公开(公告)号：US06720669B1

公开(公告)日：2004-04-13

申请号：US10287021

申请日：2002-11-04

申请人： Eugene Chiappe ,  Leven Edward Staples

发明人： Eugene Chiappe ,  Leven Edward Staples

IPC分类号： F02N1506

CPC分类号： F02N15/066

摘要： A starter for a piston aircraft engine is constructed by placing the pinion-gear and drive clutch, the engagement solenoid and the driving motor in a linear arrangement, the motor driving the clutch via a geared shaft passing by the engagement solenoid. Such construction provides minimum diameter for a solenoid-engaged piston aircraft engine starter in order to fit the available space on existing aircraft originally designed to be equipped with centrifugally-engaged starters.

摘要翻译： 用于活塞式飞机发动机的起动器通过将小齿轮和驱动离合器，接合螺线管和驱动电机放置成线性布置而构成，电动机通过通过接合螺线管的齿轮轴驱动离合器。 这种结构为螺线管接合的活塞式飞机发动机起动器提供最小直径，以便将原来设计成装备有离心式起动器的现有飞机上的可用空间配合。