摘要:
The ignition system (10) of an engine (particularly for a UAV) has a primary (10a), and a secondary (10b) ignition system to provide redundancy for ‘get you home’ capability should the primary ignition system fail. The secondary ignition provides a lower energy or shorter duration spark than the higher energy or longer duration sparking of the primary ignition system, and is retarded relative to primary sparking. Timing of the secondary sparking can be advanced in the event of primary sparking failure. Fuelling strategy can be shifted from a leaner stratified charge to a richer homogenous charge when relying just on the secondary ignition system for ignition. The secondary ignition system can be of a lower spark energy and/or duration than the primary ignition system, avoiding the cost, complexity and weight of replicating the primary ignition system, and to improve packaging within the engine housing, particularly within the limited payload and space limits of a UAV.
摘要:
When an abnormality judgement section (28) judges that there is a failure of an energy inputting circuit (6), an energy inputting line (²), through which electrical energy is inputted from the energy inputting circuit (6) to a primary winding (3), is changed over to a disconnected state by output halt switching means (29). As a result, since inputting of electrical energy to the primary winding (3) is thereby halted, problems arising due to continuation of inputting electrical energy to the energy inputting circuit (6) can be prevented, even in the event of a failure of the energy inputting circuit (6), so that reliability can be enhanced.
摘要:
An ignition control apparatus for engines is provided. The ignition control apparatus is designed to control a switch to release energy stored in a capacitor during spark discharge, thereby supplying a primary current to an other end side opposite a one end of a primary winding of an ignition coil connected to a dc power supply. This provides the ignition control apparatus which is capable of minimizing an increase in size or manufacturing cost and stabilizing the state of combustion of an air-fuel mixture.
摘要:
In a laser ignition device 1 which is mounted in an internal combustion engine 5 and at least includes a laser spark plug 10 equipped with an optical window 100 which protects an optical device from high temperature and high pressure generated in a combustion chamber and a prechamber cap 15 equipped with a cylindrical prechamber 152, a prechamber throat portion 151 that is a bottomed cylinder with a sectional area smaller than that of the prechamber, and a plurality of prechamber spray holes 150 which communicate with a combustion chamber 500 on a side of a closed end 153 of the prechamber throat portion 151, the prechamber cap 15 is arranged between the optical window 100 and the combustion chamber 500. A converging point FP is located inside the prechamber 152 to ignite an air-fuel mixture delivered into the prechamber 152, thereby jetting combustion flames from the prechamber 152 into the combustion chamber 500 to fire the internal combustion engine 5. The center axis AX F of the prechamber 152 is oriented horizontally eccentrically from the center axis AXs of the prechamber throat portion 151.
摘要翻译:在安装在内燃机5中并且至少包括配备有光学窗口100的激光火花塞10的激光点火装置1中,光学窗口100保护光学装置免受燃烧室中产生的高温和高压以及预燃室盖 15,其具备圆筒状的预燃室152,作为截面积小于预燃室的截面积的有底圆筒状的预燃室用喉部151,以及与封闭侧的燃烧室500连通的多个预燃室喷出孔150 在预燃室喉部151的端部153处,预燃室盖15布置在光学窗口100和燃烧室500之间。会聚点FP位于预燃室152内,以点燃输送到预燃室152中的空气 - 燃料混合物,由此 将燃烧火焰从预燃室152喷射到燃烧室500中以发动内燃机5.中心轴线AX F 容室152从预燃室喉部151的中心轴线AXs水平偏心地取向。
摘要:
[Problem] To provide an ignition system for a compact internal combustion engine, which does not require a complex system or a spark plug which discharges a high voltage, and which, by using only electromagnetic waves, can efficiently generate, expand and maintain plasma. Moreover, to provide an internal combustion engine. This ignition system is characterized by comprising: an electromagnetic wave oscillator (3) which oscillates electromagnetic waves; a control device (4) that controls the electromagnetic wave oscillator (3); and a plasma generator (10) which integrates a booster circuit (5) containing a resonant circuit capacitive coupled with the electromagnetic wave oscillator (3), and a discharge electrode (6) which discharges a high voltage generated by the booster circuit (5), wherein the plasma generator (10) comprises a plurality of discharge electrodes (6) arranged so as to be exposed within the combustion chamber of the internal combustion engine.