SU769046A1 - Apparatus for securing driven unit - Google Patents
Apparatus for securing driven unit Download PDFInfo
- Publication number
- SU769046A1 SU769046A1 SU782586253A SU2586253A SU769046A1 SU 769046 A1 SU769046 A1 SU 769046A1 SU 782586253 A SU782586253 A SU 782586253A SU 2586253 A SU2586253 A SU 2586253A SU 769046 A1 SU769046 A1 SU 769046A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- braces
- intermediate links
- drive
- struts
- compressor
- Prior art date
Links
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
1one
Изобретение относитс к средствам координации осей приводных агрегатов, т. е. модулей машины, и может быть использовано в турбокомпрессорных установках и других отрасл х техники, где необходима координаци осей при их угловых и линейных смещени х.The invention relates to the coordination of axles of drive units, i.e., machine modules, and can be used in turbo-compressor installations and other equipment that require coordination of axes at their angular and linear displacements.
Известно устройство дл креплени приводного агрегата, преимущественно компрессора , на газотурбинном двигателе, содержащее соосные фланцы на корпусах агрегата и двигател ,1.A device for mounting a drive unit, preferably a compressor, on a gas turbine engine, comprising coaxial flanges on the bodies of the unit and the engine, is known.
Такое крепление решает задачу тепловых компенсаций блочного корпуса, на угловое смещение осей газотурбинного двигател и приводного агрегата при работе остаетс неустраненным, что ведет к увеличению рабочих зазоров в элементах двигател .Such fastening solves the problem of thermal compensations of the block body; the angular displacement of the axes of the gas turbine engine and the drive unit during operation remains unresolved, which leads to an increase in the working gaps in the engine elements.
Наличие углового смещени осей, как правило, снижает надежность устройства и требует увеличени жесткости корпусов и их соединени между собой или координации смеш.ени осей корпусов.The presence of an angular displacement of the axes, as a rule, reduces the reliability of the device and requires an increase in the rigidity of the bodies and their interconnection or coordination of the mixing of the axes of the bodies.
Целью изобретени вл етс повыщение надежности устройства.The aim of the invention is to increase the reliability of the device.
Указанна цель достигаетс тем, что устройство снабжено, по крайней мере, двум парами подкосов, шарнирно установленных на фланце двигател , и, по крайней мере.This goal is achieved in that the device is equipped with at least two pairs of struts hinged on the engine flange, and at least.
двум соединенными скобой промежуточными звень ми, шарнирно укрепленными на консольном конце корпуса агрегата, а концы каждой пары подкосов щарнирно 5 соединены с соответствующим промежуточным звеном.two interconnected brackets with intermediate links hinged at the cantilever end of the unit casing, and the ends of each pair of braces 5 are hingedly connected to the corresponding intermediate link.
На фиг. 1 схематично изображено устройство дл креплени приводного агрегата; на фиг. 2 - вид А фиг. 1.FIG. 1 schematically shows a device for fastening a drive unit; in fig. 2 - view A of FIG. one.
10 Устройство дл креплени приводного агрегата , т. е. модулей машины, включающей консольный корпус 1 приводного осевого компрессора и корпус 2 газотурбинного привода, соединенные соосно, содержит две10 A device for fastening a drive unit, i.e. machine modules comprising a cantilever case 1 of a drive axial compressor and a case 2 of a gas turbine drive, connected coaxially, contains two
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU782586253A SU769046A1 (en) | 1978-03-06 | 1978-03-06 | Apparatus for securing driven unit |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU782586253A SU769046A1 (en) | 1978-03-06 | 1978-03-06 | Apparatus for securing driven unit |
Publications (1)
Publication Number | Publication Date |
---|---|
SU769046A1 true SU769046A1 (en) | 1980-10-07 |
Family
ID=20751774
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU782586253A SU769046A1 (en) | 1978-03-06 | 1978-03-06 | Apparatus for securing driven unit |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU769046A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5271217A (en) * | 1992-12-09 | 1993-12-21 | General Electric Company | Mounting arrangement for a single shaft combined cycle system |
-
1978
- 1978-03-06 SU SU782586253A patent/SU769046A1/en active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5271217A (en) * | 1992-12-09 | 1993-12-21 | General Electric Company | Mounting arrangement for a single shaft combined cycle system |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US8707710B2 (en) | Tailorable design configuration topologies for aircraft engine mid-turbine frames | |
US4458862A (en) | Antiresonant suspension device for helicopter | |
US4875655A (en) | Vibration isolating engine mount | |
US4441313A (en) | Mounting devices for multiple flow turbojet engines | |
Al-Hussain et al. | Dynamic response of two rotors connected by rigid mechanical coupling with parallel misalignment | |
US4589816A (en) | Robot joint | |
EP1930555A2 (en) | Mid-turbine frame | |
EP1882827A2 (en) | Embedded mount for mid-turbine frame | |
US5028001A (en) | Method of vibration isolating an aircraft engine | |
CA1176223A (en) | Skids for rotating machinery | |
JPH04231752A (en) | Secondary moment compensator in five cylinder row type internal combustion engine | |
US4140028A (en) | Vibration isolation system | |
CA2038621A1 (en) | Engine mounting assembly | |
SU769046A1 (en) | Apparatus for securing driven unit | |
US5271217A (en) | Mounting arrangement for a single shaft combined cycle system | |
EP1607330A1 (en) | Load reduced engine mount | |
US5447025A (en) | Combined gas turbine and steam turbine power plant | |
US11008884B2 (en) | Gensets and methods of producing gensets from an engine and generator for hybrid electric propulsion | |
US3330514A (en) | Support structure for rotating machinery | |
EP3890855A1 (en) | A movement simulator | |
US2393141A (en) | Power plant mounting and method | |
RU2028971C1 (en) | Device for extending working modules of space vehicle | |
RU2730630C1 (en) | Device for connection of internal and external housings of turbomachine | |
RU2161263C2 (en) | Liquid-propellant afterburner rocket engine | |
SU1366387A1 (en) | Manipulator |