发明名称 System for sealing the piston of rotary piston machines
摘要 A sealing system of rotary piston machines, the rotor excludes rotor discs which are arranged next to one another, and which are seated on the common rotor axle and are pressed apart from one another by acting spring and/or gas forces in the joints between the discs in such a way that the end sides of the discs which point towards the side walls of the housing bear sealingly against the latter and thus prevent the access of the medium to the axles. Assemblies comprising movable shaped lamellae which adapt to the changing joint widths and prevent an inner flow around the rotor are present in the part joints between the discs.
申请公布号 US8920147(B2) 申请公布日期 2014.12.30
申请号 US200712312524 申请日期 2007.11.19
申请人 发明人 Guenther Eggert
分类号 F01C19/06;F04C15/00;F01C19/04;F01C19/08;F01C21/08;F01C1/22 主分类号 F01C19/06
代理机构 Jordan and Hamburg LLP 代理人 Jordan and Hamburg LLP
主权项 1. A sealing system for rotary piston engines comprising a rotor comprising rotor segments arranged next to each other in a casing and forming an opening through which a rotor axle passes, which rotor segments are biased apart by spring force or gas pressure in grooves located between the rotor segments so that face sides of the rotor segments facing side walls of the casing seal against said side walls, the rotor segments comprising axially and radially disposed peripheral guide grooves in each of which is housed a blade box extending entirely between and within substantial portions of said rotor segments thereby forming a seal with said casing, said blade box housing therein rotor portions being respectively adjustable one relative to another so as to seal against said side walls of the casing, said sealing of said blade boxes and said rotor portions preventing access of a fluid to the axle, said rotor portions comprising axially adjustable and radially adjustable lamellae units each comprised of a complementary pair of lamellae arranged to lie over each other when housed within a respective blade box, each of the lamellae being biased by a respective spring, the lamellae units and the blade boxes being positioned on the rotor segments so as to seal an axially-extending space in a sealing arrangement between said rotor segments and further arranged to radially seal the space between the rotor segments and the side walls forming a labyrinth sealing by mutual overlapping of the lamellae units thus achieving a dynamic sealing of the rotor in the axially and radially disposed peripheral guide grooves and along contact points of the rotor with the side walls in a direction in which the rotor runs so as to provide axial and radial sealing of the rotor so as to substantially prevent respective internal and external circumferential flows of fluid around the rotor, an interior space being defined within each of the lamellae and in which a compression spring is housed, and a compression wedge and compression wedge spring housed within the blade box and disposed between the lamellae, each of the lamellae comprising chamfers disposed upwardly with respect to the compression wedge and against which the compression wedge, when biased by the compression wedge spring, is applied so as to press each member of the pair of lamellae apart from each other in the axial direction and to press the lamellae in the radial direction against the side walls of the casing so as to exert a centrifugal force thereupon, and each of the lamellae and the compression wedge being respectively, individually biased so as to move independently of each other, said independent movement between the pair of lamellae and the compression wedge effecting both said axial and radial contact of the lamellae with said side walls of the casing and radial contact of said blade box against portions of said rotor segments which said blade box extends between so as to exert a centripetal force on said rotor segments, said contact of the lamellae with the side walls of the casing together with said housing of the lamellae within the blade boxes and said contact of said blade box against said rotor segments which said blade box extends between forming said labyrinth sealing of the rotor.
地址