Apparatus for the transfer of a complete turbine module from a balancing machine to an engine and vice versa, and method
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
B21K-003/04
B23P-019/00
출원번호
US-0594904
(1984-03-29)
우선권정보
FR-0006157 (1983-04-15)
발명자
/ 주소
Bouiller Jean G. (Brunoy FRX) Delonge Jean-Claude L. (Corbeil-Essonnes FRX)
출원인 / 주소
Societe Nationale d\Etude et de Construction de Moteurs d\Aviation S.N.E.C.M.A. (Paris FRX 07)
인용정보
피인용 횟수 :
9인용 특허 :
5
초록▼
Apparatus for the transfer of a module, the module including an outer casing in which is held the stator stage and a turbine rotor constituted by disks supporting blade rows, the disks being held by tie bolts, the apparatus having a holding device of the outer casing on the balancing machine, a temp
Apparatus for the transfer of a module, the module including an outer casing in which is held the stator stage and a turbine rotor constituted by disks supporting blade rows, the disks being held by tie bolts, the apparatus having a holding device of the outer casing on the balancing machine, a temporary interconnection means of the disks of the turbine, and a transport device ensuring the securing of the turbine disks after withdrawal of the holding device.
대표청구항▼
An apparatus for transferring a turbine module from a balancing machine to an engine assembly and vice versa, the module comprising an external casing of the inlet guide nozzle array of the turbine within which the stator stage of the turbine is mounted, the turbine rotor incorporating disks and bla
An apparatus for transferring a turbine module from a balancing machine to an engine assembly and vice versa, the module comprising an external casing of the inlet guide nozzle array of the turbine within which the stator stage of the turbine is mounted, the turbine rotor incorporating disks and blade rows and is secured to the transmission shaft of the engine by tie bolts positioned in an array around the rotor axis and extending longitudinally of the axis, and the module further comprising a bell housing at the downstream end of the rotor and carrying a mounting seating, said apparatus comprising: means for mounting said external casing on a balancing machine, means for interconnecting temporarily the disks of the rotor, and transport means providing for interconnection of the turbine disks after withdrawal from the balancing machine wherein said means for mounting said external casing further comprises, an upstream part with a conical base having a seating enabling mounting of the module on the balancing machine, a downstream edge portion having a flange for securing the means for mounting said external casing to said external casing of the module, and a downstream part carrying an internal, cylindrical, portion co-axial and cooperating with said mounting seating of the bell housing and further comprising, flange means arranged at an outer, peripheral edge thereof to be secured to a downstream flange of said external casing of the module. A method of transferring a complete turbine module between an engine assembly and a balancing machine and subsequently from the balancing machine to an engine assembly, the module incorporating an external casing of the inlet guide nozzle array of the turbine within which the stator stage of the turbine is mounted, the turbine rotor incorporating disks and blade rows and being secured to the transmission shaft of the engine by tie bolts positioned in an array around the rotor axis and extending longitudinally of the axis, the module further comprising a bell housing at the downstream end of the rotor and carrying a mounting seating, the method comprising the steps of I. balancing the turbine rotor within the module including the steps of: (a) securing an upstream part of the external casing of the inlet guide nozzle array to an upstream part of mounting means, (b) securing the rotor of the turbine to the shaft of the balancing machine by tie bolts, (c) securing the downstream part of the mounting means to a downstream part of the external casing of the inlet guide nozzle array, the cylindrical part of the downstream part of the mounting means cooperating with the seating remaining mounted on the bell housing, and (d) balancing of the rotor, II. transferring the turbine module, the rotor having been balanced, including the steps of: (a) withdrawing the shaft assembly mounting means and turbine module from the balancing machine and placing the module in a vertical position within a disassembling means, (b) locating a clamping screw member along an axis of said bell housing, (c) unscrewing of the nuts of the tie bolts of the shaft of the balancing machine, (d) removing the rear part of the mounting means, (e) locating the downstream part of the transport device on a flange of the turbine module, (f) disassemblying the casinag of the inlet guide nozzle array from the front part of the mounting means, the front part and the tie bolts remaining in place on the shaft of the balancing machine, and (g) locating the front part of the transfer device secured with the aid of the said tie bolts and securing the disks; and III. locating the turbine module in the engine including the steps of: (a) removing the transfer tie bolts of the front part of the transfer means, (b) presenting the module to the engine, then securing tie bolts remaining on the transmission shaft in securing holes of the disks, and guiding the assembly into position, (c) securing the casing of the inlet guide nozzle array of the module on the casing of the combustion chamber, and (d) removing the rear part of the transport means.
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이 특허에 인용된 특허 (5)
Schuster Carl J. (Greensburg PA), Assembly and disassembly apparatus for use with a rotary machine.
Lissajoux Pierre J. (Saint Michel sur Orge FRX) Rigo Marcel L. (Paray Vieille Poste FRX), Device to correct an unbalance of the rotor of turbine engines.
Mansson ; Martin ; Torstenfelt ; Ragnar, Method of assembling a turbo-machine, apparatus for use in the method, and turbo machine constructed according to said.
Piekarski Arthur J. ; Forrester James M. ; Steckle Charles E. ; Gutta Richard F., Trilobe mounting with anti-rotation apparatus for an air duct in a gas turbine rotor.
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