序号 专利名 申请号 申请日 公开(公告)号 公开(公告)日 发明人
1 天然气压缩缸 CN201610511015.3 2016-07-04 CN105971851A 2016-09-28 陆波涛
发明公开了一种天然气压缩缸,包括:上缸筒、下缸筒、活塞杆和导向套,所述上缸筒、下缸筒分别与导向套之间通过法兰连接,所述活塞杆贯穿导向套,且活塞杆的两端分别设置有一个上活塞和一个下活塞,所述上活塞与上缸筒之间设置有密封圈,所述下活塞与下缸筒之间设置有密封圈;所述密封圈包括两个对称设置的挡圈和位于两个挡圈之间的密封圈本体,所述挡圈的截面呈竖直放置的拱桥型,所述密封圈本体的截面包括中间O型段、上长方形段和下长方形段,正好与挡圈相匹配。通过上述方式,本发明结构简单合理,活塞与筒壁之间密封性能好,保证天然气压缩顺利进行。
2 机油压 CN201610026238.0 2016-01-15 CN105673400A 2016-06-15 徐浩
一种机油压,它的浮力壳内安装有泵油壳、电磁线圈,电磁线圈在泵油壳的外面,泵油壳的下端固定在浮力壳内;出油固定在泵油壳的中心孔内,泵油壳内有弹簧和铁芯活塞,铁芯弹簧压在铁芯活塞上,密封板密封进油腔的进油通道,密封球或密封锥密封挤压腔的进油通道;铁芯活塞上端的限位孔内固定有分油限制板,铁芯活塞的内锥孔内安装有密封球或密封锥。机油压力泵的结构紧凑、外观简洁、适用,能够泵机油时漂浮在机油面上,沉淀在油底壳底部的金属销和沉淀物不进入机油泵内,能够随机油面的升高或降低而自动升高或下降。
3 一种无油单螺杆压缩机 CN201610236291.3 2016-04-18 CN105909520A 2016-08-31 不公告发明人
发明提供了一种无油单螺杆压缩机。目前公知的一种无油单螺杆压缩机,包括螺杆总成、星轮总成、气缸等,由于压缩机没有润滑油进行冷却,机体温度比较高,非金属材质的星轮很容易受热变形,导致使用寿命短。本发明采用金属材料制造星轮,克服了非金属材质星轮受热易变形的缺点,延长压缩机的使用寿命;并且金属材料的加工性能好,提高了星轮的加工精度和表面粗糙度,使螺杆和星轮的间隙控制在0.05?01mm之间,提高压缩机的容积效率。
4 直压排污环保设备 CN201610026526.6 2016-01-16 CN105697263A 2016-06-22 徐三钟
一种直压排污环保设备,属于排污领域,它的浮壳内安装有上磁体、下磁体、壳,上磁体和下磁体在泵水壳的外面,泵水壳的下端固定在浮力壳内;出水固定在泵水壳的中心孔内,泵水壳内有活塞,密封球或密封锥密封进水腔和挤压腔的进水通道;铁芯活塞上端的限位孔内固定有分水限制板,铁芯活塞的内锥孔内安装有密封球或密封锥,铁芯活塞的下端有容纳孔。直压排污环保设备的结构紧凑、振动小、电能利用率高、动力强劲,适合污水处理站抽排污水、污水池中抽排污水和在堵塞的污水沟中抽排污水,抽污水时漂浮在污水面上随污水位的降低而自动下降,进行移动排污作业方便。
5 制造叶片组件的方法 CN200980127991.7 2009-07-16 CN102099135B 2014-06-18 达米恩·阿奎尔; 塞巴斯蒂安·迪加布鲁德库萨特
发明涉及一种制造用于涡轮机低压导流叶片的金属叶片区(1)的方法,所述叶片区的至少一个叶片(14)包含一个内部腔体(13)和形成在壁上的至少一个孔(19),所述内部腔体用于容纳气体检测探头或与气体检测探头相通,所述至少一个孔(19)构成了气体从涡轮机低压区向所述腔体(13)和所述探头的通道,所述方法通过将对应于所述腔体(13)的型芯安装到铸模并在所述铸模的腔中铸造熔融金属来制造所述金属叶片区。这种方法的特征在于,对于用于与所述腔连通的每个孔(19)而言,所述型芯(20)包括突起物(22),该突起物(22)穿透模型的内部表面,并构成了将型芯(20)保持在铸模中的适当位置的唯一因素。
6 热固性聚酰亚胺耐磨自润滑斜盘及制备方法 CN201010138688.1 2010-03-30 CN101806299B 2012-09-05 孙志华
发明公开了一种热固性聚酰亚胺耐磨自润滑斜盘及制备方法。旨在提供一种使用寿命长,能在短期内承受干摩擦的热固性聚酰亚胺耐磨自润滑斜盘及制备方法。热固性聚酰亚胺耐磨自润滑斜盘是由金属基体和自润滑耐磨涂层组成,所述金属基体为基、铁烧结基、铜基、基、锌基中的一种,所述金属基体是通过机械加工方式制成的;在金属基体两侧环形平面上涂覆有自润滑耐磨涂层,该自润滑耐磨涂层构成所述斜盘环形平面工作层;其特征在于:所述的自润滑耐磨涂层的耐磨涂料组成成份按重量百分含量包括:热固性聚酰亚胺40~65%和固体润滑剂35~60%。自润滑耐磨涂层的涂覆方法依次是:自润滑耐磨涂料的配制;喷涂;自润滑耐磨涂层烧结。
7 制造叶片组件的方法 CN200980127991.7 2009-07-16 CN102099135A 2011-06-15 达米恩·阿奎尔; 塞巴斯蒂安·迪加布鲁德库萨特
发明涉及一种制造用于涡轮机低压导流叶片的金属叶片区(1)的方法,所述叶片区的至少一个叶片(14)包含一个内部腔体(13)和形成在壁上的至少一个孔(19),所述内部腔体用于容纳气体检测探头或与气体检测探头相通,所述至少一个孔(19)构成了气体从涡轮机低压区向所述腔体(13)和所述探头的通道,所述方法通过将对应于所述腔体(13)的型芯安装到铸模并在所述铸模的腔中铸造熔融金属来制造所述金属叶片区。这种方法的特征在于,对于用于与所述腔连通的每个孔(19)而言,所述型芯(20)包括突起物(22),该突起物(22)穿透模型的内部表面,并构成了将型芯(20)保持在铸模中的适当位置的唯一因素。
8 热固性聚酰亚胺耐磨自润滑斜盘及制备方法 CN201010138688.1 2010-03-30 CN101806299A 2010-08-18 孙志华
发明公开了一种热固性聚酰亚胺耐磨自润滑斜盘及制备方法。旨在提供一种使用寿命长,能在短期内承受干摩擦的热固性聚酰亚胺耐磨自润滑斜盘及制备方法。热固性聚酰亚胺耐磨自润滑斜盘是由金属基体和自润滑耐磨涂层组成,所述金属基体为基、铁烧结基、铜基、基、锌基中的一种,所述金属基体是通过机械加工方式制成的;在金属基体两侧环形平面上涂覆有自润滑耐磨涂层,该自润滑耐磨涂层构成所述斜盘环形平面工作层;其特征在于:所述的自润滑耐磨涂层的耐磨涂料组成成份按重量百分含量包括:热固性聚酰亚胺40~65%和固体润滑剂35~60%。自润滑耐磨涂层的涂覆方法依次是:自润滑耐磨涂料的配制;喷涂;自润滑耐磨涂层烧结。
9 Dry running flexible impeller pump and method of manufacture US12925331 2010-10-19 US08997348B2 2015-04-07 Mark R. Harvie
This invention relates to a Dry Running Flexible Impeller Pump and Method of Manufacture designed to provide a flexible impeller pump capable of being run dry for extended periods of time without damage. The pump's components are comprised of low friction materials limiting the heat of friction created by the impeller in use. The impeller is cast of pre-molding silicone substrate containing a quantity of mold release that will not prevent the deposition of a low friction compound coating on the surface of the impeller in a mold that is treated with a low friction industrial coating. Once the impeller is removed from the mold it is solvent cleaned, vacuum baked at a temperature high enough to drive off residual traces of mold release or compounds used to maintain the silicone substrate in suspension, and then coated with a polymer of Poly Para Xylylene by vacuum deposition.
10 METHOD OF MANUFACTURING A BLADING COMPONENT US13002992 2009-07-16 US20110113627A1 2011-05-19 Damien Alquier; Sebastien Digard Brou De Cuissart
A method of manufacturing a metal blading sector for low-pressure guide vanes of a turbomachine of which at least one blade includes an internal cavity configured to accept or communicate with a gas detection probe and at least one hole formed in the wall constituting a passage for gas from a low-pressure zone of the turbomachine toward the cavity and the probe through the fitting, into a casting mold, of a core corresponding to the cavity and the casting of a molten metal in the cavity of the casting mold. The core includes, for each hole for communication with the cavity, a protrusion penetrating the internal surface of the mold and constituting the only element holding the core in position in the casting mold.
11 Dry running flexible impeller pump and method of manufacture US12925331 2010-10-19 US20110038713A1 2011-02-17 Mark R. Harvie
This invention relates to a Dry Running Flexible Impeller Pump and Method of Manufacture designed to provide a flexible impeller pump capable of being run dry for extended periods of time without damage. The pump's components are comprised of low friction materials limiting the heat of friction created by the impeller in use. The impeller is cast of pre-molding silicone substrate containing a quantity of mold release that will not prevent the deposition of a low friction compound coating on the surface of the impeller in a mold that is treated with a low friction industrial coating. Once the impeller is removed from the mold it is solvent cleaned, vacuum baked at a temperature high enough to drive off residual traces of mold release or compounds used to maintain the silicone substrate in suspension, and then coated with a polymer of Poly Para Xylylene by vacuum deposition.
12 Method for fabricating integral composite structural material US11618062 2006-12-29 US07854969B2 2010-12-21 Michael Lee Millard; Horace Richardson, Jr.; Joseph Anthony Corrado
The present invention is an integral composite structural (ICS) material comprising an open metal structure having at least one external side and internal surfaces defining a plurality of open shapes with a ceramic matrix composite bonded to at least one external side and the surfaces of at least a substantial portion of the plurality of open shapes and occupying at least a substantial portion of the plurality of open shapes. The open metal structure, independent of the ceramic matrix composite, has a total metal volume percent in the range of about 10% to about 90%, with no dimension of any open shape being greater than about ¾ inch. The ceramic matrix layer covers a substantial portion of at least one external side of the open metal structure. At least one external side of the metal portion of the ICS material is bonded with a ceramic matrix composite such that the ceramic layer occupies at least a significant portion of the open pores of the metal portion and is bonded to a significant portion of at least one external side of the metal element. The present invention is also a method of manufacturing such an ICS material.
13 Integral composite structural material US10703271 2003-11-07 US07282274B2 2007-10-16 Michael Lee Millard; Horace Richardson, Jr.; Joseph Anthony Corrado
The present invention is an integral composite structural (ICS) material comprising an open metal structure having at least one external side and internal surfaces defining a plurality of open shapes with a ceramic matrix composite bonded to at least one external side and the surfaces of at least a substantial portion of the plurality of open shapes and occupying at least a substantial portion of the plurality of open shapes. The open metal structure, independent of the ceramic matrix composite, has a total metal volume percent in the range of about 10% to about 90%, with no dimension of any open shape being greater than about ¾ inch. The ceramic matrix layer covers a substantial portion of at least one external side of the open metal structure. At least one external side of the metal portion of the ICS material is bonded with a ceramic matrix composite such that the ceramic layer occupies at least a significant portion of the open pores of the metal portion and is bonded to a significant portion of at least one external side of the metal element. The present invention is also a method of manufacturing such an ICS material.
14 Vane assembly US3790317D 1972-11-20 US3790317A 1974-02-05 HYDE A; LA FRAMBOISE L
A sintered metal vane hub and a vane blade formed of an epoxy and woven glass cloth laminate are assembled by die casting magnesium or injecting plastic into recesses on the hub and blade. The vane is shown in a semi-articulated vane pump used to inject air into the exhaust system of a vehicle engine.
15 The method of manufacturing the blade arrangement parts JP2011517981 2009-07-16 JP5449347B2 2014-03-19 アルキエ・ダミアン; デイガール・ブルー・ドウ・キユイサール,セバスチヤン
16 Scroll fluid machine JP30789888 1988-12-07 JPH02157487A 1990-06-18 MOROZUMI NAOYA; SAKATA KANJI; HAYANO MAKOTO
PURPOSE:To restrain the thermal expansion in the radial direction of a revolving scroll, reduce the leakage of a gas, and improve performance and reliability by reinforcing at least the portion including the outer periphery of the end plate of a revolving scroll with an iron group metal member. CONSTITUTION:The outer periphery of the end plate 1b of a revolving scroll body 1 which are integrally formed with an aluminum alloy, the back face of the end plate 1b, and the outer periphery of a boss portion 1c are press fitted into an iron group metal ring body 2 by a means of shrink-age fit, etc. to reinforce the surface. Thereby, the thermal expansion in the radial direction of the end plate 1b and boss portion 1c can be restrained to a degree equal to that of an iron group metal while, at the time of forming a compression mechanism portion by fitting a fixed scroll to laps 1a, the clearance in the radial direction caused by the difference in the degree of thermal expansion can be restrained small. Also, since the back face of the end plate 1b is also reinforce, sliding thereof on a thrust receiver can be made smooth. Thereby, the thermal expansion in the radial direction of the revolving scroll can be restrained, reducing the leakage of a gas while improving performance and reliability.
17 KOLBENBOLZENBUCHSE EP05736835.9 2005-03-16 EP1725691B1 2010-06-30 DEICKE, Klaus; SCHUBERT, Werner; BUSCHENHENKE, Theo; RATHJE, Reimond; LANGNER, Heinbert
18 Compressor coating EP00104565.7 2000-03-13 EP1036938A2 2000-09-20 Sugiura, Manabu; Iwama, Kazuaki; Sato, Teiichi

The durability of a coating layer formed on the sliding surface between two members of a compressor, and the sliding contact between the two members, is kept excellent over a long period of time. In a peripheral portion 10d of a swash plate 10, a pair of shoes 20 are connected to the swash plate 10 while intervening between the swash plate 10 and a piston 8. Both the swash plate 10 and the shoes 20 are formed from an iron series material. A film 23 is formed on both surfaces 22 of the peripheral portion 10d of the swash plate 10, and the shoes 20 slide on the film 23 on the swash plate 10. The film 23 is a coating layer formed from a resin containing metallic particles. The particle size of the metallic particles is larger than the thickness of the film 23 (e.g., from 10 to 100 µm), and the surface of the film 23 is made smooth by polishing. The resin functioning as a binder of the metallic particles is formed from, for example, a polyimide resin.

19 ROTARY LOBE PUMP WITH WIPER BLADES US14746493 2015-06-22 US20150285248A1 2015-10-08 Randy Dixon; Brett Howell
A positive displacement rotary pump with an improved impeller design integrating replaceable wiper inserts. The impeller generally has one or more lobes and an equal number of conjugate surfaces. Each lobe has an arcuate peripheral end comprising a plurality of wiper blades. Each lobe further has a facial wiper blade on each face of the lobe. The wiper blades improve efficiency by making a seal with a pump chamber or the conjugate surface on the other impeller as it rotates. The wiper blades are arranged such that constant and successive contact between wiper blades and impellers is achieved.
20 Method of manufacturing a blading component US13002992 2009-07-16 US08615875B2 2013-12-31 Damien Alquier; Sebastien Digard Brou De Cuissart
A method of manufacturing a metal blading sector for low-pressure guide vanes of a turbomachine of which at least one blade includes an internal cavity configured to accept or communicate with a gas detection probe and at least one hole formed in the wall constituting a passage for gas from a low-pressure zone of the turbomachine toward the cavity and the probe through the fitting, into a casting mold, of a core corresponding to the cavity and the casting of a molten metal in the cavity of the casting mold. The core includes, for each hole for communication with the cavity, a protrusion penetrating the internal surface of the mold and constituting the only element holding the core in position in the casting mold.
QQ群二维码
意见反馈