CN200996324Y - Supporting cartridge receiver - Google Patents
Supporting cartridge receiver Download PDFInfo
- Publication number
- CN200996324Y CN200996324Y CN 200620168689 CN200620168689U CN200996324Y CN 200996324 Y CN200996324 Y CN 200996324Y CN 200620168689 CN200620168689 CN 200620168689 CN 200620168689 U CN200620168689 U CN 200620168689U CN 200996324 Y CN200996324 Y CN 200996324Y
- Authority
- CN
- China
- Prior art keywords
- support plate
- casing
- cylinder
- supporting casing
- supporting
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Images
Landscapes
- Supercharger (AREA)
Abstract
A bearing casing is characterized in that an external ring is V-shaped and an internal ring is C-shaped, and the external ring is connected with the internal ring.
Description
Technical field
The utility model relates to the gas turbine turbine technology.
Background technique
Gas turbine turbine exhaust diffuser basic structure is made of exhaust casing, support plate, bearing casing and supporting casing.Because temperature must be higher than cylinder place temperature in the blast tube, the thermal expansion amount of support plate is big, and the swell increment of cylinder is little, and along with constantly changing repeatedly of operating temperature, outside cylinder and support plate crack initiating failure because of thermal fatigue in causing easily.The hot problem of disharmony that solves cylinder and support plate generally has two kinds of structural designs, and a kind of is that supporting casing framework adds tapered wall, and another kind is that supporting casing framework adds oblique support plate, but these two kinds of structures more complicated all is not easy to realization.
Summary of the invention
The purpose of this utility model is to provide a kind of simple in structure, supporting casing of being easy to realize.
The utility model provides a kind of supporting casing, it is characterized in that: outer ring portion is the V-arrangement shape, and annular inner portion is the C shape, and VC links to each other, and forms elastic member.When the thermal expansion amount of support plate is big, utilize the resiliently deformable of yielding support casing to absorb the thermal expansion amount of support plate, reduce the extruding of support plate, thereby keep this part thermostability of turbine exhaust casing cylinder, avoid support plate and cylinder to produce heat fatigue cracking.
The supporting casing that the utility model provides, its outer ring portion two places are connected with the cylinder support plate with screw bolt and nut, and annular inner portion is connected with the bearing casing with tight bolt, to keep the balance on the fore-and-aft direction.
The supporting casing that the utility model provides, its advantage is: absorbs the thermal expansion amount of support plate, reduces the extruding of support plate, keep this part thermostability of turbine exhaust casing cylinder, simple in structure, be easy to processing and assembling.
Description of drawings
Fig. 1 is the structural representation of supporting casing.
Embodiment
Embodiment 1
The structure of supporting casing as shown in Figure 1, its outer ring portion is the V-arrangement shape, annular inner portion is the C shape, VC links to each other, and forms elastic member; Outer ring portion two places are connected with the cylinder support plate with screw bolt and nut, and annular inner portion is connected with the bearing casing with tight bolt.During work, the support plate expanded by heating, because of cylinder is a rigid design, and the supporting casing is an elastic design, yielding support casing pressurized absorbs the thermal expansion distortion of support plate to internal strain, thereby guarantees that cylinder is not subjected to too big thermal pressure, avoids the thermal fatigue of support plate, cylinder.
Claims (3)
1, a kind of supporting casing is characterized in that: outer ring portion is the V-arrangement shape, and annular inner portion is the C shape, and VC links to each other.
2, according to the described supporting casing of claim 1, it is characterized in that: outer ring portion two places of described sector are connected with the cylinder support plate with screw bolt and nut.
3, according to the described supporting casing of claim 1, it is characterized in that: the annular inner portion of described sector is connected with the bearing casing with tight bolt.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 200620168689 CN200996324Y (en) | 2006-12-28 | 2006-12-28 | Supporting cartridge receiver |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 200620168689 CN200996324Y (en) | 2006-12-28 | 2006-12-28 | Supporting cartridge receiver |
Publications (1)
Publication Number | Publication Date |
---|---|
CN200996324Y true CN200996324Y (en) | 2007-12-26 |
Family
ID=38994754
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 200620168689 Expired - Fee Related CN200996324Y (en) | 2006-12-28 | 2006-12-28 | Supporting cartridge receiver |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN200996324Y (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105179028A (en) * | 2015-04-22 | 2015-12-23 | 北京航空航天大学 | Turbine back-bearing-force casing and gate-leaf integrated structure |
-
2006
- 2006-12-28 CN CN 200620168689 patent/CN200996324Y/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105179028A (en) * | 2015-04-22 | 2015-12-23 | 北京航空航天大学 | Turbine back-bearing-force casing and gate-leaf integrated structure |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN204610035U (en) | A kind of pipeline heat compensating unit | |
CN200996324Y (en) | Supporting cartridge receiver | |
CN112503183B (en) | Elastic sealing structure | |
CN204477507U (en) | A kind of pipeline fixing support with compensation | |
CN107035017A (en) | Damper is surrendered stage by stage | |
CN210344675U (en) | Unrestrained bending-resistant metal corrugated expansion joint | |
CN201035981Y (en) | Device of reducing noise | |
CN206831025U (en) | A kind of connection locking structure of compressed air tunnel | |
CN213018297U (en) | Composite ceramic expansion joint | |
CN207999571U (en) | A kind of high-temperature composite material expansion joint | |
CN2924240Y (en) | Spherical compensator sealing structure | |
CN203273038U (en) | Expansion sealing device | |
CN210599440U (en) | Compressor valve plate, compressor and air conditioner | |
CN203362337U (en) | Heater part for hot-air engine | |
CN203499739U (en) | Flow channel structure for case behind modularized turbine | |
CN203499738U (en) | Flow passage structure for turbine back cartridge receiver | |
CN207261644U (en) | A kind of Novel piston pin | |
CN202756070U (en) | Flexible connection structure of exhaust system of diesel engine | |
CN204942881U (en) | A kind of low temperature vacuum thermal insulation pipeline single axial expansion joint | |
CN218151163U (en) | Gas turbine exhaust diffuser structure | |
CN202417717U (en) | Turbine support framework for aviation turbine engine | |
CN201779198U (en) | Multifunctional support shock absorber | |
CN201448487U (en) | Simple type check valve | |
CN210770949U (en) | Large-diameter hinge type metal corrugated expansion joint | |
CN218780775U (en) | Butterfly valve with compensation limit structure |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20071226 Termination date: 20151228 |
|
EXPY | Termination of patent right or utility model |