CN204527666U - Helicopter oil-cooled generator driven equipment - Google Patents
Helicopter oil-cooled generator driven equipment Download PDFInfo
- Publication number
- CN204527666U CN204527666U CN201520145706.7U CN201520145706U CN204527666U CN 204527666 U CN204527666 U CN 204527666U CN 201520145706 U CN201520145706 U CN 201520145706U CN 204527666 U CN204527666 U CN 204527666U
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- China
- Prior art keywords
- oil
- lubricating oil
- oil feed
- pump
- carrying cabinet
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- 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
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Abstract
The utility model belongs to ground power supply equipment technical field, particularly relates to a kind of helicopter oil-cooled generator driven equipment.Helicopter oil-cooled generator driven equipment, it is characterized in that, comprise: variable high-speed electric motor (3), operator's station (4), frequency converter (6), lubricating oil cooler (7), dump pump (8), cooling lubricating oil case (9), oil feed pump (12) and carrying cabinet (10), this driven equipment volume is little, lightweight, noise is low, conveniently moving.
Description
Technical field
The invention belongs to ground power supply equipment technical field, particularly relate to a kind of helicopter oil-cooled generator driven equipment.
Background technology
The existing oil-cooled generator driven equipment of helicopter industry be divided into driven equipment and and oil coolant source device two parts, two parts are separate.
The dragging motor of driven equipment adopts low-speed motor, and electrical motor is connected with oil-cooled generator by raising speed gear case.The shortcoming of this project organization is that equipment volume is comparatively large, Heavy Weight; Equipment vibrations are large, need equipment to fix on the ground during use; Noise of equipment is large, produces larger noise emission during use.
Oil coolant source device is connected with oil-cooled generator, adopts gravity circuit to reclaim cooling lubricating oil.The shortcoming of this project organization is that cooling lubricating oil flow is low, and cooling performance is poor, needs more cooling lubricating oil, causes equipment volume to increase.
Summary of the invention
The object of invention
Limit by helicopter general assembly site environment, volume, the noise of driven equipment should be little as far as possible, and must accomplish can by Manual-pushing, therefore prior art design driven equipment and not to be suitable for helicopter general assembly on-the-spot, must be applicable to according to helicopter general assembly test, environmental quality development the helicopter oil-cooled generator driven equipment that assembly shop uses.
The technical scheme of invention
Helicopter oil-cooled generator driven equipment, comprising: variable high-speed electric motor 3, operator's station 4, frequency converter 6, lubricating oil cooler 7, dump pump 8, cooling lubricating oil case 9, oil feed pump 12 and carrying cabinet 10, wherein,
Carrying cabinet 10 is three-decker, and 4 BOGEY WHEELs are equipped with in bottom;
Variable high-speed electric motor 3 and operator's station 4 are arranged on the upper strata of carrying cabinet 10; Frequency converter 6 and lubricating oil cooler 7 are arranged on and carry cabinet 10 middle level; Dump pump 8, cooling lubricating oil case 9 and oil feed pump 12 are arranged on carrying cabinet 10 lower floor.
Frequency converter 6 is connected with variable high-speed electric motor 3 with operator's station 4 respectively by transit cable 5, and variable high-speed electric motor 3 and connector assembly 2 are bolted, and connector assembly 2 is connected with by measured motor 1 physical construction by clip; Be connected with lubricating oil cooler 7 with oil feed pump 12 by oil feed line 11 by the cooling hydraulic fluid port of measured motor 1; Lubricating oil cooler 7 is connected with dump pump 8 by oil feed line 11; Dump pump 8 is connected with cooling lubricating oil case 9 by oil feed line 11, and cooling lubricating oil case 9 is connected with oil feed pump 12 by oil feed line 11.
There is push and pull bar described carrying cabinet 10 side.
Described carrying cabinet 10 also has 4 fixing lower margins, temporary fixed for equipment.
To be operating personal control frequency converter 6 by operator's station 4 drives variable high-speed electric motor 3 to drive to be worked by measured motor 1 for the principle of work of equipment, cooling lubricating oil is transported to by measured motor 1 from cooling lubricating oil case 9 by oil feed line 11 by oil feed pump 12, cooling lubricating oil is extracted out from by measured motor 1 by oil feed line 11 by dump pump 8, is transported in cooling lubricating oil case 9 after lubricating oil cools by lubricating oil cooler 7.
The effect of invention
This driven equipment volume is little, lightweight, noise is low, conveniently moving.
Accompanying drawing explanation
Accompanying drawing 1 is structural scheme of mechanism of the present invention.
Detailed description of the invention
Helicopter oil-cooled generator driven equipment, comprising: variable high-speed electric motor 3, operator's station 4, frequency converter 6, lubricating oil cooler 7, dump pump 8, cooling lubricating oil case 9, oil feed pump 12 and carrying cabinet 10, wherein,
Carrying cabinet 10 is three-decker, and 4 BOGEY WHEELs are equipped with in bottom;
Variable high-speed electric motor 3 and operator's station 4 are arranged on the upper strata of carrying cabinet 10; Frequency converter 6 and lubricating oil cooler 7 are arranged on and carry cabinet 10 middle level; Dump pump 8, cooling lubricating oil case 9 and oil feed pump 12 are arranged on carrying cabinet 10 lower floor.
Frequency converter 6 is connected with variable high-speed electric motor 3 with operator's station 4 respectively by transit cable 5, and variable high-speed electric motor 3 and connector assembly 2 are bolted, and connector assembly 2 is connected with by measured motor 1 physical construction by clip; Be connected with lubricating oil cooler 7 with oil feed pump 12 by oil feed line 11 by the cooling hydraulic fluid port of measured motor 1; Lubricating oil cooler 7 is connected with dump pump 8 by oil feed line 11; Dump pump 8 is connected with cooling lubricating oil case 9 by oil feed line 11, and cooling lubricating oil case 9 is connected with oil feed pump 12 by oil feed line 11.
There is push and pull bar described carrying cabinet 10 side.
Described carrying cabinet 10 also has 4 fixing lower margins, temporary fixed for equipment.
To be operating personal control frequency converter 6 by operator's station 4 drives variable high-speed electric motor 3 to drive to be worked by measured motor 1 for the principle of work of equipment, cooling lubricating oil is transported to by measured motor 1 from cooling lubricating oil case 9 by oil feed line 11 by oil feed pump 12, cooling lubricating oil is extracted out from by measured motor 1 by oil feed line 11 by dump pump 8, is transported in cooling lubricating oil case 9 after lubricating oil cools by lubricating oil cooler 7
Breathing out the source of AC dynamic test stand flying to use is exactly by this driven equipment, and it adopts three layers of carrying cabinet as equipment body, and carrying cabinet is equipped with 4 BOGEY WHEELs and push and pull bar, facilitates equipment moving, and carrying cabinet also has 4 fixing lower margins, fixes for equipment.
Variable high-speed electric motor, operator's station and frequency converter all adopt the auxiliary products of Siemens, and rotating speed can reach 14500r/min, and oil feed pump and dump pump adopt adjustable design, can adjustment System flow and pressure by the parameter of adjustment structure pump.
Claims (3)
1. helicopter oil-cooled generator driven equipment, it is characterized in that, comprise: variable high-speed electric motor (3), operator's station (4), frequency converter (6), lubricating oil cooler (7), dump pump (8), cooling lubricating oil case (9), oil feed pump (12) and carrying cabinet (10), wherein
Carrying cabinet (10) is three-decker, bottom is equipped with (4) individual BOGEY WHEEL;
Variable high-speed electric motor (3) and operator's station (4) are arranged on the upper strata of carrying cabinet (10); Frequency converter (6) and lubricating oil cooler (7) are arranged on and carry cabinet (10) middle level; Dump pump (8), cooling lubricating oil case (9) and oil feed pump (12) are arranged on carrying cabinet (10) lower floor;
Frequency converter (6) is connected with variable high-speed electric motor (3) with operator's station (4) respectively by transit cable (5), variable high-speed electric motor (3) and connector assembly (2) are bolted, and connector assembly (2) is connected with by measured motor (1) physical construction by clip; Be connected with lubricating oil cooler (7) with oil feed pump (12) by oil feed line (11) by the cooling hydraulic fluid port of measured motor (1); Lubricating oil cooler (7) is connected with dump pump (8) by oil feed line (11); Dump pump (8) is connected with cooling lubricating oil case (9) by oil feed line (11), and cooling lubricating oil case (9) is connected with oil feed pump (12) by oil feed line (11).
2. helicopter oil-cooled generator driven equipment as claimed in claim 1, it is characterized in that, there is push and pull bar described carrying cabinet (10) side.
3. helicopter oil-cooled generator driven equipment as claimed in claim 1, is characterized in that, described carrying cabinet (10) also has 4 fixing lower margins, temporary fixed for equipment.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520145706.7U CN204527666U (en) | 2015-03-13 | 2015-03-13 | Helicopter oil-cooled generator driven equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520145706.7U CN204527666U (en) | 2015-03-13 | 2015-03-13 | Helicopter oil-cooled generator driven equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204527666U true CN204527666U (en) | 2015-08-05 |
Family
ID=53741694
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520145706.7U Expired - Fee Related CN204527666U (en) | 2015-03-13 | 2015-03-13 | Helicopter oil-cooled generator driven equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204527666U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107765193A (en) * | 2016-08-23 | 2018-03-06 | 哈尔滨飞机工业集团有限责任公司 | A kind of high power system general assembly test method |
-
2015
- 2015-03-13 CN CN201520145706.7U patent/CN204527666U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107765193A (en) * | 2016-08-23 | 2018-03-06 | 哈尔滨飞机工业集团有限责任公司 | A kind of high power system general assembly test method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20170606 Address after: 150066 Heilongjiang Province, Harbin city Youxie Street Pingfang District No. 15 Patentee after: Harbin Hafei Aviation Industry Co. Ltd. Address before: 150066 Heilongjiang Province, Harbin city Youxie Street Pingfang District No. 15 Patentee before: Harbin Aircraft Industrial (Group) Co., Ltd. |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150805 Termination date: 20180313 |