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    • 2. 发明授权
    • Internal combustion engine with air reservoir
    • 内燃机带气库
    • US4103648A
    • 1978-08-01
    • US730321
    • 1976-10-07
    • Philippe Jarry
    • Philippe Jarry
    • F02B23/00F02B21/00F02B29/06F02B41/00
    • F02B21/00F02B2275/14Y02T10/123
    • Disclosed is an internal combustion engine having a reservoir in communication through a passage with the combustion chamber. A valve is provided in the passage to enable the reservoir, when the valve is open, to receive a fraction of the air during the compression stage of the engine cycle. The valve closes in response to a decrease in pressure in the combustion chamber. The valve is automatically controlled to open at the beginning of the next compression stage to inject heated air into the combustion chamber. The valve then remains open to enable the reservoir to receive a fraction of air from the cylinder during its high pressure cycle for restitution to the cylinder chamber at the beginning of the next compression stage.
    • 公开了一种内燃机,其具有通过与燃烧室的通道连通的储存器。 在通道中设置有一个阀门,以在阀门打开时能够使储存器在发动机循环的压缩阶段期间接收一部分空气。 响应于燃烧室中的压力降低,阀关闭。 阀门在下一个压缩阶段开始时自动控制打开以将加热的空气注入燃烧室。 然后阀门保持打开,以使储存器在其高压循环期间从气缸接收一部分空气,以在下一个压缩阶段开始时恢复到气缸室。
    • 4. 发明申请
    • MANUFACTURING METHOD OF MAKING ALUMINUM ALLOY SEMI-FINISHED PRODUCT WITH IMPROVED MICROPOROSITY
    • 制备具有改善的微孔的铝合金半成品的制造方法
    • US20120237395A1
    • 2012-09-20
    • US13398691
    • 2012-02-16
    • Philippe JARRY
    • Philippe JARRY
    • B22D11/124B22D11/00C22C21/00B22D27/02
    • C22C21/00B22D1/00C22B9/026C22B21/06C22F1/04Y02P10/234
    • The invention relates to a manufacturing method for making an unwrought semi-finished product having at mid thickness a density of micropores of size greater than 90 μm less than 50% and preferably less than 20% of the density of micropores of size greater than 90 μm obtained by a method according to prior art. The method according to the invention comprises in particular an ultrasound treatment step for the molten metal bath in a furnace and/or a vessel using an immersed device comprising at least one ultrasound transmitter. The semi-finished products obtained according to the method of the invention are particularly advantageous for manufacturing by rolling sheets designed for the aircraft industry to produce spars, ribs, upper and lower wing skins and for manufacturing by extrusion sections designed for the aircraft industry to produce stiffeners.
    • 本发明涉及一种用于制造中等厚度的未加工半成品的制造方法,其中微孔的尺寸大于90μm的密度小于尺寸大于90μm的微孔的密度的50%,优选小于20% 通过现有技术的方法获得。 根据本发明的方法特别地包括使用包括至少一个超声波发射器的浸没装置的熔炉和/或容器中的熔融金属浴的超声处理步骤。 根据本发明的方法获得的半成品特别有利于通过设计用于飞机工业的轧制板来制造产生翼梁,肋骨,上部和下部翼皮以及通过设计用于飞机工业的挤压部分来生产 扶强材。
    • 6. 发明申请
    • ALUMINUM ALLOY PRODUCTS WITH HIGH TOUGHNESS AND PRODUCTION PROCESS THEREOF
    • 具有高韧性和生产工艺的铝合金产品
    • US20100006186A1
    • 2010-01-14
    • US12563698
    • 2009-09-21
    • Bernard BésPhilippe Jarry
    • Bernard BésPhilippe Jarry
    • C22C21/14B32B15/00C22C21/16
    • C22C1/06C22B21/06C22B21/062C22C1/02C22C1/026C22C21/02C22C21/08C22C21/14C22C21/16C22C21/18C22F1/04
    • Process for manufacturing aluminium alloy products, with high toughness and fatigue resistance comprising: (a) preparing an aluminium alloy bath, (b) adding a refining agent containing particles of AlTiC type phases into the bath, (c) casting an as-cast form such as an extrusion ingot, a forging ingot or a rolling ingot, (d) hot transforming the as-cast form, possibly after scalping, to form a blank or a product with final thickness, (e) optionally cold transforming the blank to a final thickness, (f) applying a solution heat treatment and quenching the product output from (d) or (e), followed by relaxation by controlled stretching with permanent elongation between 0.5 and 5%, and optionally annealing, wherein the quantity of refining agent is chosen such that the average casting grain size of the as-cast form is more than 500 μm. The present invention may be used, for example, to manufacture fuselage sheet or light-gauge plates made with 6056 alloy.
    • 具有高韧性和耐疲劳性的铝合金制品的制造方法包括:(a)制备铝合金浴,(b)将含有AlTiC型相的颗粒的澄清剂加入到所述槽中,(c)铸造铸态 例如挤出锭,锻造锭或轧制锭,(d)可能在烫印之后热成型铸塑形式以形成具有最终厚度的坯料或产品,(e)可选地将坯料变冷至 最终厚度,(f)施加固溶热处理并淬火(d)或(e)的产物,然后通过控制拉伸松弛,永久伸长率在0.5%至5%之间,任选地退火,其中精炼剂量 被选择为使得铸态形式的平均铸造晶粒尺寸大于500μm。 本发明可以用于例如制造用6056合金制成的机身板或轻量板。
    • 7. 发明授权
    • Aluminum alloy products with high toughness and production process thereof
    • 具有高韧性和生产工艺的铝合金产品
    • US07615125B2
    • 2009-11-10
    • US11232934
    • 2005-09-23
    • Bernard BésPhilippe Jarry
    • Bernard BésPhilippe Jarry
    • C22F1/05C22F1/047
    • C22C1/06C22B21/06C22B21/062C22C1/02C22C1/026C22C21/02C22C21/08C22C21/14C22C21/16C22C21/18C22F1/04
    • Process for manufacturing aluminum alloy products, with high toughness and fatigue resistance comprising: (a) preparing an aluminum alloy bath, (b) adding a refining agent containing particles of AlTiC type phases into the bath, (c) casting an as-cast form such as an extrusion ingot, a forging ingot or a rolling ingot, (d) hot transforming the as-cast form, possibly after scalping, to form a blank or a product with final thickness, (e) optionally cold transforming the blank to a final thickness, (f) applying a solution heat treatment and quenching the product output from (d) or (e), followed by relaxation by controlled stretching with permanent elongation between 0.5 and 5%, and optionally annealing, wherein the quantity of refining agent is chosen such that the average casting grain size of the as-cast form is more than 500 μm. The present invention may be used, for example, to manufacture fuselage sheet or light-gauge plates made with 6056 alloy.
    • 具有高韧性和耐疲劳性的铝合金制品的制造方法包括:(a)制备铝合金浴,(b)将含有AlTiC型相的颗粒的澄清剂加入到所述槽中,(c)铸造铸态 例如挤出锭,锻造锭或轧制锭,(d)可能在烫印之后热成型铸造形式,以形成具有最终厚度的坯料或产品,(e)可选地将坯料变冷至 最终厚度,(f)施加固溶热处理并淬火(d)或(e)的产物,然后通过控制拉伸松弛,永久伸长率在0.5%至5%之间,任选地退火,其中精炼剂量 被选择为使得铸态形式的平均铸造晶粒尺寸大于500μm。 本发明可以用于例如制造用6056合金制成的机身板或轻量板。
    • 10. 发明授权
    • Method of manufacturing an infrared-sensitive charge coupled device
    • 制造红外线敏感电荷耦合器件的方法
    • US4749659A
    • 1988-06-07
    • US20065
    • 1987-02-27
    • Philippe Jarry
    • Philippe Jarry
    • H01L29/762H01L21/306H01L21/339H01L27/148H01L29/76H01L29/765H01L29/768H01L29/772H01L21/208
    • H01L21/30612H01L27/14875H01L29/765H01L29/768Y10S438/977
    • A charge coupled device (CCD) sensitive to infrared radiation composed of a succession of three layers of Group III-V semiconductor material. The layers are a window layer, a sensitive layer and a storage layer. The layers are fixed to a supporting plate serving as input for the radiation and as a rear surface of the device. The front surface of the device supports a plurality of control electrodes and at least one output electrode.The window layer and the storage layer of the CCD are made of a binary compound AB. The sensitive layer is made of an n-ary compound (A,X,Y . . . ).sub.III (B,M,N . . . ).sub.V having a larger forbidden energy band and a smaller absorption limit wavelength than the window and storage layers.The three layers of the device are formed by epitaxial growth on a substrate. The substrate is a layer of the binary compound AB coated with an epitaxial layer of the n-ary compound. The epitaxial substrate layer is a chemical blocking layer. The substrate and the chemical blocking layer are subsequently removed chemically.
    • 对由三层III-V族III族半导体材料组成的红外辐射敏感的电荷耦合器件(CCD)。 层是窗口层,敏感层和存储层。 这些层被固定到用作辐射的输入的支撑板和作为装置的后表面。 器件的前表面支撑多个控制电极和至少一个输出电极。 CCD的窗口层和存储层由二元化合物AB制成。 敏感层由具有比窗口和存储器更大的禁带能量和更小的吸收极限波长的正构化合物(A,X,Y ...)III(B,M,N ...)V 层。 器件的三层通过在衬底上外延生长而形成。 衬底是涂覆有正构化合物的外延层的二元化合物AB的层。 外延衬底层是化学阻挡层。 随后基板和化学阻挡层被化学去除。