxial generating.
Summary of the invention
The object of the invention is: the refrigeration and the generating integration device that provide a kind of air turbine to drive, can rationally utilize resource on machine, reduce the compensatory loss of aircraft, improve aircraft reliability and system and combine integration capability.
Technological scheme of the present invention is: refrigeration and generating integration device that a kind of air turbine drives, comprise: air turbine assembly, on the axle of air turbine assembly, be provided with generator amature, the generator unit stator mating with described generator amature is fixed on air turbine assembly housing.
The invention has the beneficial effects as follows: this invention can make full use of the energy of environmental control system air turbine assembly in rotary course, do not changing on the basis of environmental control system turbine original function, realize the self-supporting function of power supply of environmental control system, contribute to the raising of aircraft safety and environmental control system reliability, for the integrated self-adaptive design of follow-up environmental control system refrigeration heating system provides platform
Brief description of the drawings
Fig. 1 is that the present invention makes existing two wheel constructions into refrigeration and generating integration device structural representation that the air turbine after three-wheel form drives.
Fig. 2 is that the present invention makes existing tricycle structure into refrigeration and generating integration device structural representation that the air turbine after four-wheel form drives.
Embodiment
Below in conjunction with accompanying drawing, the present invention is described in further detail:
The present invention increases a generating rotor coil in the middle of air turbine assembly (two-wheeled, the Three-wheel type) axle of active service moulding, and the generating stator coil mating with described generating rotor coil is fixed on air turbine assembly housing.Drive turbine gas to expand by high-pressure air source and outwards do work, drive coaxial rotor to rotate, rotor rotation process cuts the generating stator coil magnetic line of force coaxial with turbine and forms electric current output.
The present invention improves existing turbine and system, utilizes turbine output to drive gas compressor fan and generator to carry out work.Specific implementation method is as follows:
As shown in Figure 1, make existing two wheel constructions into three-wheel form, between fan and turbine, increase an electricity generating device, utilize the output work of turbine to generate electricity.
As shown in Figure 2, make existing tricycle structure into four-wheel form, between fan and gas compressor, increase an electricity generating device, utilize the output work of turbine to generate electricity.
This technology is a kind of new invention, this invention can make full use of the energy of environmental control system air turbine assembly in rotary course, do not changing on the basis of environmental control system turbine original function, realize the self-supporting function of power supply of environmental control system, contribute to the raising of aircraft safety and environmental control system reliability, for the integrated self-adaptive design of follow-up environmental control system refrigeration heating system provides platform.
Claims (1)
1. refrigeration and the generating integration device that air turbine drives, comprise: air turbine assembly, it is characterized in that, on the axle of air turbine assembly, be provided with generator amature, the generator unit stator mating with described generator amature is fixed on air turbine assembly housing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310041391.7A CN103967535A (en) | 2013-02-01 | 2013-02-01 | Refrigeration and electricitygeneration integrated device driven by air turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310041391.7A CN103967535A (en) | 2013-02-01 | 2013-02-01 | Refrigeration and electricitygeneration integrated device driven by air turbine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103967535A true CN103967535A (en) | 2014-08-06 |
Family
ID=51237491
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310041391.7A Pending CN103967535A (en) | 2013-02-01 | 2013-02-01 | Refrigeration and electricitygeneration integrated device driven by air turbine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103967535A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH1068357A (en) * | 1996-08-28 | 1998-03-10 | Ishikawajima Harima Heavy Ind Co Ltd | High speed aircraft |
| CN1682023A (en) * | 2002-09-06 | 2005-10-12 | 普维尼布伦卡斯托伊纳大比泰什公司 | Jet motor or turbine motor |
| CN1869437A (en) * | 2006-06-05 | 2006-11-29 | 南京航空航天大学 | Built-in by-pass punching ram-air turbine generator |
| CN101016847A (en) * | 2007-02-27 | 2007-08-15 | 南京航空航天大学 | High supersound air-intake air turbogenerator |
| CN101237171A (en) * | 2008-02-14 | 2008-08-06 | 吴亚娟 | Novel vehicular wind power generator and vehicular wind dynamics air-conditioner |
| CN101446301A (en) * | 2008-12-17 | 2009-06-03 | 中国航天科技集团公司第六研究院第十一研究所 | Miniature high-speed air turbine pump |
| CN101451464A (en) * | 2007-12-03 | 2009-06-10 | 上海空间电源研究所 | Fuel cell engine air turbine compressor with energy recovery |
-
2013
- 2013-02-01 CN CN201310041391.7A patent/CN103967535A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH1068357A (en) * | 1996-08-28 | 1998-03-10 | Ishikawajima Harima Heavy Ind Co Ltd | High speed aircraft |
| CN1682023A (en) * | 2002-09-06 | 2005-10-12 | 普维尼布伦卡斯托伊纳大比泰什公司 | Jet motor or turbine motor |
| CN1869437A (en) * | 2006-06-05 | 2006-11-29 | 南京航空航天大学 | Built-in by-pass punching ram-air turbine generator |
| CN101016847A (en) * | 2007-02-27 | 2007-08-15 | 南京航空航天大学 | High supersound air-intake air turbogenerator |
| CN101451464A (en) * | 2007-12-03 | 2009-06-10 | 上海空间电源研究所 | Fuel cell engine air turbine compressor with energy recovery |
| CN101237171A (en) * | 2008-02-14 | 2008-08-06 | 吴亚娟 | Novel vehicular wind power generator and vehicular wind dynamics air-conditioner |
| CN101446301A (en) * | 2008-12-17 | 2009-06-03 | 中国航天科技集团公司第六研究院第十一研究所 | Miniature high-speed air turbine pump |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20140806 |