发明公开
EP0473530A1 Variable regulator for pneumatic airplane starters
失效
变量调节器fneumzechen Flugzeuganlasser。
- 专利标题： Variable regulator for pneumatic airplane starters
- 专利标题（中）： 变量调节器fneumzechen Flugzeuganlasser。
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申请号： EP91500101.0申请日： 1991-08-23
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公开(公告)号： EP0473530A1公开(公告)日： 1992-03-04
- 发明人: Lorente Arcas, Ambrosio
- 申请人： Lorente Arcas, Ambrosio
- 申请人地址： Angel Beato, 12 E-28035 Madrid ES
- 专利权人： Lorente Arcas, Ambrosio
- 当前专利权人： Lorente Arcas, Ambrosio
- 当前专利权人地址： Angel Beato, 12 E-28035 Madrid ES
- 代理机构： Ungria Lopez, Javier
- 优先权： ES9002266 19900825
- 主分类号： F02N7/14
- IPC分类号： F02N7/14 ; B64F1/34
摘要：
The regulator makes it possible to start different types of airplanes with a single starter, providing it the pressure and air flow required.
Upon the operator selecting the start step corresponding to the plane to start, the convenient rating of the turbine is set by operating a simple control that controls the flow of fuel to the combustion chamber, using the indications of a sensor that indicates to it the rotation speed achieved by the turbine. When the operation so requires, in order to obtain the pressure and air flow that the airplane needs to start, the system also activates different mechanisms.
As an alternative, by means of a microprocessor the start step corresponding to the plane to start can be chosen automatically, using the indications of pressure and flow at the inlet of the airplane.
Upon the operator selecting the start step corresponding to the plane to start, the convenient rating of the turbine is set by operating a simple control that controls the flow of fuel to the combustion chamber, using the indications of a sensor that indicates to it the rotation speed achieved by the turbine. When the operation so requires, in order to obtain the pressure and air flow that the airplane needs to start, the system also activates different mechanisms.
As an alternative, by means of a microprocessor the start step corresponding to the plane to start can be chosen automatically, using the indications of pressure and flow at the inlet of the airplane.
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