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  1. #11
    مشرف قسم تقنية الطيران وعلوم الفضاء
    تاريخ التسجيل
    May 2007
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    افتراضي

    Two Stroke Engine
    The two stroke engine employs the crankcase as well as the cylinder to achieve all the elements of the Otto cycle in only two strokes of the piston. Intake. The fuel/air mixture is first drawn into the crankcase by the vacuum created during the upward stroke of the piston. The illustrated engine features a poppet intake valve, however many engines use a rotary value incorporated into the crankshaft.
    During the downward stroke the poppet valve is forced closed by the increased crankcase pressure. The fuel mixture is then compressed in the crankcase during the remainder of the stroke.
    Transfer/Exhaust. Toward the end of the stroke, the piston exposes the intake port, allowing the compressed fuel/air mixture in the crankcase to escape around the piston into the main cylinder. This expels the exhaust gasses out the exhaust port, usually located on the opposite side of the cylinder. Unfortunately, some of the fresh fuel mixture is usually expelled as well. Compression. The piston then rises, driven by flywheel momentum, and compresses the fuel mixture. (At the same time, another intake stroke is happening beneath the piston).
    Power. At the top of the stroke the spark plug ignites the fuel mixture. The burning fuel expands, driving the piston downward, to complete the cycle.
    Since the two stroke engine fires on every revolution of the crankshaft, a two stroke engine is usually more powerful than a four stroke engine of equivalent size. This, coupled with their lighter, simpler construction, makes two stroke engines popular in chainsaws, line trimmers, outboard motors, snowmobiles, jet-skis, light motorcycles, and model airplanes. Unfortunately most two stroke engines are inefficient and are terrible polluters due to the amount of unspent fuel that escapes through the exhaust port.
    اللهم أرنا الحق ,,, حقا ,,,, و أرزقنا اتباعه ,,,,
    و أرنا الباطل ,,, باطلا ,,,, و
    ارزقنا اجتنابه


  2. #12
    عضو
    تاريخ التسجيل
    Apr 2007
    الدولة
    فلسطين
    المشاركات
    456

    افتراضي

    بارك الله فيك يا أبو أيوي على المعلومات عن المحركات
    وإذا أمكنك مع الوقت أن تتوسع في المحركات النفاثة لكن بشكل مبسط فحيهلا

  3. #13
    مشرف قسم تقنية الطيران وعلوم الفضاء
    تاريخ التسجيل
    May 2007
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    188

    افتراضي

    Wankel Engine
    The Wankel radial engine is a fascinating beast that features a very clever rearrangment of the four elements of the Otto cycle. It was developed by Felix Wankel in the 1950s.1 In the Wankel a triangular rotor incorporating a central ring gear is driven around a fixed pinion within an oblong chamber.

    The fuel/air mixture is drawn in the intake port during this phase of the rotation.
    The mixture is compressed here.
    The mixture burns here, driving the rotor around.
    And the exhaust is expelled here.
    The rotory motion is transferred to the drive shaft via an eccentric wheel (illustrated in blue) that rides in a matching bearing in the rotor. The drive shaft rotates once during every power stroke instead of twice as in the Otto cycle.
    The Wankel promised higher power output with fewer moving parts than the Otto cycle engine, however technical difficulties have apparently interfered with widespread adoption. In spite of valiant efforts by Mazda, the four stroke engine remains much more popular.
    اللهم أرنا الحق ,,, حقا ,,,, و أرزقنا اتباعه ,,,,
    و أرنا الباطل ,,, باطلا ,,,, و
    ارزقنا اجتنابه


  4. #14
    مشرف قسم تقنية الطيران وعلوم الفضاء
    تاريخ التسجيل
    May 2007
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    افتراضي

    Atkinson Engine
    The Atkinson engine is essentially an Otto-cycle engine with a different means of linking the piston to the crankshaft. It was originally designed to compete with the Otto engine, but without infringing on any of Otto's patents.
    The clever arrangement of levers allows the Atkinson to cycle the piston through all four strokes in only one revolution of the main crankshaft, and allows the strokes to be different lengths -- the intake and exhaust strokes are longer than the compression and power strokes (In this illustration... see below).
    This also obviates the need for a separate cam shaft. The intake (if used), exhaust, and ignition cams are located on the main crank shaft. My illustration shows only an exhaust cam.
    Everything I know about the Atkinson engine came out of Building the Atkinson cycle Engine. This illustration draws heavily from that excellent book.
    10/1/00 Update: A sharp-eyed, well informed visitor to this site has just discovered an important error in one of the above statements, and in my illustration. In Atkinson's original engine, the power stroke was made longer than the intake stroke. Apparently, by allowing the mixture to expand to a larger volume than was drawn into the cylinder, more energy was extracted giving greater fuel efficiency than the Otto-cycle (everything else being equal). Thank yous go to George, for pointing this out; and John for the additional information. My illustration draws from a book about building a model of the Atkinson engine. I may have my measurements wrong, or perhaps even the model designer may not have taken the stroke lengths so carefully into account. After all, he didn't have much to work with: "...Jim was able to build his engine using one simple drawing and a photo..."2
    In any case I still recommend the book, and still feel that I've correctly illustrated the fundamental operation of the Atkinson. I would love to hear any additional comments about this delightful engine.
    اللهم أرنا الحق ,,, حقا ,,,, و أرزقنا اتباعه ,,,,
    و أرنا الباطل ,,, باطلا ,,,, و
    ارزقنا اجتنابه


  5. #15
    مشرف قسم تقنية الطيران وعلوم الفضاء
    تاريخ التسجيل
    May 2007
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    افتراضي

    I've grudgingly included this section by popular request. Rocket and turbojet engines are fabulous technological achievements--But they're so simple the animations are boring! ...At least I think so. You be the judge!
    Rocket
    The rocket engine is the simplest of this family, so I'll start with it.
    In order to work in outer space, rocket engines must carry their own supply of oxygen as well as fuel. The mixture is injected into the combustion chamber where it burns continuously. The high-pressure gas escapes through the nozzle, causing thrust in the opposite direction.To illustrate the principle yourself, inflate a toy balloon and release it (without tying it off!). ...rocket propulsion at its simplest.
    Turbojet
    The turbojet employs the same principle as the rocket. It burns oxygen from the atmosphere instead of carrying a supply along.
    Notice the similarities: Fuel continuously burns inside a combustion chamber just like the rocket. The expanding gasses escape out the nozzle generating thrust in the opposite direction.
    Now the differences: On its way out the nozzle, some of the gas pressure is used to drive a turbine. A turbine is a series of rotors or fans connected to a single shaft. Between each pair of rotors is a stator -- something like a stationary fan. The stators realign the gas flow to most effectively direct it toward the blades of the next rotor.At the front of the engine, the turbine shaft drives a compressor. The compressor works a lot like the turbine only in reverse. Its purpose is to draw air into the engine and pressurize it. Turbojet engines are most efficient at high altitudes, where the thin air renders propellers almost useless.
    Turboprop
    The turboprop is similar to the turbojet, except that most of the nozzle gas pressure drives the turbine shaft -- by the time the gas gets past the turbine, there's very little pressure left to create thrust. Instead, the shaft is geared to a propeller which creates the majority of the thrust. 'Jet' helicopters work the same way, except that their engines are connected to the main rotor shaft instead of a propeller.
    Turboprops are more fuel efficient than turbojets at low altitudes, where the thicker air gives a propeller a lot more 'traction.' This makes them popular on planes used for short flights, where the time spent at low altitudes represents a greater percentage of the overall flight time.
    Turbofan
    The turbofan is something like a compromise between a pure turbojet and a turboprop. It works like the turbojet, except that the turbine shaft also drives an external fan, usually located at the front of the engine. The fan has more blades than a propeller and spins much faster. It also features a shroud around its perimeter, which helps to capture and focus the air flowing through it. These features enable the fan to generate some thrust at high altitudes, where a propeller would be ineffective.
    Much of the thrust still comes from the exhaust jet, but the addition of the fan makes the engine more fuel efficient than a pure turbojet. Most modern jetliners now feature turbofan engines.
    اللهم أرنا الحق ,,, حقا ,,,, و أرزقنا اتباعه ,,,,
    و أرنا الباطل ,,, باطلا ,,,, و
    ارزقنا اجتنابه


  6. #16
    مشرف قسم تقنية الطيران وعلوم الفضاء
    تاريخ التسجيل
    May 2007
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    افتراضي

    Gnome
    The Gnome was one of several rotary engines popular on fighter planes during World War I. In this type of engine, the crankshaft is mounted on the airplane, while the crankcase and cylinders rotate with the propeller.The Gnome was unique in that the intake valves were located within the pistons. Otherwise, this engine used the familiar Otto four stroke cycle. At any given point, each of the cylinders is in a different phase of the cycle. In the following discussion, follow the master cylinder with the green connecting rod. During this portion of the stroke, a vacuum forms in the cylinder, forcing the intake valve open and drawing the fuel-air mixture in from the crankcase.The mixture is compressed during this phase. The spark plug fires toward the end of the compression stroke, slightly before top dead center.The power stroke happens here. Note that the exhaust valve opens early -- well before bottom dead center. This engine has a fairly long exhaust stroke. In order to improve power or efficiency, engine valve timing often varies from what one might expect.
    When I first learned how these engines worked, I thought the only person crazier than the engine designer was the one who paid money for it. At first glance it seems ridiculously backwards.
    Nonetheless, a number of engines were designed this way, including the Gnome, Gnome Monosoupape, LeRhone, Clerget, and Bentley to name a few. It turns out there were some good reasons for the configuration:
    Balance. Note that the crankcase and cylinders revolve in one circle, while the pistons revolve in another, offset circle. Relative to the engine mounting point, there are no reciprocating parts. This means there's no need for a heavy counterbalance.
    Air Cooling. Keeping an engine cool was an ongoing challenge for early engine designers. Many resorted to heavy water cooling systems. Air cooling was quite adequate on rotary engines, since the cylinders are always in motion.
    No flywheel. The crankcase and cylinders provided more than adequate momentum to smooth out the power pulses, eliminating the need for a heavy flywheel.
    All these factors gave rotary engines the best power-to-weight ratio of any configuration at the time, making them ideal for use in fighter planes. Of course, there were disadvantages as well:
    Gyroscopic effect. A heavy spinning object resists efforts to disturb its orientation (A toy gyroscope demonstrates the effect nicely). This made the aircraft difficult to maneuver.
    Total Loss Oil system. Centrifugal force throws lubricating oil out after its first trip through the engine. It was usually castor oil that could be readily combined with the fuel. (The romantic-looking scarf the pilot wore was actually a towel used to wipe the slimy stuff off his goggles!)
    The aircraft's range was thus limited by the amount of oil it could carry as well as fuel. Most conventional engines continuously re-circulate a relatively small supply of oil.
    اللهم أرنا الحق ,,, حقا ,,,, و أرزقنا اتباعه ,,,,
    و أرنا الباطل ,,, باطلا ,,,, و
    ارزقنا اجتنابه


  7. #17
    مشرف قسم تقنية الطيران وعلوم الفضاء
    تاريخ التسجيل
    May 2007
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    افتراضي

    اقتباس المشاركة الأصلية كتبت بواسطة شبلي موعد مشاهدة المشاركة
    بارك الله فيك يا أبو أيوي على المعلومات عن المحركات
    وإذا أمكنك مع الوقت أن تتوسع في المحركات النفاثة لكن بشكل مبسط فحيهلا
    شكرا يا شبلي علي التشجيع ,,,,, و يبدو ان اهتمامك بالطيران ,,,, سيطغي قريبا ,,,, علي ,,, الطوب و الزلط ,,,و الخرسانه و الاسمنت ,,,

    مع اطيب التحيات ,,,, :)
    اللهم أرنا الحق ,,, حقا ,,,, و أرزقنا اتباعه ,,,,
    و أرنا الباطل ,,, باطلا ,,,, و
    ارزقنا اجتنابه


  8. #18
    مشرف قسم تقنية الطيران وعلوم الفضاء
    تاريخ التسجيل
    May 2007
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    افتراضي

    بصراحه الموضوع كله جميل ,,,, و رائع ,,,, و مفيد

    و لكن اجمل ما في الموضوع ,,, المحرك الصغير "خلود فهد الرفاعي"

    تحياتي العطرة
    اللهم أرنا الحق ,,, حقا ,,,, و أرزقنا اتباعه ,,,,
    و أرنا الباطل ,,, باطلا ,,,, و
    ارزقنا اجتنابه


  9. #19
    مشرف قسم تقنيةالميكانيكا العام الصورة الرمزية مهند الدهش
    تاريخ التسجيل
    Nov 2006
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    افتراضي

    السلام عليكم و رحمة الله و بركاته

    اتقدم بشكري للاخ الزميل فارس مسلم لهذه المواضيع القيمة و المفيدة
    بارك الله فيك و بجهودك
    وقل ربي زدني علما

  10. #20
    مشرف قسم تقنية الطيران وعلوم الفضاء
    تاريخ التسجيل
    May 2007
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    افتراضي

    الاخ و الزميل مهند الدهش ,,,,,,

    مرورك يشرفنا ,,,
    اللهم أرنا الحق ,,, حقا ,,,, و أرزقنا اتباعه ,,,,
    و أرنا الباطل ,,, باطلا ,,,, و
    ارزقنا اجتنابه


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