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    • 1. 发明公开
    • SPLIT-CYCLE AIRCRAFT ENGINE
    • 对于共享CYCLE飞机发动机
    • EP2061951A2
    • 2009-05-27
    • EP07837818.9
    • 2007-09-04
    • The Scuderi Group, LLC
    • HEATON, Clifford, D.
    • F01B7/12
    • F01B17/025B64D27/24B64D2027/026F02B59/00F02B69/00Y02T50/44Y02T50/64
    • A split -cycle aircraft engine includes a crankshaft rotatable about a crankshaft axis. A power piston is slidably received within a power cylinder and is operatively connected to the crankshaft such that the power piston reciprocates through an expansion stroke and an exhaust stroke during a single rotation of the crankshaft. A compression piston is slidably received within a compression cylinder and is operatively connected to the crankshaft such that the compression piston reciprocates through an intake stroke and a compression stroke during a single, rotation of the crankshaft. A gas crossover passage operatively interconnects the compression cylinder and the power cylinder. An air reservoir is operatively connected to the gas crossover passage by a reservoir passage. The air reservoir is selectively operable to receive and deliver compressed air. The engine is mounted to an aircraft and the air reservoir is disposed within the aircraft.A split -cycle aircraft engine includes a crankshaft rotatable about a crankshaft axis. A power piston is slidably received within a power cylinder and is operatively connected to the crankshaft such that the power piston reciprocates through an expansion stroke and an exhaust stroke during a single rotation of the crankshaft. A compression piston is slidably received within a compression cylinder and is operatively connected to the crankshaft such that the compression piston reciprocates through an intake stroke and a compression stroke during a single, rotation of the crankshaft. A gas crossover passage operatively interconnects the compression cylinder and the power cylinder. An air reservoir is operatively connected to the gas crossover passage by a reservoir passage. The air reservoir is selectively operable to receive and deliver compressed air. The engine is mounted to an aircraft and the air reservoir is disposed within the aircraft.A split -cycle aircraft engine includes a crankshaft rotatable about a crankshaft axis. A power piston is slidably received within a power cylinder and is operatively connected to the crankshaft such that the power piston reciprocates through an expansion stroke and an exhaust stroke during a single rotation of the crankshaft. A compression piston is slidably received within a compression cylinder and is operatively connected to the crankshaft such that the compression piston reciprocates through an intake stroke and a compression stroke during a single, rotation of the crankshaft. A gas crossover passage operatively interconnects the compression cylinder and the power cylinder. An air reservoir is operatively connected to the gas crossover passage by a reservoir passage. The air reservoir is selectively operable to receive and deliver compressed air. The engine is mounted to an aircraft and the air reservoir is disposed within the aircraft.
    • 2. 发明公开
    • MODIFIED OTTO ENGINE WITH ONE CYLINDER
    • 与气缸改进汽油发动机
    • EP1383994A1
    • 2004-01-28
    • EP02703025.3
    • 2002-03-12
    • GE-TOP Aktiebolag
    • ERIKSSON, Göran
    • F02B75/04
    • F02B69/00F02B75/044F02D15/04
    • The present invention relates to a method for modifying a petrol-driven, single-cylinder Otto engine, which engine comprises an engine block (1) with a cylinder (2), a cylinder head (3), a piston (4) disposed movably inside the cylinder, two valves (5, 5') arranged by the cylinder, a carburettor (6) with a fuel nozzle (7) and an air filter arrangement (8). The invention is characterized in that the method comprises measuring the existing mimimum play (S1) between the end (5A) of the valve in its extreme position in the open state and the surface (4A; 3A) that faces said end (5A) of the valve, removal of the cylinder head (3), machining of the cylinder head (3), its surface (3B) facing the engine block (1) being cut and levellled by 40-100 % of the existing minimum play (S1) to obtain a considerably smaller modified play (S2) between said valve end (5A) and said opposing surface (4A; 3A), checking that said modified play (S2) does not fall below a certain set value (SB), fitting of the cylinder head (3) and adjustment of the fuel/air admixture so that an increase in the fuel flow in relation to the air flow is achieved, following which the engine has been modified for operation by means of a fuel containing mainly ethanol.
    • 9. 发明公开
    • An engine and a method for producing the engine
    • Brennkraftmaschine und Verfahren zur Herstellung
    • EP1447542A1
    • 2004-08-18
    • EP03003715.4
    • 2003-02-19
    • Kubota Corporation
    • Aketa, MasahiroIwanaga, WataruUmeda, Yuzo
    • F02B63/06F02B69/00F01B1/12F02B75/20F02M39/00F02M63/02F02F7/00
    • F02B67/04F01B1/12F02B3/06F02B63/06F02B69/00F02B75/20F02B2075/1816F02F7/0043F02F7/0073F02M39/00
    • The present invention relates to an engine and a method for producing the engine.
      The engine is constructed as follows.
      The engine interlockingly operates a pump (39, 139) for feeding fuel under pressure, by power of a crank shaft (1). A pair of gears (32a) and (32b) are arranged to be attached to a gear attaching shaft (32). The paired gears (32a) and (32b) are attached to the gear attaching shaft (32). At least one gear (32a) of the paired gears (32a) and (32b) constitutes a gear train (14, 114) through which the power of the crank shaft (1) is transmitted to the pump (39, 139).
      The method for producing the engine is constructed as follows.
      The method uses a common part for each of the gear trains (14) and (114) so as to produce engines of an injection pump specification and a common rail .specification and alternatively manufactures the gear trains (14) and (114) through the common part. It comprises attaching a pair of gears (32a) and (32b) to a gear attaching shaft (32) of the engine of every specification, making one gear (32a) of the paired gears (32a) and (32b) serve as a basic gear and the other gear (32b) serve as a second gear, employing the basic gear (32a) as the common part for each of the gear trains (14) and (114) and alternatively manufactures the gear trains (14) and (114) of the engines of the respective specifications through the basic gear (32a) of the common part.
    • 发动机及其制造方法技术领域本发明涉及发动机及其制造方法。 发动机的构造如下。 发动机联动地操作用于通过曲轴(1)的动力在压力下供给燃料的泵(39,139)。 一对齿轮(32a)和(32b)被布置成附接到齿轮连接轴(32)。 成对的齿轮(32a)和(32b)附接到齿轮连接轴(32)。 一对齿轮(32a)和(32b)中的至少一个齿轮(32a)构成齿轮系(14,114),曲轴(1)的动力通过该齿轮系传递到泵(39,139)。 发动机的制造方法如下构成。 该方法为每个齿轮系(14)和(114)使用公共部件,以便产生喷射泵规格和共轨的发动机,并且可替代地制造齿轮系(14)和( 114)通过公共部分。 它包括将一对齿轮(32a)和(32b)连接到每个规格的发动机的齿轮连接轴(32)上,使得一对齿轮(32a)和(32b)的一个齿轮(32a)用作基本 齿轮和另一个齿轮(32b)用作第二齿轮,使用基本齿轮(32a)作为每个齿轮系(14)和(114)的公共部分,并且可替代地制造齿轮系(14)和(114 )通过公共部分的基本齿轮(32a)的相应规格的发动机。