CN204314065U - A kind of Compressor test part rock-steady structure - Google Patents
A kind of Compressor test part rock-steady structure Download PDFInfo
- Publication number
- CN204314065U CN204314065U CN201420713241.6U CN201420713241U CN204314065U CN 204314065 U CN204314065 U CN 204314065U CN 201420713241 U CN201420713241 U CN 201420713241U CN 204314065 U CN204314065 U CN 204314065U
- Authority
- CN
- China
- Prior art keywords
- test part
- compressor test
- casing
- air entraining
- entraining pipe
- 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.)
- Active
Links
Abstract
A kind of Compressor test part rock-steady structure, comprises Compressor test part and measures casing, Compressor test part sprue, Compressor test part switching outer shroud, bypass is moved back and is breathed heavily system air entraining pipe subassembly, Compressor test part switching inner ring, the weld seam of flange and air entraining pipe, air entraining pipe weld seam, Compressor test part exit casing, left side exhaust column, bleed metal hose, bypass is moved back and is breathed heavily system air entraining pipe subassembly, Compressor test part casing, right side exhaust column, gas gathering manifold road; Wherein: it is Compressor test part sprue that Compressor test part is measured between casing and Compressor test part switching inner ring, Compressor test part switching outer shroud is measured casing with Compressor test part and is connected by bolt and seam; Gas gathering manifold road is vented column with left side and right side exhaust column is connected.Advantage of the present utility model: effectively alleviate exhaust throttle load.System works is effective, alleviates this exerciser deficiency of test capability under high temperature rise, high discharge pressure in the past.
Description
Technical field
The utility model relates to Compressor test field, particularly a kind of Compressor test part rock-steady structure.
Background technology
Compressor surge be air-flow pneumatic plant axis direction occurs low frequency, high amplitude air-flow reforming phenomena.The mechanical vibration brought thus, can cause badly damaged at short notice the operation of testpieces.In compressor part test, the generation of surge greatly threatens the safe handling of pneumatic plant.
Utility model content
The purpose of this utility model stablizes to realize Compressor test part, and spy provides a kind of Compressor test part rock-steady structure.
The utility model provides a kind of Compressor test part rock-steady structure, it is characterized in that: described Compressor test part rock-steady structure, comprise Compressor test part and measure casing 1, Compressor test part sprue 2, Compressor test part switching outer shroud 3, bypass is moved back and is breathed heavily system air entraining pipe subassembly 4, Compressor test part switching inner ring 5, the weld seam 6 of flange and air entraining pipe, air entraining pipe weld seam 7, Compressor test part exit casing 8, left side exhaust column 9, bleed metal hose 10, bypass is moved back and is breathed heavily system air entraining pipe subassembly 11, Compressor test part casing 12, right side exhaust column 13, gas gathering manifold road 14,
Wherein: it is Compressor test part sprue 2 that Compressor test part is measured between casing 1 and Compressor test part switching inner ring 5, Compressor test part switching outer shroud 3 is measured casing 1 with Compressor test part and is connected by bolt and seam; Bypass move back breathe heavily system air entraining pipe subassembly 4 be welded on Compressor test part switching outer shroud 3 on form air entraining pipe weld seam 7; Flange and bypass are moved back and are breathed heavily system air entraining pipe subassembly 4 and weld, and form the weld seam 6 of flange and air entraining pipe; Compressor test part exit casing 8 and Compressor test part outer shroud 3 of transferring is connected; Left side exhaust column 9 is connected with Compressor test part casing 12 respectively by bleed metal hose 10 with right side exhaust column 13, and gas gathering manifold road 14 is vented column 9 with left side and right side exhaust column 13 is connected.
The number of described bleed metal hose 10 is 6 ~ 12.
Advantage of the present utility model:
Compressor test part rock-steady structure described in the utility model, effectively alleviates exhaust throttle load.System works is effective, alleviates this exerciser deficiency of test capability under high temperature rise, high discharge pressure in the past.
Accompanying drawing explanation
Below in conjunction with drawings and the embodiments, the utility model is described in further detail:
Fig. 1 is Compressor test part rock-steady structure scheme of installation;
Fig. 2 is Compressor test part rock-steady structure lateral plan.
Embodiment
Embodiment 1
Present embodiments provide a kind of Compressor test part rock-steady structure, it is characterized in that: described Compressor test part rock-steady structure, comprise Compressor test part and measure casing 1, Compressor test part sprue 2, Compressor test part switching outer shroud 3, bypass is moved back and is breathed heavily system air entraining pipe subassembly 4, Compressor test part switching inner ring 5, the weld seam 6 of flange and air entraining pipe, air entraining pipe weld seam 7, Compressor test part exit casing 8, left side exhaust column 9, bleed metal hose 10, bypass is moved back and is breathed heavily system air entraining pipe subassembly 11, Compressor test part casing 12, right side exhaust column 13, gas gathering manifold road 14,
Wherein: it is Compressor test part sprue 2 that Compressor test part is measured between casing 1 and Compressor test part switching inner ring 5, Compressor test part switching outer shroud 3 is measured casing 1 with Compressor test part and is connected by bolt and seam; Bypass move back breathe heavily system air entraining pipe subassembly 4 be welded on Compressor test part switching outer shroud 3 on form air entraining pipe weld seam 7; Flange and bypass are moved back and are breathed heavily system air entraining pipe subassembly 4 and weld, and form the weld seam 6 of flange and air entraining pipe; Compressor test part exit casing 8 and Compressor test part outer shroud 3 of transferring is connected; Left side exhaust column 9 is connected with Compressor test part casing 12 respectively by bleed metal hose 10 with right side exhaust column 13, and gas gathering manifold road 14 is vented column 9 with left side and right side exhaust column 13 is connected.
The number of described bleed metal hose 10 is 6.
Embodiment 2
Present embodiments provide a kind of Compressor test part rock-steady structure, it is characterized in that: described Compressor test part rock-steady structure, comprise Compressor test part and measure casing 1, Compressor test part sprue 2, Compressor test part switching outer shroud 3, bypass is moved back and is breathed heavily system air entraining pipe subassembly 4, Compressor test part switching inner ring 5, the weld seam 6 of flange and air entraining pipe, air entraining pipe weld seam 7, Compressor test part exit casing 8, left side exhaust column 9, bleed metal hose 10, bypass is moved back and is breathed heavily system air entraining pipe subassembly 11, Compressor test part casing 12, right side exhaust column 13, gas gathering manifold road 14,
Wherein: it is Compressor test part sprue 2 that Compressor test part is measured between casing 1 and Compressor test part switching inner ring 5, Compressor test part switching outer shroud 3 is measured casing 1 with Compressor test part and is connected by bolt and seam; Bypass move back breathe heavily system air entraining pipe subassembly 4 be welded on Compressor test part switching outer shroud 3 on form air entraining pipe weld seam 7; Flange and bypass are moved back and are breathed heavily system air entraining pipe subassembly 4 and weld, and form the weld seam 6 of flange and air entraining pipe; Compressor test part exit casing 8 and Compressor test part outer shroud 3 of transferring is connected; Left side exhaust column 9 is connected with Compressor test part casing 12 respectively by bleed metal hose 10 with right side exhaust column 13, and gas gathering manifold road 14 is vented column 9 with left side and right side exhaust column 13 is connected.
The number of described bleed metal hose 10 is 10.
Embodiment 3
Present embodiments provide a kind of Compressor test part rock-steady structure, it is characterized in that: described Compressor test part rock-steady structure, comprise Compressor test part and measure casing 1, Compressor test part sprue 2, Compressor test part switching outer shroud 3, bypass is moved back and is breathed heavily system air entraining pipe subassembly 4, Compressor test part switching inner ring 5, the weld seam 6 of flange and air entraining pipe, air entraining pipe weld seam 7, Compressor test part exit casing 8, left side exhaust column 9, bleed metal hose 10, bypass is moved back and is breathed heavily system air entraining pipe subassembly 11, Compressor test part casing 12, right side exhaust column 13, gas gathering manifold road 14,
Wherein: it is Compressor test part sprue 2 that Compressor test part is measured between casing 1 and Compressor test part switching inner ring 5, Compressor test part switching outer shroud 3 is measured casing 1 with Compressor test part and is connected by bolt and seam; Bypass move back breathe heavily system air entraining pipe subassembly 4 be welded on Compressor test part switching outer shroud 3 on form air entraining pipe weld seam 7; Flange and bypass are moved back and are breathed heavily system air entraining pipe subassembly 4 and weld, and form the weld seam 6 of flange and air entraining pipe; Compressor test part exit casing 8 and Compressor test part outer shroud 3 of transferring is connected; Left side exhaust column 9 is connected with Compressor test part casing 12 respectively by bleed metal hose 10 with right side exhaust column 13, and gas gathering manifold road 14 is vented column 9 with left side and right side exhaust column 13 is connected.
The number of described bleed metal hose 10 is 12.
Claims (2)
1. a Compressor test part rock-steady structure, it is characterized in that: described Compressor test part rock-steady structure, comprise Compressor test part and measure casing (1), Compressor test part sprue (2), Compressor test part switching outer shroud (3), bypass is moved back and is breathed heavily system air entraining pipe subassembly (4), Compressor test part switching inner ring (5), the weld seam (6) of flange and air entraining pipe, air entraining pipe weld seam (7), Compressor test part exit casing (8), left side exhaust column (9), bleed metal hose (10), bypass is moved back and is breathed heavily system air entraining pipe subassembly (11), Compressor test part casing (12), right side exhaust column (13), gas gathering manifold road (14),
Wherein: it is Compressor test part sprue (2) that Compressor test part is measured between casing (1) and Compressor test part switching inner ring (5), Compressor test part switching outer shroud (3) is measured casing (1) with Compressor test part and is connected by bolt and seam; Bypass is moved back and is breathed heavily system air entraining pipe subassembly (4) and be welded on that Compressor test part switching outer shroud (3) is upper forms air entraining pipe weld seam (7); Flange and bypass are moved back and are breathed heavily system air entraining pipe subassembly (4) and weld, and form the weld seam (6) of flange and air entraining pipe; Compressor test part exit casing (8) and Compressor test part outer shroud (3) of transferring is connected; Left side exhaust column (9) is connected with Compressor test part casing (12) respectively by bleed metal hose (10) with right side exhaust column (13), and gas gathering manifold road (14) and left side are vented column (9) and right side exhaust column (13) is connected.
2. according to Compressor test part rock-steady structure according to claim 1, it is characterized in that: the number of described bleed metal hose (10) is 6 ~ 12.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420713241.6U CN204314065U (en) | 2014-11-21 | 2014-11-21 | A kind of Compressor test part rock-steady structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420713241.6U CN204314065U (en) | 2014-11-21 | 2014-11-21 | A kind of Compressor test part rock-steady structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204314065U true CN204314065U (en) | 2015-05-06 |
Family
ID=53136372
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420713241.6U Active CN204314065U (en) | 2014-11-21 | 2014-11-21 | A kind of Compressor test part rock-steady structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204314065U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105443439A (en) * | 2015-05-19 | 2016-03-30 | 中国航空工业集团公司沈阳发动机设计研究所 | Exhaust casing assembly used for test piece of gas compressor |
| CN106989857A (en) * | 2017-03-20 | 2017-07-28 | 西北工业大学 | A kind of vertical lift fan experimental provision of ring-shaped bearing |
| CN107515109A (en) * | 2017-08-04 | 2017-12-26 | 中国航空工业集团公司西安飞机设计研究所 | A kind of total load measuring method of testpieces |
| CN110397615A (en) * | 2019-07-31 | 2019-11-01 | 中国航发沈阳发动机研究所 | A kind of multistage compressor experimental rig |
| CN112360793A (en) * | 2020-11-06 | 2021-02-12 | 中国船舶重工集团公司第七0三研究所 | Diffusion casing for large-flow ship gas turbine compressor test |
-
2014
- 2014-11-21 CN CN201420713241.6U patent/CN204314065U/en active Active
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105443439A (en) * | 2015-05-19 | 2016-03-30 | 中国航空工业集团公司沈阳发动机设计研究所 | Exhaust casing assembly used for test piece of gas compressor |
| CN106989857A (en) * | 2017-03-20 | 2017-07-28 | 西北工业大学 | A kind of vertical lift fan experimental provision of ring-shaped bearing |
| CN106989857B (en) * | 2017-03-20 | 2019-05-10 | 西北工业大学 | A kind of vertical lift fan experimental provision of ring-shaped bearing |
| CN107515109A (en) * | 2017-08-04 | 2017-12-26 | 中国航空工业集团公司西安飞机设计研究所 | A kind of total load measuring method of testpieces |
| CN110397615A (en) * | 2019-07-31 | 2019-11-01 | 中国航发沈阳发动机研究所 | A kind of multistage compressor experimental rig |
| CN112360793A (en) * | 2020-11-06 | 2021-02-12 | 中国船舶重工集团公司第七0三研究所 | Diffusion casing for large-flow ship gas turbine compressor test |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN204314065U (en) | A kind of Compressor test part rock-steady structure | |
| CN204647511U (en) | Anti-surge control device | |
| CN204286730U (en) | The system of breathing heavily is moved back in a kind of bypass for Compressor test part | |
| CN204061253U (en) | A kind of miniature gas turbine gas compressor | |
| CN203822435U (en) | Exhaust connection structure of supercharger of diesel | |
| CN102974177A (en) | Heat compensation device for high-temperature bag dust remover pulse spraying system | |
| CN203488432U (en) | Ternary-flow impeller of high-efficiency compressor | |
| CN202854110U (en) | Base of oxygen sensor | |
| CN203002140U (en) | Spraying-blowing system cooling device of bag type dust remover | |
| CN206972342U (en) | A kind of nuclear power generating sets muffler | |
| CN204785016U (en) | Explosion -proof valve base | |
| CN208518427U (en) | A kind of structure that zirconium tower ontology is connect with carbon steel skirt | |
| CN204164665U (en) | The special bleeding device of a kind of pressure regulating cabinet | |
| CN206722939U (en) | A kind of light bus blower air inlet assembly | |
| CN204142435U (en) | A kind of gas cylinder airtight detecting apparatus | |
| CN204301933U (en) | Araeosystyle film film pipe and upper end cover detect bubble-tight system simultaneously | |
| CN204405332U (en) | The analogue means of exhaust-driven turbo-charger exhaust-gas turbo charger in the simulation test of engine plateau | |
| CN203422677U (en) | Explosion-proof positive pressure control device | |
| CN202621894U (en) | Vacuum sand box for casting large-scale valve bodies | |
| CN209012780U (en) | A kind of gas-oil valve air accumulator safety vent device | |
| CN201803680U (en) | Convex type check tool for exhaust manifold air passage | |
| CN209143212U (en) | A kind of auxiliary blowing apparatus of painting raw material | |
| CN205015205U (en) | Ambient air particulate matter sampling pump unit | |
| CN205437355U (en) | Gas supply device | |
| CN206194886U (en) | Lithium ion power battery |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |