CN102062058A - Engine room for wind generating set - Google Patents
Engine room for wind generating set Download PDFInfo
- Publication number
- CN102062058A CN102062058A CN2009102245197A CN200910224519A CN102062058A CN 102062058 A CN102062058 A CN 102062058A CN 2009102245197 A CN2009102245197 A CN 2009102245197A CN 200910224519 A CN200910224519 A CN 200910224519A CN 102062058 A CN102062058 A CN 102062058A
- Authority
- CN
- China
- Prior art keywords
- cabin
- generating set
- wind power
- power generating
- wall
- 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.)
- Pending
Links
Images
Classifications
-
- Y02E10/722—
Landscapes
- Wind Motors (AREA)
Abstract
The invention provides an engine room for a wind generating set. The engine room comprises a plurality of walls, wherein the plurality of walls are mutually connected to form the internal space of the engine room. The engine room is characterized in that: a supporting beam is arranged on the internal surface of the connecting part of at least one group of adjacent walls; and the part of the supporting beam, which contacts the adjacent walls, has the shape matched with the internal surface shape of the connecting part. The engine room for the wind generating set is simple in structure, convenient in transportation, easy to install and high in mechanical connection strength.
Description
Technical field
The present invention relates to the wind power generating set field, relate in particular to a kind of cabin that is used for wind power generating set.
Background technique
Along with energy shortage and environmental deterioration, wind-power electricity generation is because its recyclability and environmentally friendly characteristic and more and more be much accounted of.Be used for the wind wheel that the wind power generating set of wind-power electricity generation generally includes pylon, is positioned at the cabin on pylon top and is positioned at cabin one end.In the cabin, be provided with transmission system, braking system, yaw system, control system and generator etc. usually.Become big wind power generating set day by day and require to adopt increasing cabin, this causes the transportation in cabin and installation to become more and more difficult.In order to address this problem, overall structure is not adopted in the cabin usually, but is made up of a plurality of parts that can fit together.
For example WO2007/132408 discloses a kind of cabin that is used for wind power generating set, it comprises along the cabin the vertically longilineal a plurality of fuel plates of one-tenth, two adjacent panels linear elements adopt two L shaped angle brackets to be joined together, wherein each angle bracket is connected with a fuel plate respectively, and two angle brackets also interconnect.The disclosed another kind of Placement of WO2007/132408 forms T shape slit on a fuel plate, on another fuel plate, form elongated cuts, the lockplate that will have a bolt inserts the T shape slit on the fuel plate and makes bolt pass elongated cuts on another fuel plate, utilizes packing ring and nut that they are locked together again.
US2009/0191051 disclose a kind of be used for wind power generating set can stacked cabin, it comprise can be stacked a plurality of parts, the edge periphery of each part is provided with outward extending flange, and the flange of adjacent two parts can be secured together with bolt, thereby constitute a complete cabin.
The cabin of these prior aries not only complex structure, be difficult for to install, and the mechanical connection intensity between two adjacent constituent elements in cabin a little less than.Because the cabin is to use in the bigger wild environment of wind-force, under the large wind effect, the more weak cabin of mechanical connection intensity can produce distortion even thoroughly damage, thereby causes whole wind power generating set normally to move.
Therefore, need provide a kind of improved cabin that is used for wind power generating set.
Summary of the invention
Purpose of the present invention will overcome above-mentioned problems of the prior art or shortcoming exactly, provide a kind of simple in structure, be convenient to transport, be easy to install and the cabin that is used for wind power generating set that mechanical connection intensity is stronger.
According to the present invention, a kind of cabin that is used for wind power generating set is provided, described cabin comprises a plurality of walls, described a plurality of wall is connected with each other to form the engine room inside space, it is characterized in that, the internal surface of the connecting part of at least one group of adjacent wall in described a plurality of walls is provided with support beam, and the part that described support beam contacts with adjacent wall has the shape that the inner surface configuration with the connecting part is complementary.
Preferably, the internal surface of the connecting part of described at least one group of adjacent wall is curved shape, and the part that described support beam contacts with adjacent wall has the curved shape that the internal surface curved shape with corresponding connecting part is complementary.
Preferably, described at least one group of adjacent wall is vertical wall, and described support beam is the longitudinal bracing beam.
Preferably, described support beam is a hollow.
Preferably, described at least one group of adjacent wall is made up of a plurality of wall sections respectively, and each wall section is formed with inside vertically extending flange at its edge, and the adjacent wall part is closely linked together by inside vertically extending flange.
Preferably, described support beam is formed with and is used for keeping therein adeciduate at least one slot of connection strap.
Preferably, second sidewall, roof, aft bulkhead and front bulkhead that described cabin comprises diapire, the first side wall, is oppositely arranged with the first side wall, wherein, the internal surface of the connecting part of adjacent two walls in diapire, the first side wall, second sidewall and the roof is provided with the longitudinal bracing beam, and described adjacent two walls are fixed on the described longitudinal bracing beam.
Preferably, the part that contacts with described adjacent two walls of described longitudinal bracing beam has the curved shape that the internal surface curved shape with described connecting part is complementary.
Preferably, described longitudinal bracing beam is a hollow.
Preferably, described adjacent two walls are spliced together.
Preferably, described longitudinal bracing beam is provided with the hollow sleeve that has internal thread, is screwed in the described hollow sleeve so that will fix the bolt of described adjacent two walls.
Preferably, described roof partly is overlapped on the described the first side wall and second sidewall.
Preferably, be provided with liner strip between described roof and the described longitudinal bracing beam.
Preferably, described liner strip is provided with a plurality of tapped holes.
Preferably, at least one wall in described diapire, the first side wall, second sidewall and the roof is grouped into by a plurality of transverse wall portion.
Preferably, described lateral wall portion is formed with inside vertically extending flange at its transverse edge, and the adjacent transverse wall section is closely linked together by inside vertically extending flange.
Preferably, described aft bulkhead and front bulkhead are installed on the cabin body that is formed by diapire, the first side wall, second sidewall and roof.
Preferably, described longitudinal bracing beam is formed with at least one longitudinal socket, and the connection strap that is threaded the hole can be maintained in the described longitudinal socket and not come off.
Preferably, described longitudinal bracing beam longitudinally is formed with projection at least one side of its hollow space that contacts with described adjacent two walls.
Described support beam can be made by any suitable material, but preferably made of aluminum.Described cabin can be made by any suitable material, but is preferably made by glass fibre.Described cabin can be made into any suitable dimensions.
According to the cabin that is used for wind power generating set of the present invention, because the internal surface of the connecting part of at least one group of adjacent wall in described a plurality of walls is provided with support beam, the part that described support beam contacts with adjacent wall has the shape that the inner surface configuration with the connecting part is complementary, has stronger mechanical connection intensity between two adjacent walls, can stand the large wind effect of wild environment, can prevent that the cabin from producing distortion and damage, thereby can guarantee the normal operation of whole wind power generating set.In addition, the engine room structure that is used for wind power generating set according to the present invention simple, be convenient to transportation and be easy to install.Constitute each wall in cabin and support beam can be transported to other machining location at an easy rate or transportation or be transported to actual wind field between country variant, so that can be at the scene or other machining location assembling.
Description of drawings
Other purpose of the present invention and feature will become clearer by the detailed description below in conjunction with accompanying drawing, wherein:
Fig. 1 is that wherein, mainframe has been fixed in the cabin according to the stereogram of the part in the cabin that is used for wind power generating set of the present invention;
Fig. 2 is and the similar stereogram of Fig. 1 that wherein, the part wall is removed;
Fig. 3 is the front view in cabin shown in Figure 1;
Fig. 4 A is the zoomed-in view of circled part A among Fig. 3;
Fig. 4 B is the zoomed-in view of circled part B among Fig. 3;
Fig. 5 be with Fig. 1 in the stereogram of mainframe;
Fig. 6 A is the end elevation according to support beam of the present invention; And
Fig. 6 B is the stereogram according to support beam of the present invention.
Embodiment
Describe in detail according to the cabin 1 that is used for wind power generating set of the present invention below with reference to accompanying drawing.Second sidewall 7 and roof 9 that cabin 1 according to the present invention comprises diapire 3, the first side wall 5, is oppositely arranged with the first side wall 5.Cabin 1 according to the present invention also comprises rear end cover or aft bulkhead 11 and front cover that does not illustrate or front bulkhead.These walls are connected with each other and form the space of hexahedral shape substantially.Certainly, the installation needs according to other parts of wind power generating set can be formed with opening in the relevant position on the wall in cabin 1.Should be understood that, cabin 1 according to the present invention can form with shown in different any other suitable shape of hexahedral shape, for example pentahedron shape or cylindroid shape.
According to the present invention, be provided with the first longitudinal bracing beam 13a and the second longitudinal bracing beam 13b with the internal surface of the connecting part of the first side wall 5 and second sidewall 7 respectively at diapire 3, diapire 3 and the first side wall 5 are fixed on the first longitudinal bracing beam 13a by the fastening piece such as bolt or rivet etc. respectively, the diapire 3 and second sidewall 7 are fixed on the second longitudinal bracing beam 13b by the fastening piece such as bolt or rivet etc. respectively, thereby diapire 3 and the first side wall 5 and second sidewall 7 are linked together securely.Similarly, be provided with the 3rd longitudinal bracing beam 13c and the 4th longitudinal bracing beam 13d with the internal surface of the connecting part of the first side wall 5 and second sidewall 7 respectively at roof 9, roof 9 and the first side wall 5 are fixed on the 3rd longitudinal bracing beam 13c by the fastening piece such as bolt or rivet etc. respectively, the roof 9 and second sidewall 7 are fixed on the 4th longitudinal bracing beam 13d by the fastening piece such as bolt or rivet etc. respectively, thereby roof 9 and the first side wall 5 and second sidewall 7 are linked together securely.
In order to reduce the influence of wind-force to cabin 1, the outer surface in cabin 1 is usually designed to streamlined, and diapire 3, the first side wall 5, second sidewall 7 and roof 9 are designed to curved shape interconnecting the position at least.In order to ensure between the first longitudinal bracing beam 13a and diapire 3 and the first side wall 5, between the second longitudinal bracing beam 13b and the diapire 3 and second sidewall 7, between the 3rd longitudinal bracing beam 13c and roof 9 and the first side wall 5 and between the 4th longitudinal bracing beam 13d and the roof 9 and second sidewall 7 closely and firm engagement, the part that each longitudinal bracing beam contacts with wall has the curved shape that the internal surface curved shape with corresponding connecting part is complementary, thereby makes each longitudinal bracing beam contact ordinatedly with corresponding wall appropriateness.The cross section of longitudinal bracing beam can be required Any shape.For weight reduction and guarantee join strength, the longitudinal bracing beam is hollow preferably.
Fig. 4 A has shown that specifically roof 9 and the first side wall 5 interconnect by the 3rd longitudinal bracing beam 13c.The crooked inner surface of the first side wall 5 upper ends is close to the 3rd longitudinal bracing beam 13c and is fixed on the 3rd longitudinal bracing beam 13c by the fastening piece (such as bolt or rivet etc.) that passes the first side wall 5 and the 3rd longitudinal bracing beam 13c.Roof 9 and the first side wall 5 splicings, its crooked inner surface also is close to the 3rd longitudinal bracing beam 13c and is fixed on the 3rd longitudinal bracing beam 13c by the fastening piece that passes roof 9 and the 3rd longitudinal bracing beam 13c.In order to make operator when assembling the cabin, can carry out operation and need not enter engine room inside, preferably on the 3rd longitudinal bracing beam 13c, a plurality of tapped holes 15 be set in nacelle exterior.Having internal thread and externally threaded hollow sleeve 17 can be screwed in the tapped hole 15 on the 3rd longitudinal bracing beam 13c, by roof 9 and the first side wall 5 being fixed on the 3rd longitudinal bracing beam 13c in the internal thread that bolt is screwed into hollow sleeve 17.Certainly, hollow sleeve 17 can not have outside thread yet, and it is fixed on the 3rd longitudinal bracing beam by riveted joint or alternate manner.In order to prevent that dirts such as sand and dust from entering in the cabin, roof 9 preferably partly is overlapped on the first side wall 5.Because roof 9 partly is overlapped on the first side wall 5, is formed with the gap like this between the curved surface 13c ' of roof 9 and the 3rd longitudinal bracing beam 13c, between roof 9 and the 3rd longitudinal bracing beam 13c liner strip 19 is set for this reason.Also be provided with a plurality of tapped holes on the liner strip 19.At first, by part tapped hole and the bolt among the 3rd longitudinal bracing beam 13c that is screwed on the liner strip 19 liner strip 19 is fixed on the 3rd longitudinal bracing beam 13c, by the bolt that is screwed in another part tapped hole on roof 9 and the liner strip 19 roof 9 is fixed on the liner strip 19 subsequently, thereby roof 9 is fixed on the 3rd longitudinal bracing beam 13c.
Preferably, roof 9 and the first side wall 5 also can be made up of a plurality of transverse top wall part 9a and a plurality of horizontal the first side wall part 5a, thereby are convenient to transportation more.Transverse top wall part 9a is formed with inside vertically extending flange 9b at its transverse edge, and adjacent transverse top wall portion 9a is closely linked together by inside vertically extending flange 9b.Similarly, laterally the first side wall part 5a is formed with inside vertically extending flange 5b at its transverse edge, and adjacent transverse the first side wall part 5a is closely linked together by inside vertically extending flange 5b.
The connection of roof 9, second sidewall 7 and the 4th longitudinal bracing beam 13d can realize with the above-mentioned same way as that is connected of roof 9, the first side wall 5 and the 3rd longitudinal bracing beam 13c.
Fig. 4 B has shown that specifically diapire 3 and the first side wall 5 interconnect by the first longitudinal bracing beam 13a.The crooked inner surface of the first side wall 5 lower ends is close to the first longitudinal bracing beam 13a and is fixed on the first longitudinal bracing beam 13a by the fastening piece that passes the first side wall 5 and the first longitudinal bracing beam 13a.Diapire 3 and the first side wall 5 splicings, its crooked inner surface also is close to the first longitudinal bracing beam 13a and is fixed on the first longitudinal bracing beam 13a by the fastening piece that passes the diapire 3 and the first longitudinal bracing beam 13a.Preferably, when assembling the cabin, can carry out operation and need not enter engine room inside, can on the first longitudinal bracing beam, a plurality of tapped holes be set in nacelle exterior in order to make operator.Having internal thread and externally threaded hollow sleeve can be screwed in the tapped hole on the first longitudinal bracing beam, by diapire and the first side wall being fixed on the first longitudinal bracing beam in the internal thread that bolt is screwed into hollow sleeve.In order to prevent that dirts such as sand and dust from entering in the cabin, the first side wall 5 can partly be overlapped on the diapire 3.
Preferably, diapire 3 also can be made up of a plurality of horizontal bottom wall portion 3a, thereby is convenient to transportation more.Laterally bottom wall portion 3a is formed with inside vertically extending flange at its transverse edge, and adjacent transverse bottom wall portion 3a is closely linked together by inside vertically extending flange.
The connection of diapire 3, second sidewall 7 and the second longitudinal bracing beam 13b can realize with the above-mentioned same way as that is connected of diapire 3, the first side wall 5 and the first longitudinal bracing beam 13a.
Similarly, second sidewall 7 also can be made up of a plurality of horizontal second wall portion 7a, thereby is convenient to transportation more.The horizontal second wall portion 7a is formed with inside vertically extending flange at its transverse edge, and the adjacent transverse second wall portion 7a is closely linked together by inside vertically extending flange.
Aft bulkhead and front bulkhead can be installed on the cabin body that is formed by diapire, the first side wall, second sidewall and roof in a known manner in the art.
Well known in the artly be that 1 inside is provided with the mainframe 21 of the primary clustering that is used to support wind power generating set in the cabin.Fig. 5 has shown mainframe 21 with stereogram signal property ground.Be fixed with a plurality of carriages 23 respectively in mainframe 21 upper and lowers, be used for mainframe 21 is fixed to cabin 1.As required, each carriage can be difformity.For the ease of being connected and making simple in structurely of mainframe 21 and cabin 1, longitudinal bracing beam 13 according to the present invention also is formed with at least one longitudinal socket 25.Longitudinal bracing beam 13 demonstrations among Fig. 6 A and the 6B are formed with two longitudinal sockets 25.The connection strap that is threaded the hole can and be maintained in the longitudinal socket from the longitudinal end insertion longitudinal socket of longitudinal bracing beam.In addition, longitudinal bracing beam 13 longitudinally is formed with projection 13 ' in its hollow space that contacts with machinery space bulkhead one side according to the preferred embodiment of the invention, but also can longitudinally not be formed with projection or all longitudinally be formed with projection in its hollow space both sides that contact with machinery space bulkhead in its hollow space that contacts with machinery space bulkhead one side.
Fig. 4 A has shown that the connection strap 27 that is threaded the hole is from the longitudinal end insertion longitudinal socket 25 of the 3rd longitudinal bracing beam 13c.The shape of longitudinal socket 25 can guarantee that connection strap 27 is maintained in the longitudinal socket 25 and can come off.Bolt 29 passes the carriage 23 that is arranged on mainframe 21 tops and is screwed in the tapped hole of the connection strap 27 that remains in the longitudinal socket 25, thereby mainframe 21 and the 3rd longitudinal bracing beam 13c are coupled together.Can in a similar manner mainframe 21 and the 4th longitudinal bracing beam 13d be coupled together.
Fig. 4 B has shown that the connection strap 27 that is threaded the hole inserts the longitudinal socket 25 and is maintained in the longitudinal socket 25 from the longitudinal end of the first longitudinal bracing beam 13a.Bolt 29 passes the carriage 23 that is arranged on mainframe 21 bottoms and is screwed in the tapped hole of the connection strap 27 that remains in the longitudinal socket 25, thereby the mainframe 21 and the first longitudinal bracing beam 13a are coupled together.Can in a similar manner the mainframe 21 and the second longitudinal bracing beam 13b be coupled together.
In the manner described above, mainframe 21 can be fixed in the cabin 1.In the reality, can be as required, cabin 1 is assembled after being fixed to longitudinal bracing beam 13 on the mainframe 21 again by elder generation.
The present invention has below been described in conjunction with the preferred embodiments.But it should be understood that the present invention is not limited to above preferred embodiment.Under the situation that does not break away from the scope of protection of present invention, can carry out various improvement to the present invention.In addition, support beam can not be longitudinally, for example is used for the cross-brace beam that connects between the transverse wall.Support beam also can be arranged on the internal surface place of the connecting part of non-bending.In a preferred embodiment, the internal surface of the connecting part of all adjacent two walls in diapire, the first side wall, second sidewall and the roof all is provided with the longitudinal bracing beam, but also can be only therein the internal surface of the connecting part of some adjacent two walls all be provided with the longitudinal bracing beam.All these improvement all drop within the protection domain of the present invention.
Claims (19)
1. cabin that is used for wind power generating set, described cabin comprises a plurality of walls, described a plurality of wall is connected with each other to form the engine room inside space, it is characterized in that, the internal surface of the connecting part of at least one group of adjacent wall in described a plurality of walls is provided with support beam, and the part that described support beam contacts with adjacent wall has the shape that the inner surface configuration with the connecting part is complementary.
2. the cabin that is used for wind power generating set as claimed in claim 1, it is characterized in that, the internal surface of the connecting part of described at least one group of adjacent wall is curved shape, and the part that described support beam contacts with adjacent wall has the curved shape that the internal surface curved shape with corresponding connecting part is complementary.
3. the cabin that is used for wind power generating set as claimed in claim 1 is characterized in that, described at least one group of adjacent wall is vertical wall, and described support beam is the longitudinal bracing beam.
4. the cabin that is used for wind power generating set as claimed in claim 1 is characterized in that described support beam is a hollow.
5. the cabin that is used for wind power generating set as claimed in claim 1, it is characterized in that, described at least one group of adjacent wall is made up of a plurality of wall sections respectively, each wall section is formed with inside vertically extending flange at its edge, the adjacent wall part is closely linked together by inside vertically extending flange.
6. the cabin that is used for wind power generating set as claimed in claim 1 is characterized in that, described support beam is formed with and is used for keeping therein adeciduate at least one slot of connection strap.
7. the cabin that is used for wind power generating set as claimed in claim 1, it is characterized in that, second sidewall, roof, aft bulkhead and front bulkhead that described a plurality of wall comprises diapire, the first side wall, is oppositely arranged with the first side wall, wherein, the internal surface of the connecting part of adjacent two walls in diapire, the first side wall, second sidewall and the roof is provided with the longitudinal bracing beam, and described adjacent two walls are fixed on the described longitudinal bracing beam.
8. the cabin that is used for wind power generating set as claimed in claim 7 is characterized in that, the part that described longitudinal bracing beam contacts with described adjacent two walls has the curved shape that the internal surface curved shape with described connecting part is complementary.
9. the cabin that is used for wind power generating set as claimed in claim 7 is characterized in that, described longitudinal bracing beam is a hollow.
10. the cabin that is used for wind power generating set as claimed in claim 7 is characterized in that, described adjacent two walls are spliced together.
11. the cabin that is used for wind power generating set as claimed in claim 7 is characterized in that, described longitudinal bracing beam is provided with the hollow sleeve that has internal thread, is screwed in the described hollow sleeve so that will fix the bolt of described adjacent two walls.
12. the cabin that is used for wind power generating set as claimed in claim 7 is characterized in that, described roof partly is overlapped on the described the first side wall and second sidewall.
13. the cabin that is used for wind power generating set as claimed in claim 12 is characterized in that, is provided with liner strip between described roof and the described longitudinal bracing beam.
14. the cabin that is used for wind power generating set as claimed in claim 13 is characterized in that described liner strip is provided with a plurality of tapped holes.
15. the cabin that is used for wind power generating set as claimed in claim 7 is characterized in that, at least one wall in described diapire, the first side wall, second sidewall and the roof is grouped into by a plurality of transverse wall portion.
16. the cabin that is used for wind power generating set as claimed in claim 15, it is characterized in that, described lateral wall portion is formed with inside vertically extending flange at its transverse edge, and the adjacent transverse wall section is closely linked together by inside vertically extending flange.
17. the cabin that is used for wind power generating set as claimed in claim 7 is characterized in that, described aft bulkhead and front bulkhead are installed on the cabin body that is formed by diapire, the first side wall, second sidewall and roof.
18. the cabin that is used for wind power generating set as claimed in claim 7 is characterized in that, described longitudinal bracing beam is formed with at least one longitudinal socket, and the connection strap that is threaded the hole can be maintained in the described longitudinal socket and not come off.
19. the cabin that is used for wind power generating set as claimed in claim 9 is characterized in that, described longitudinal bracing beam longitudinally is formed with projection at least one side of the hollow space that it contacts with described adjacent two walls.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009102245197A CN102062058A (en) | 2009-11-17 | 2009-11-17 | Engine room for wind generating set |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009102245197A CN102062058A (en) | 2009-11-17 | 2009-11-17 | Engine room for wind generating set |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102062058A true CN102062058A (en) | 2011-05-18 |
Family
ID=43997497
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009102245197A Pending CN102062058A (en) | 2009-11-17 | 2009-11-17 | Engine room for wind generating set |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102062058A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112943564A (en) * | 2019-11-26 | 2021-06-11 | 新疆金风科技股份有限公司 | Cabin cover and wind generating set |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4209892A (en) * | 1978-08-18 | 1980-07-01 | The Budd Company | Method of manufacturing, packaging and assembling a railway car |
| DE102006001931A1 (en) * | 2006-01-14 | 2007-07-19 | Nordex Energy Gmbh | Housing for gondola of wind energy plant has frame assembled with wall elements so that interior space thereof is defined at least in part by curved faces for better stability |
| WO2007132408A2 (en) * | 2006-05-11 | 2007-11-22 | Jupiter Plast A/S | Modular construction of a nacelle |
| CN201621019U (en) * | 2009-11-17 | 2010-11-03 | 维斯塔斯风力系统集团公司 | Engine room for wind generating set |
-
2009
- 2009-11-17 CN CN2009102245197A patent/CN102062058A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4209892A (en) * | 1978-08-18 | 1980-07-01 | The Budd Company | Method of manufacturing, packaging and assembling a railway car |
| DE102006001931A1 (en) * | 2006-01-14 | 2007-07-19 | Nordex Energy Gmbh | Housing for gondola of wind energy plant has frame assembled with wall elements so that interior space thereof is defined at least in part by curved faces for better stability |
| WO2007132408A2 (en) * | 2006-05-11 | 2007-11-22 | Jupiter Plast A/S | Modular construction of a nacelle |
| CN201621019U (en) * | 2009-11-17 | 2010-11-03 | 维斯塔斯风力系统集团公司 | Engine room for wind generating set |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112943564A (en) * | 2019-11-26 | 2021-06-11 | 新疆金风科技股份有限公司 | Cabin cover and wind generating set |
| CN112943564B (en) * | 2019-11-26 | 2023-04-21 | 新疆金风科技股份有限公司 | Cabin cover and wind generating set |
| US11959462B2 (en) | 2019-11-26 | 2024-04-16 | Goldwind Science & Technology Co., Ltd. | Cabin cover and wind turbine generator set |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US8591186B2 (en) | Nacelle for wind turbine | |
| CN201400218Y (en) | Vehicle chassis | |
| KR101650973B1 (en) | Photovoltaic assemblies and methods for transporting | |
| US20040124711A1 (en) | Mobile power system | |
| US8875394B2 (en) | Solar energy collecting modules and method for assembling the same | |
| CN103474491A (en) | High-integration-level folding-type photovoltaic array | |
| CN101338726A (en) | Low cost rail-transportable wind turbine tower | |
| CN108068602A (en) | The cell-support structure of vehicle body | |
| CN102628429B (en) | For transporting and/or promote transport structure and the method for high-rating generator | |
| DK202000034Y3 (en) | Solar Carport | |
| CN105966467A (en) | Automobile and threshold beam thereof | |
| CN201621019U (en) | Engine room for wind generating set | |
| CN102717899A (en) | Venus probe configuration | |
| CN102062058A (en) | Engine room for wind generating set | |
| CN212605879U (en) | Rocket ejection type thrust cone connecting angle box structure | |
| CN205089530U (en) | Tapered multilateral burst is bent molding composition and is inserted connection mode wind -powered electricity generation pylon | |
| CN210526879U (en) | Satellite structure suitable for occultation detection | |
| CN102135076B (en) | Wind power generation tower sheathing transportation device | |
| CN105035360A (en) | Cabin-segmentation type separable platform configuration based on four-point connection | |
| CN212386951U (en) | Fixed frock of tower node transportation mixes | |
| CN205203870U (en) | Angle coupling assembling of container and have its container modularization building | |
| CN201953581U (en) | Sleeved conveying device for wind power tower | |
| CN204110150U (en) | A kind of integral electric car chassis | |
| CN2928707Y (en) | Transport container and its angle part | |
| CN201918398U (en) | Photovoltaic system and mounting device thereof |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20110518 |