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    • 1. 发明申请
    • METHOD OF PRODUCING A YOGHURT-BASED PRODUCT
    • 生产基于YOGHURT的产品的方法
    • WO2010147530A1
    • 2010-12-23
    • PCT/SE2010/000139
    • 2010-05-24
    • TETRA LAVAL HOLDINGS & FINANCE S.A.NILSSON, Lars-Ebbe
    • NILSSON, Lars-Ebbe
    • A23C9/127
    • A23C3/0332A23C3/02A23C9/123
    • The invention relates to a method of producing a yoghurt-based product. The milk raw material is pre-treated normally by pasteurization, de-aeration, homogenization and possible dry matter adjustment. A stabilizer and possible flavourings are also added. A first bacteria culture is added to the milk raw material and the milk raw material is held at a temperature of 37-45°C during an incubation period. Thereafter, the product is heat treated at a temperature of 75-110°C during a predetermined period of time. Thereafter, a second bacteria culture is added to the heat treated, yoghurt-based product. The second bacteria culture must be of the type which is not active below a given pH. The finished product is packed aseptically.
    • 本发明涉及一种生产基于酸奶的产品的方法。 通过巴氏消毒,除气,均质化和可能的干物质调整来对牛奶原料进行预处理。 还加入稳定剂和可能的调味剂。 在牛奶原料中加入第一细菌培养物,在孵育期间将奶原料保持在37-45℃的温度。 此后,在预定的时间内,将产物在75-110℃的温度下热处理。 此后,将第二细菌培养物加入到经热处理的基于酸奶的产品中。 第二种细菌培养物必须是低于给定pH值的活性物质。 成品无菌包装。
    • 2. 发明申请
    • METHOD AND DEVICE FOR A MULTIPLE STEP ROCKET
    • 用于多个步骤的方法和装置
    • WO0236955A8
    • 2005-11-10
    • PCT/SE0102381
    • 2001-10-30
    • SAAB ABNILSSON LARSAX LARS
    • NILSSON LARSAX LARS
    • F02K9/08F02K9/32F02K9/70F02K9/76F02K9/95F02K9/97F42B15/36
    • F42B15/36F02K9/08F02K9/32F02K9/70F02K9/76F02K9/763F02K9/95F02K9/978
    • The present invention relates to a method and an arrangement for, in multi-stage rockets (3) provided with a number of successively ignitable rocket engines (7, 13) arranged one in front of another in the flying direction of the rocket and joined together detachably with one another, each following rocket engine (13) in the ignition sequence depending, for its ignition, on being initiated after a preceding rocket engine (7) has been able to bun out, causing each preceding rocket engine (7) included in the ignition sequence to be jettisoned by virtue of the next engine having reached its working pressure. According to the invention, each preceding rocket engine is designed with a preferably conical guide part (11) which is directed forwards in the flying direction of the rocket and geometrically adapted to the exhaust nozzle (12) of the following rocket engine (13) and which, in the initial position, is fitted into said exhaust nozzle (12) and fixed in this position by means of at least one blocking part (15) which is deformable or capable of elastic recovery.
    • 本发明涉及一种多级火箭(3)中的方法和装置,该多级火箭(3)具有在火箭的飞行方向上一个在另一个前方排列并连接在一起的若干连续可点燃的火箭发动机(7,13) 每个随后的火箭发动机(13)在点火顺序中依赖于其点火,在先前的火箭发动机(7)能够蹦出之后被启动,使得每个先前的火箭发动机(7)包括在 由于下一个发动机已经达到其工作压力而要排出的点火顺序。 根据本发明,每个先前的火箭发动机被设计成具有优选的圆锥形引导部分(11),其沿着火箭的飞行方向向前指向并几何地适应于随后的火箭发动机(13)的排气喷嘴(12)和 其在初始位置被装配到所述排气喷嘴(12)中并且通过至少一个可变形或能够弹性恢复的阻挡部分(15)固定在该位置。
    • 9. 发明申请
    • DEVICE FOR DRAWING THROUGH ELECTRIC LEADS TO CUBICLES OR CASINGS FOR ELECTRIC EQUIPMENT
    • 通过电气引线到电气设备的箱体或箱子上的装置
    • WO1989007851A1
    • 1989-08-24
    • PCT/SE1989000064
    • 1989-02-15
    • NILSSON, Lars-GöstaNILSSON, Bo, Anders
    • H02G03/22
    • H02G3/083
    • A device for drawing through electric leads to cubicles or casings (3) for electric equipment includes a lead-through member (9) with lead-through and sealing portions (10) which are disposed beside each other and which are made of elastic material and workable to adapt as sealing collars (10') to electric leads (2') extending therethrough, whereby the lead-through and sealing portion (10) of the lead-through member (9) as well as connecting portions (11) forming part of the lead-through member (9) and connecting the lead-through and sealing portions (10) to each other are provided in one piece and made of the same elastic material. In order for the lead-through and sealing portions (10) to adapt to and sealingly engage an electric lead, the thicknessof which is substantially equal to or substantially less than the width of the lead-through and sealing portion, and adapt to and sealingly engage electric leads of various cross-sectional shape and in order for the device to be brought to adapt to and sealingly engage the outer side of the cubicle or casing (3) onto which it shall be fastened, said elastic material has a hardness of 70-95 Shore A.
    • 用于通过电引线到电气设备的隔间或壳体(3)的装置包括具有穿过和密封部分(10)的引导构件(9),它们彼此相邻设置并且由弹性材料制成, 可作为密封套(10')适应于延伸穿过其中的电引线(2'),由此引导件(9)的引出和密封部分(10)以及连接部分(11)形成部分 的引导部件(9)并且将引导和密封部分(10)彼此连接,并且由相同的弹性材料制成。 为了使引线和密封部分(10)适应并密封地接合电引线,该电引线的厚度基本上等于或基本上小于引出和密封部分的宽度,并适应和密封 接合各种横截面形状的电引线,并且为了使装置适应并密封地接合在其上应紧固在其上的隔间或外壳(3)的外侧,所述弹性材料具有70的硬度 -95岸A.