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1. 发明专利

JP2011052074A Fuel oil base and aviation fuel composition containing the same 有权
标题翻译：燃油基础和航空燃料组合物
公开(公告)号：JP2011052074A
公开(公告)日：2011-03-17
申请号：JP2009200777
申请日：2009-08-31
申请人： Jx Nippon Oil & Energy Corp , Jx日鉱日石エネルギー株式会社
发明人： IGUCHI YASUTOSHI , ONO HIDEKI , KOYAMA SHIGERU
IPC分类号： C10L1/04 , C10G3/00
CPC分类号： C10G3/50 , C10G3/46 , C10G3/49 , C10G45/58 , C10G65/043 , C10G2300/1014 , C10G2300/1018 , C10G2300/202 , C10G2300/30 , C10G2300/301 , C10G2300/4018 , C10G2300/80 , C10G2400/08 , C10L1/04 , C10L2200/043 , C10L2200/0461 , C10L2270/04 , C10L2290/10 , Y02P30/10 , Y02P30/20
摘要： PROBLEM TO BE SOLVED: To provide a fuel oil base useful for producing an aviation fuel composition which is excellent in a life cycle CO 2 discharge characteristic and oxidation stability and is also excellent in low-temperature flowability. SOLUTION: The aviation fuel oil base, which is obtained by hydrogenating an oil to be processed that contains an oxygen-containing hydrocarbon compound derived from an animal/plant oil or fat and a sulfur-containing hydrocarbon compound, and then subjecting the resulting oil to a hydrogenation isomerization treatment includes: a yield of the distillate fraction having a boiling range of 140-300°C of not less than 70 mass%; an isoparaffin content of not less than 80 mass%; a di- or higher branched isoparaffin content of not less than 17 mass%; an aromatic content of less than 0.1 vol.%; an olefin content of less than 0.1 vol.%; a sulfur content of less than 1 mass ppm; and an oxygen content of less than 0.1 mass%. COPYRIGHT: (C)2011,JPO&INPIT
摘要翻译：要解决的问题：提供一种用于制造寿命周期CO 2 放电特性和氧化稳定性优异的航空燃料组合物的燃料油基料，并且在低温下也是优异的流动性。解决方案：通过将含有来自动植物油或脂肪的含氧烃化合物和含硫烃化合物的待处理油进行氢化而得到的航空燃油基料，得到的油进行氢化异构化处理包括：沸点范围为140-300℃的馏出物馏分的产率不小于70质量％; 异构烷烃含量为80质量％以上; 二支或更多支链异构烷烃含量不小于17质量％; 芳族含量小于0.1体积％; 烯烃含量小于0.1体积％; 硫含量小于1质量ppm; 氧含量小于0.1质量％。版权所有（C）2011，JPO＆INPIT

2. 发明专利

JP2011052082A Method for producing aviation fuel oil base material and aviation fuel oil composition 有权
标题翻译：制造航空燃料油基材料和航空燃料油组合物的方法
公开(公告)号：JP2011052082A
公开(公告)日：2011-03-17
申请号：JP2009201023
申请日：2009-08-31
申请人： Jx Nippon Oil & Energy Corp , Jx日鉱日石エネルギー株式会社
发明人： ONO HIDEKI , KOYAMA SHIGERU , IKI SUGURU
IPC分类号： C10G65/04 , B01J23/42 , B01J27/19 , C10G3/00 , C10G45/08 , C10G45/10 , C10G45/12 , C10L1/04
CPC分类号： Y02P30/20
摘要： PROBLEM TO BE SOLVED: To provide a method for producing an aviation fuel oil base material originating from an animal and vegetable oil which has a high yield of the aviation fuel oil base material and exhibits excellent low temperature performance. SOLUTION: The method for producing the aviation fuel oil base material includes: a first step of hydrogenating raw oil containing a mixture of two or more kinds of animal and vegetable oil having different fatty acid composition and a sulfur-containing hydrocarbon compound in the presence of hydrogen; and a second step of hydroisomerizing the hydrogenated oil obtained in the first step in the presence of hydrogen. In the mixture of the animal and vegetable oil, the total content of each fatty acid composition having a 9-15C fatty acid carbon chain is 50-70 mass% and the ratio of respective fatty aid compositions having a 11C, a 13C and 15C fatty acid carbon chain is 10-60 when total content of fatty acid composition having a 9-15C fatty acid carbon chain is defined as 100. COPYRIGHT: (C)2011,JPO&INPIT
摘要翻译：解决问题的方案：提供一种具有优异的低温性能的具有高产率的动植物油的航空燃料油基材的制造方法。解决方案：用于制造航空燃料油基材的方法包括：将含有两种或更多种具有不同脂肪酸组成的动植物油的混合物的原油和含硫烃化合物氢化的第一步骤氢的存在; 以及在氢存在下将第一步骤中获得的氢化油加氢异构化的第二步骤。在动植物油的混合物中，具有9-15C脂肪酸碳链的各脂肪酸组合物的总含量为50-70质量％，各脂肪族助剂组合物的比例为11℃，13℃，15℃脂肪当具有9-15C脂肪酸碳链的脂肪酸组合物的总含量定义为100时，酸性碳链为10-60。版权所有（C）2011，JPO＆INPIT

3. 发明专利

JP2013199595A Lubricant composition for internal combustion engine 有权
标题翻译：内燃机用润滑剂组合物
公开(公告)号：JP2013199595A
公开(公告)日：2013-10-03
申请号：JP2012069012
申请日：2012-03-26
申请人： Jx Nippon Oil & Energy Corp , Jx日鉱日石エネルギー株式会社
发明人： KOYAMA SHIGERU
IPC分类号： C10M169/04 , C10M101/02 , C10M133/04 , C10M133/16 , C10M133/56 , C10M137/04 , C10M137/06 , C10M137/08 , C10M145/14 , C10M159/22 , C10N10/12 , C10N20/00 , C10N20/02 , C10N30/00 , C10N30/04 , C10N30/10
摘要： PROBLEM TO BE SOLVED: To provide a lubricant composition for an internal combustion engine that can achieve antioxidation, a base value retention property, high temperature cleanability, caulking resistance and NOx resistance at high-level and by favorable balance.SOLUTION: A lubricant composition for an internal combustion engine includes: a lubricant base oil (A) in which an aromatic content is 10-50 mass%, and an NOACK evaporation mass is at most 10% by mass; 0.01-0.1 mass% of at least one phosphorus compound (B) chosen from a group consisting of an organophosphorus compound not containing sulfur, a metal salt thereof and an amine salt thereof, and a derivative thereof by 0.01-0.1 mass% as a phosphorus amount based on the total amount of the composition; and an organic molybdenum compound (C) by 0.005-0.1 mass% as a molybdenum amount based on the total amount of the composition.
摘要翻译：要解决的问题：提供一种内部发动机的润滑剂组合物，其可以实现高水平和平衡地获得抗氧化，碱值保持性，耐高温清洁性，耐铆接性和耐NOx性。内燃机包括：芳烃含量为10〜50质量％，NOACK蒸发量为10质量％以下的润滑油基础油（A） 0.01-0.1质量％的选自由不含硫的有机磷化合物，其金属盐和胺盐组成的组中的至少一种磷化合物（B）及其衍生物，以0.01〜0.1质量％的磷基于组合物总量的量; 和作为钼量的有机钼化合物（C），以组合物总量计为0.005〜0.1质量％。

4. 发明专利

JP2011052068A Aviation fuel oil composition 有权
标题翻译：航空燃油组合物
公开(公告)号：JP2011052068A
公开(公告)日：2011-03-17
申请号：JP2009200695
申请日：2009-08-31
申请人： Jx Nippon Oil & Energy Corp , Jx日鉱日石エネルギー株式会社
发明人： KOYAMA SHIGERU
IPC分类号： C10L1/04 , C10G45/08 , C10G45/10 , C10G65/04
CPC分类号： C10G3/50 , B01J21/12 , B01J23/38 , B01J23/42 , B01J23/70 , B01J27/19 , B01J29/064 , B01J35/023 , B01J37/0009 , B01J37/0201 , C10G3/46 , C10G3/48 , C10G3/49 , C10G45/02 , C10G45/58 , C10G65/043 , C10G2300/1014 , C10G2300/1018 , C10G2300/1033 , C10G2300/202 , C10G2300/301 , C10G2300/308 , C10G2300/4018 , C10G2300/80 , C10G2400/08 , C10L1/04 , C10L1/19 , C10L1/2235 , C10L1/2283 , C10L2200/0407 , C10L2200/043 , C10L2230/22 , C10L2270/04 , Y02P30/10 , Y02P30/20
摘要： PROBLEM TO BE SOLVED: To provide an aviation fuel oil composition that is excellent in life cycle characteristics and achieves excellent fuel consumption rate. SOLUTION: The aviation fuel oil composition comprises: a first base, which is a distillate fraction having a boiling range of 140-280°C, and which is obtained via a step of conducting a hydrogenation treatment of a first raw material oil that contains a sulfur-containing hydrocarbon compound and an oxygen-containing hydrocarbon compound derived from an animal/plant oil or fat or, alternatively, a second raw material oil that is a mixture of the first raw material oil and a petroleum base obtained by refining crude oil; and a second base, which is a distillate fraction having a boiling range of 140-280°C, and which is obtained from a heavy oil cracking apparatus. COPYRIGHT: (C)2011,JPO&INPIT
摘要翻译：要解决的问题：提供一种寿命周期特性优异，燃料消耗率优异的航空燃料油组合物。解决方案：航空燃料油组合物包括：第一碱，其是沸程为140-280℃的馏出物馏分，其通过对第一原料油进行氢化处理的步骤获得其包含来自动植物油或脂肪的含硫烃化合物和含氧烃化合物，或者作为第一原料油和通过精制获得的石油基质的混合物的第二原料油原油; 和第二碱，其为沸程为140-280℃的馏出物馏分，其由重油裂化装置获得。版权所有（C）2011，JPO＆INPIT

5. 发明专利

JP2012201807A Lubricant composition 有权
标题翻译：润滑剂组合物
公开(公告)号：JP2012201807A
公开(公告)日：2012-10-22
申请号：JP2011068068
申请日：2011-03-25
申请人： Jx Nippon Oil & Energy Corp , Jx日鉱日石エネルギー株式会社
发明人： KOYAMA SHIGERU
IPC分类号： C10M169/04 , C10M101/02 , C10M129/18 , C10M129/54 , C10M137/02 , C10M137/04 , C10M137/06 , C10M137/08 , C10M137/10 , C10M139/00 , C10M159/22 , C10N10/12 , C10N20/02 , C10N30/00 , C10N30/04 , C10N40/04 , C10N40/08 , C10N40/12 , C10N40/25 , C10N40/30
摘要： PROBLEM TO BE SOLVED: To provide a lubricant composition suitable when a lead-containing metallic material is used in a sliding part.SOLUTION: The lubricant composition is obtained by incorporating, in a lubricant base oil (A): at least one kind of phosphorus compound (B), which is selected from the group comprising the phosphorus compounds shown by general formula (1) and/or general formula (2), metal salts of them, amine salts of them and derivatives of them by 0.01-0.1 mass% in terms of a phosphorus amount; and 0.05-1.0 mass% of an epoxy compound (C). In the general formula (1): X, Xand Xare each an oxygen atom or a sulfur atom individually on condition that at least one of them is oxygen; R, Rand Rare each a hydrogen atom or a 1C-30C hydrocarbon group individually. In the general formula (2): X, X, Xand Xare each an oxygen atom or a sulfur atom individually on condition that at least one of them is oxygen and one or two of X, Xand Xmay be single bonds or (poly)oxyalkylene groups; R, Rand Rare each a hydrogen atom or a 1C-30C hydrocarbon group individually.
摘要翻译：要解决的问题：提供一种当在滑动部分中使用含铅金属材料时适合的润滑剂组合物。解决方案：润滑剂组合物通过在润滑油基础油（A）中掺入：至少一种磷化合物（B），其由选自由通式（1）表示的磷化合物组成的组中，和/或通式（2），它们的金属盐，它们的胺盐和它们的衍生物以磷量计为0.01-0.1质量％; 和0.05〜1.0质量％的环氧化合物（C）。在通式（1）中：X 1 ，X 2 和X 3 < SP>各自为氧原子或硫原子，条件是其中至少一个为氧; R 1 ，R 2 和R 3 分别为氢原子或单独的1C-30C烃基。在通式（2）中：X 4 ，X 5 ，X 6 < 条件是它们中的至少一个是氧并且X 和X 7 分别是氧原子或硫原子， > 4 ，X 5 和X 6 可以是单键或（聚）氧化烯基团; R 4 ，R 5 和R 6 分别为氢原子或单独的1C-30C烃基。版权所有（C）2013，JPO＆INPIT

6. 发明专利

JP2011052077A Method for producing aviation fuel oil base and aviation fuel oil composition 有权
标题翻译：制造航空燃油油基和航空燃料油组合物的方法
公开(公告)号：JP2011052077A
公开(公告)日：2011-03-17
申请号：JP2009200918
申请日：2009-08-31
申请人： Jx Nippon Oil & Energy Corp , Jx日鉱日石エネルギー株式会社
发明人： HAYASAKA KAZUAKI , ONO HIDEKI , KOYAMA SHIGERU , IKI SUGURU
IPC分类号： C10G65/04 , B01J27/198 , B01J29/76 , C10G3/00 , C10G45/08 , C10G45/64 , C10G47/12 , C10L1/04
CPC分类号： B01J29/7484 , B01J23/85 , B01J23/883 , B01J29/7461 , B01J29/7492 , B01J29/85 , C10G3/46 , C10G3/49 , C10G3/50 , C10G45/64 , C10G2300/1014 , C10G2300/1018 , C10G2300/202 , C10G2400/08 , C10L1/04 , Y02P30/20
摘要： PROBLEM TO BE SOLVED: To provide a method for producing an aviation fuel oil base producing an aviation fuel oil base with a high yield, which is excellent in low-temperature characteristics while having excellent life cycle characteristics resulted from components of vegetable oil and animal fat origin contained. SOLUTION: The method for producing an aviation fuel oil base includes: a first step wherein a raw material oil containing an oxygen-containing hydrocarbon compound of vegetable oil and animal fat origin is brought into contact with a first bifunctional catalyst, which has dehydrogenation and hydrogenation functions and contains a group 6A metal and a group 8 metal of the periodic table and an amorphous solid acidic substance, in the co-presence of hydrogen, thereby hydrogenating the raw material oil and obtaining a first produced oil; and a second step wherein the first produced oil is brought into contact with a second bifunctional catalyst, which has dehydrogenation and hydrogenation functions and contains a group 8 metal of the periodic table and a crystalline solid acidic substance, in the co-presence of hydrogen, thereby hydrogenating and isomerizing the first produced oil and obtaining a second produced oil that contains an aviation fuel oil base. COPYRIGHT: (C)2011,JPO&INPIT
摘要翻译：解决问题的方案：提供一种生产航空燃料油基料的方法，其生产出具有优异的低温特性的航空燃料油基料，同时具有由植物油组分产生的优异的生命周期特性和动物脂肪来源。解决方案：用于生产航空燃料油基料的方法包括：第一步骤，其中将含有植物油和动物脂肪来源的含氧烃化合物的原料油与第一双功能催化剂接触，所述第一双功能催化剂具有脱氢和氢化功能，并且含有元素周期表中的6A族金属和第8族金属和无定形固体酸性物质，在氢气共存下，由此使原料油氢化并获得第一产生的油; 和第二步骤，其中第一产生的油与具有脱氢和氢化功能的第二双功能催化剂接触，并且在氢的共存下含有周期表的第8族金属和结晶固体酸性物质，从而使第一产生的油氢化和异构化并获得含有航空燃料油基料的第二产生的油。版权所有（C）2011，JPO＆INPIT

7. 发明专利

JP2019019154A 潤滑油組成物审中-公开
公开(公告)号：JP2019019154A
公开(公告)日：2019-02-07
申请号：JP2017135672
申请日：2017-07-11
申请人： JX NIPPON OIL & ENERGY CORP
发明人： TAGAWA KAZUO , KOYAMA SHIGERU , TAKAGI AKIRA
IPC分类号： C10M145/14 , C10M169/04
摘要：【課題】ポリ(メタ)アクリレート系粘度指数向上剤を含有し、向上した耐スラッジ性を有する潤滑油組成物の提供。【解決手段】潤滑油基油と、(A)式(1)で表される構造単位と、(B)式(1)で表わされる構造単位とを含み、式(3)で表されるパラメタaの値が0.12以下である、(メタ)アクリレート系重合体とを含む、潤滑油組成物。[R1はH又はメチル基;R2はC1〜4の直鎖/分岐鎖のアルキル基が構造単位(A)、R2はC16〜24の直鎖/分岐鎖のアルキル基が構造単位(B)]a=log(Mh(t1/2))−log(M(t))・・・・(3)(GPCより得るM(t)は分子量分布のピーク;Mh(t1/2)はM(t)の強度1/2の強度を与える分子量)【選択図】なし

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