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1. 发明申请

US20060105136A1 Mat 审中-公开
标题翻译：垫
公开(公告)号：US20060105136A1
公开(公告)日：2006-05-18
申请号：US10516861
申请日：2003-06-13
申请人： Peter Brazier , Thomas Brock , Robert Kerr , Bhawan Patel , Flemming Bojstrup , Patrick Morel
发明人： Peter Brazier , Thomas Brock , Robert Kerr , Bhawan Patel , Flemming Bojstrup , Patrick Morel
IPC分类号： D04H11/00 , D03D27/00 , B32B5/02 , B32B3/26 , B32B27/12
CPC分类号： B32B37/24 , A47G27/02 , A47L23/266 , B32B25/10 , B32B37/10 , B32B37/1027 , B32B37/12 , B32B2305/18 , B32B2305/70 , B32B2309/02 , B32B2309/12 , B32B2319/00 , B32B2471/04 , D06N7/0084 , D06N2203/068 , D06N2205/20 , Y10T428/23957 , Y10T428/23964 , Y10T428/23971 , Y10T428/23979 , Y10T428/249953 , Y10T442/2369
摘要： A mat with a textile surface (1) and an elastomer backing layer (2) that includes elastomer crumbs and a binder. The elastomer backing layer (2) includes voids between the elastomer crumbs for increased flexibility.
摘要翻译：具有织物表面（1）的垫和弹性体背衬层（2），其包括弹性体面包屑和粘合剂。弹性体背衬层（2）在弹性体面包屑之间包括用于增加柔性的空隙。

2. 发明申请

US20060008612A1 Mat 审中-公开
标题翻译：垫
公开(公告)号：US20060008612A1
公开(公告)日：2006-01-12
申请号：US10516967
申请日：2003-06-12
申请人： Peter Brazier , Thomas Brock , Robert Kerr , Bhawan Patel , Flemming Bojstrup , Patrick Morel
发明人： Peter Brazier , Thomas Brock , Robert Kerr , Bhawan Patel , Flemming Bojstrup , Patrick Morel
IPC分类号： B32B33/00
CPC分类号： B32B37/24 , A47G27/02 , A47L23/266 , B32B25/10 , B32B37/10 , B32B37/1027 , B32B37/12 , B32B2305/18 , B32B2305/70 , B32B2309/02 , B32B2309/12 , B32B2319/00 , B32B2471/04 , D06N7/0084 , D06N2203/068 , D06N2205/20 , Y10T428/23957 , Y10T428/23964 , Y10T428/23971 , Y10T428/23979 , Y10T428/249953 , Y10T442/2369
摘要： A mat with a tufted textile pile surface (1) comprises tufts of yarn tufted into a tufting substrate and an elastomer backing layer (2). The elastomer backing layer (2) includes elastomer crumbs and a binder.
摘要翻译：具有簇绒纺织物绒头表面（1）的垫包括簇绒成簇绒基质的绒头簇和弹性体背衬层（2）。弹性体背衬层（2）包括弹性体面包屑和粘合剂。

3. 发明申请

US20060151908A1 Method of making a mat 有权
标题翻译：制作垫子的方法
公开(公告)号：US20060151908A1
公开(公告)日：2006-07-13
申请号：US10516905
申请日：2003-06-12
申请人： Peter Brazier , Thomas Brock , Robert Kerr , Bhawan Patel , Remming Bojstrup , Patrick Morel
发明人： Peter Brazier , Thomas Brock , Robert Kerr , Bhawan Patel , Remming Bojstrup , Patrick Morel
IPC分类号： D04H11/00 , B32B25/12
CPC分类号： B32B37/24 , A47G27/02 , A47L23/266 , B32B25/10 , B32B37/10 , B32B37/1027 , B32B37/12 , B32B2305/18 , B32B2305/70 , B32B2309/02 , B32B2309/12 , B32B2319/00 , B32B2471/04 , D06N7/0084 , D06N2201/0254 , D06N2201/0263 , D06N2201/042 , D06N2201/087 , D06N2203/02 , D06N2203/041 , D06N2203/042 , D06N2203/068 , D06N2205/10 , D06N2205/14 , D06N2205/18 , D06N2205/20 , D06N2209/046 , D06N2209/067 , D06N2209/0823 , D06N2209/1671 , D06N2211/066 , Y02P70/649
摘要： A method of making a mat with a textile surface and an elastomer backing is provided. The method includes mixing elastomer crumbs and a binder, depositing the crumb/binder mixture in a layer (22), placing a textile surface element (34) on the layer to form a mat assembly, and pressing the mat assembly in a press (9) while setting the binder. The elastomer crumbs are consolidated to form an elastomer backing (2) that includes voids between the elastomer crumbs, and the textile surface element is bonded to the elastomer backing to form the upper textile layer (1) of the mat.
摘要翻译：提供了制造具有织物表面和弹性体背衬的垫的方法。该方法包括混合弹性体碎屑和粘合剂，将碎屑/粘合剂混合物沉积在层（22）中，将织物表面元件（34）放置在层上以形成垫组件，并将垫组件按压（9 ），同时设置粘合剂。弹性体碎屑被固结以形成弹性体背衬（2），其包括在弹性体面包屑之间的空隙，并且织物表面元件结合到弹性体背衬以形成垫的上部织物层（1）。

4. 发明授权

US07566374B2 Method of making a mat 有权
标题翻译：制作垫子的方法
公开(公告)号：US07566374B2
公开(公告)日：2009-07-28
申请号：US10516905
申请日：2003-06-12
申请人： Peter C. Brazier , Thomas A. P. Brock , Robert C. Kerr , Bhawan Patel , Flemming Bojstrup , Patrick Morel
发明人： Peter C. Brazier , Thomas A. P. Brock , Robert C. Kerr , Bhawan Patel , Flemming Bojstrup , Patrick Morel
IPC分类号： B32B37/24 , B30B5/02 , B30B5/04
CPC分类号： B32B37/24 , A47G27/02 , A47L23/266 , B32B25/10 , B32B37/10 , B32B37/1027 , B32B37/12 , B32B2305/18 , B32B2305/70 , B32B2309/02 , B32B2309/12 , B32B2319/00 , B32B2471/04 , D06N7/0084 , D06N2201/0254 , D06N2201/0263 , D06N2201/042 , D06N2201/087 , D06N2203/02 , D06N2203/041 , D06N2203/042 , D06N2203/068 , D06N2205/10 , D06N2205/14 , D06N2205/18 , D06N2205/20 , D06N2209/046 , D06N2209/067 , D06N2209/0823 , D06N2209/1671 , D06N2211/066 , Y02P70/649
摘要： A method of making a mat with a textile surface and an elastomer backing is provided. The method includes mixing elastomer crumbs and a binder, depositing the crumb/binder mixture in a layer (22), placing a textile surface element (34) on the layer to form a mat assembly, and pressing the mat assembly in a press (9) while setting the binder. The elastomer crumbs are consolidated to form an elastomer backing (2) that includes voids between the elastomer crumbs, and the textile surface element is bonded to the elastomer backing to form the upper textile layer (1) of the mat.
摘要翻译：提供了制造具有织物表面和弹性体背衬的垫的方法。该方法包括混合弹性体碎屑和粘合剂，将碎屑/粘合剂混合物沉积在层（22）中，将织物表面元件（34）放置在层上以形成垫组件，并将垫组件按压（9 ），同时设置粘合剂。弹性体碎屑被固结以形成弹性体背衬（2），其包括在弹性体面包屑之间的空隙，并且织物表面元件结合到弹性体背衬以形成垫的上部织物层（1）。

5. 发明申请

US20050129343A1 Arrangement of bearing supports for the rotating shaft of an aircraft engine and an aircraft engine fitted with such an arrangement 有权
标题翻译：用于飞机发动机的旋转轴的轴承支撑件的布置和配备有这种布置的飞机发动机
公开(公告)号：US20050129343A1
公开(公告)日：2005-06-16
申请号：US10870059
申请日：2004-06-18
申请人： Gael Bouchy , Alain Mazelet , Daniel Martin , Patrick Morel
发明人： Gael Bouchy , Alain Mazelet , Daniel Martin , Patrick Morel
IPC分类号： F01D21/04 , F01D25/16 , F16C27/04 , F16C27/00
CPC分类号： F01D21/045 , F01D21/04 , F01D25/16 , F05B2260/3011 , F16C19/06 , F16C27/04 , F16C2360/23 , Y10S416/50
摘要： The arrangement of bearing supports (20, 50; 22, 52, 520) for a rotating shaft (10) mounted on bearings (20, 50) connected to an engine stator structure (16) by bearing supports 22, 52, 520) of which at least one is made up of N>1 elements (24, 240; 40, 400) effectively acting in parallel to simultaneously connect the said bearing (20, 50) to the said structure (16), of which N−1 of the said. N elements form this connection by means of fusible links (80, 800, 810), is made up of a first bearing (20) supported by a first bearing support (22) and a second bearing (50) supported by a second bearing support (52, 520), that of the two bearing supports (22, 52, 520) which makes up the said N>1 elements being the second bearing support (52, 520). Application to the rotating shaft (10) of an aircraft engine.
摘要翻译：安装在通过轴承支撑件22,52,520连接到发动机定子结构（16）的轴承（20,50）上的旋转轴（10）的轴承支撑件（20,50; 22,52,520）的布置其中至少一个由有效地并联作用的N> 1个元件（24,240; 40,400）组成，以将所述轴承（20,50）同时连接到所述结构（16），其中N-1个说。 N元件通过可熔连接件（80,800,810）形成该连接，由第一轴承（20）和第二轴承（50）组成，第一轴承（20）由第一轴承支撑件（22）支撑，第二轴承（50）由第二轴承支撑（52,520），构成所述N> 1个元件的两个轴承支撑件（22,52,520）的轴承支撑件（52,520）是第二轴承支撑件（52,520）。应用于飞机发动机的旋转轴（10）。

6. 发明授权

US07237959B2 Breakable coupling system for a turbojet fan shaft 有权
标题翻译：涡轮喷气风扇轴的可分离联接系统
公开(公告)号：US07237959B2
公开(公告)日：2007-07-03
申请号：US10500863
申请日：2002-10-24
申请人： Gael Bouchy , Bertrand Jean-Joseph Marie Heurtel , Eric Jean Masson , Bien-Aime Rakotondrainibe , Pierre Pandelakis , Daniel Martin , Patrick Morel , Henry Souyeaux
发明人： Gael Bouchy , Bertrand Jean-Joseph Marie Heurtel , Eric Jean Masson , Bien-Aime Rakotondrainibe , Pierre Pandelakis , Daniel Martin , Patrick Morel , Henry Souyeaux
IPC分类号： F16C19/08
CPC分类号： F01D25/16 , F01D21/045 , F01D25/162 , F05B2260/3011 , F16C19/522 , F16C2360/23
摘要： The invention relates to a rotary shaft arrangement carrying equipment at one end and extending rearwards from the equipment, the shaft (1) being supported by a first bearing (2) behind the equipment, and by a second bearing (3) behind the first bearing (2), the first bearing (2) being carried by a casing (4) surrounding the shaft (1) and extending rearwards from the first bearing (2) to a stator structure (5) to which the casing (4) is fastened by screws (6) that extend parallel to the shaft (1) and that are fusible in traction, the arrangement being characterized by the fact that the second bearing (3) is disposed with radial clearance (J) in a bore (7) of an annular support (8) secured to the stator structure (5), and is fastened to said annular support (8) by screws (9) that are parallel to the shaft (1) and that are fusible in shear, whereby the second bearing (3) can bear against said support (8) in the event of said screws (9) rupturing. The invention relates more particularly to the support for the fan shaft of a turbojet.
摘要翻译：本发明涉及一种旋转轴装置，其在一端承载设备并从设备向后延伸，所述轴（1）由设备后面的第一轴承（2）支撑，以及在第一轴承后面的第二轴承（3）（2），所述第一轴承（2）由围绕所述轴（1）的壳体（4）承载并且从所述第一轴承（2）向后延伸到定子结构（5），所述壳体（4）紧固到所述定子结构通过平行于轴（1）延伸并且易于牵引的螺钉（6），该装置的特征在于第二轴承（3）在径向间隙（J）中设置有径向间隙（J）固定到定子结构（5）上的环形支撑件（8），并且通过螺钉（9）固定到所述环形支撑件（8）上，所述螺钉（9）平行于所述轴（1）并且在剪切中是可熔的，由此所述第二轴承（3）在所述螺钉（9）断裂的情况下可承受所述支撑件（8） G。本发明更具体地涉及涡轮喷气发动机的风扇轴的支撑。

7. 发明授权

US06799416B2 Device for supporting and recentering the shaft of a turbojet fan after uncoupling 有权
标题翻译：拆卸后支撑和重新安装涡轮喷气风扇的轴的装置
公开(公告)号：US06799416B2
公开(公告)日：2004-10-05
申请号：US10387392
申请日：2003-03-14
申请人： Daniel Plona , Patrick Morel
发明人： Daniel Plona , Patrick Morel
IPC分类号： F02K306
CPC分类号： F01D21/045 , F01D25/16 , F05B2260/3011 , F05D2260/30 , F16C19/52 , F16C2360/23
摘要： The invention provides a device for supporting and recentering a shaft (2) after decoupling. The device comprises an annular support (4) surrounding the shaft (2), a bearing (5) secured to the annular support (4) and having an inner ring (9) which is spaced apart from the shaft by clearance J. The inner ring (9) has two webs or tenons (14a, 14b) that are normally held to the periphery of two troughs (16a, 16b) carried by the shaft (2). Two sets of balls (28a, 28b) normally bear against the bottoms of indentations (25, 26) formed facing one another in the adjacent radial walls of the troughs (16a, 16b) and of the inner ring (9). Resilient means (26) tend to urge the troughs (16a and 16b) towards each other. In the event of the webs or tenons (14a, 14b) breaking due to a large unbalance, the balls (28a, 28b) roll on the walls of the indentations (25, 26) and move the troughs (16a, 16b) apart from each other. The resilient mans (20) tend to bring the balls (28a, 28b) back towards the bottoms of the indentations and to recenter the shaft (2) relative to the inner ring (9).
摘要翻译：本发明提供一种用于在解耦之后支撑和重新调节轴（2）的装置。该装置包括围绕轴（2）的环形支撑件（4），固定到环形支撑件（4）并具有内部环（9）的轴承（5），该内圈与轴间隔开。环（9）具有通常保持在由轴（2）承载的两个槽（16a，16b）的周边的两个腹板或榫头（14a，14b）。两组球（28a，28b）通常抵靠在槽（16a，16b）和内圈（9）的相邻径向壁中彼此面对形成的凹陷（25,26）的底部。弹性装置（26）趋向于朝向彼此推动槽（16a和16b）。在由于大的不平衡导致腹板或榫头（14a，14b）断裂的情况下，滚珠（28a，28b）在压痕（25,26）的壁上滚动并使槽（16a，16b）从彼此。弹性杆（20）倾向于将球（28a，28b）返回到凹陷的底部并且相对于内圈（9）更换轴（2）。

8. 发明授权

US08622699B2 Device adapted to be fitted with propeller blades 有权
标题翻译：适用于安装螺旋桨叶片的装置
公开(公告)号：US08622699B2
公开(公告)日：2014-01-07
申请号：US12904852
申请日：2010-10-14
申请人： François Gallet , Patrick Morel , Wouter Balk
发明人： François Gallet , Patrick Morel , Wouter Balk
IPC分类号： F01D7/00
CPC分类号： F01D7/00 , B64C11/04 , F05D2260/79 , Y02T50/672 , Y02T50/673
摘要： A device adapted to be fitted with propeller blades includes a first retention ring including over a periphery thereof a plurality of radial bores; and a second retention ring including over a periphery thereof a plurality of radial bores, the first and second retention rings being mounted one on top of the other in the radial direction, each bore in the first retention ring being positioned opposite a bore in the second retention ring, a bore in the first retention ring arranged opposite a bore in the second retention ring forming a bore pair adapted to receive a foot of a blade.
摘要翻译：适于安装有螺旋桨叶片的装置包括第一保持环，其在其周边上包括多个径向孔; 以及第二保持环，其包括在其周边上的多个径向孔，所述第一和第二保持环在径向方向上一个地安装在另一个的顶部上，所述第一保持环中的每个孔与所述第二保持环中的孔相对地定位保持环，第一保持环中的孔与第二保持环中的孔相对布置，形成适于接收叶片脚的孔对。

9. 发明授权

US07299621B2 Three-spool by-pass turbojet with a high by-pass ratio 有权
标题翻译：具有高旁路比率的三线路旁路涡轮喷气发动机
公开(公告)号：US07299621B2
公开(公告)日：2007-11-27
申请号：US11045365
申请日：2005-01-31
申请人： Jacques Bart , Fabienne Lacorre , Yann Lebret , Vanessa Le Rousseau , Patrick Morel
发明人： Jacques Bart , Fabienne Lacorre , Yann Lebret , Vanessa Le Rousseau , Patrick Morel
IPC分类号： F02K3/065 , F02K3/072
CPC分类号： F02K3/072 , F01D17/162 , F02C3/067 , Y02T50/671
摘要： The invention relates to aerodynamically matching the rear fan of a turbojet having two fans and a low-pressure compressor at the front of the intermediate casing, said fans being driven by two independent shafts. Said compressor is disposed between the blades of the two fans and includes at least one ring of rotor blades around the periphery of a wheel driven by the drive shaft for the front fan, and at least two grids of stator vanes disposed on either side of the ring of rotor blades and inside a grid carrier ring. A stationary outer grid and a stator of variable pitch connect the ring to the fan casing.
摘要翻译：本发明涉及空气动力学匹配具有两个风扇的涡轮喷气发动机的后风扇和在中间壳体前部的低压压缩机，所述风扇由两个独立的轴驱动。所述压缩机设置在两个风扇的叶片之间，并且包括围绕由用于前风扇的驱动轴驱动的轮的周边的至少一个转子叶片环，以及设置在该风扇两侧的至少两个定子叶片格栅转子叶片环和电网载体环内。固定外格栅和可变节距的定子将环连接到风扇外壳。

10. 发明申请

US20050241291A1 Three-spool by-pass turbojet with a high by-pass ratio 有权
标题翻译：具有高旁路比率的三线路旁路涡轮喷气发动机
公开(公告)号：US20050241291A1
公开(公告)日：2005-11-03
申请号：US11045365
申请日：2005-01-31
申请人： Jacques Bart , Fabienne Lacorre , Yann Lebret , Vanessa Le Rousseau , Patrick Morel
发明人： Jacques Bart , Fabienne Lacorre , Yann Lebret , Vanessa Le Rousseau , Patrick Morel
IPC分类号： F02C9/20 , F01D17/16 , F02C3/067 , F02C3/073 , F02K3/06 , F02K3/072 , F02K3/04
CPC分类号： F02K3/072 , F01D17/162 , F02C3/067 , Y02T50/671
摘要： The invention relates to aerodynamically matching the rear fan of a turbojet having two fans and a low-pressure compressor at the front of the intermediate casing, said fans being driven by two independent shafts. Said compressor is disposed between the blades of the two fans and includes at least one ring of rotor blades around the periphery of a wheel driven by the drive shaft for the front fan, and at least two grids of stator vanes disposed on either side of the ring of rotor blades and inside a grid carrier ring. A stationary outer grid and a stator of variable pitch connect the ring to the fan casing.
摘要翻译：本发明涉及空气动力学匹配具有两个风扇的涡轮喷气发动机的后风扇和在中间壳体前部的低压压缩机，所述风扇由两个独立的轴驱动。所述压缩机设置在两个风扇的叶片之间，并且包括围绕由用于前风扇的驱动轴驱动的轮的周边的至少一个转子叶片环，以及设置在该风扇两侧的至少两个定子叶片格栅转子叶片环和电网载体环内。固定外格栅和可变节距的定子将环连接到风扇外壳。

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