CN213743698U - Aircraft engine ignition structure with atomizing nozzle - Google Patents
Aircraft engine ignition structure with atomizing nozzle Download PDFInfo
- Publication number
- CN213743698U CN213743698U CN202022976715.4U CN202022976715U CN213743698U CN 213743698 U CN213743698 U CN 213743698U CN 202022976715 U CN202022976715 U CN 202022976715U CN 213743698 U CN213743698 U CN 213743698U
- Authority
- CN
- China
- Prior art keywords
- ignition
- oil pipe
- combustion chamber
- atomizer
- nozzle
- 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.)
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- 238000002485 combustion reaction Methods 0.000 claims abstract description 51
- 230000005611 electricity Effects 0.000 claims abstract description 6
- 239000000523 sample Substances 0.000 claims description 20
- 230000006698 induction Effects 0.000 claims description 12
- 238000010438 heat treatment Methods 0.000 claims 1
- 239000000446 fuel Substances 0.000 abstract description 18
- 239000003921 oil Substances 0.000 description 46
- 230000001939 inductive effect Effects 0.000 description 8
- 238000002347 injection Methods 0.000 description 3
- 239000007924 injection Substances 0.000 description 3
- 238000007599 discharging Methods 0.000 description 2
- 239000002912 waste gas Substances 0.000 description 2
- 238000000889 atomisation Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 230000008054 signal transmission Effects 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
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- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
Abstract
Description
Claims (4)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN202022976715.4U CN213743698U (en) | 2020-12-08 | 2020-12-08 | Aircraft engine ignition structure with atomizing nozzle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN202022976715.4U CN213743698U (en) | 2020-12-08 | 2020-12-08 | Aircraft engine ignition structure with atomizing nozzle |
Publications (1)
Publication Number | Publication Date |
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CN213743698U true CN213743698U (en) | 2021-07-20 |
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ID=76834428
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN202022976715.4U Active CN213743698U (en) | 2020-12-08 | 2020-12-08 | Aircraft engine ignition structure with atomizing nozzle |
Country Status (1)
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CN (1) | CN213743698U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115493162A (en) * | 2022-09-13 | 2022-12-20 | 保定市玄云涡喷动力设备研发有限公司 | Ignition device of engine |
-
2020
- 2020-12-08 CN CN202022976715.4U patent/CN213743698U/en active Active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115493162A (en) * | 2022-09-13 | 2022-12-20 | 保定市玄云涡喷动力设备研发有限公司 | Ignition device of engine |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant | ||
CP03 | Change of name, title or address |
Address after: No. 66 Jianye East Road, Gaokai District, Baoding City, Hebei Province, 071000 Patentee after: BAODING XUANYUN TURBOJET POWER EQUIPMENT R&D CO.,LTD. Country or region after: China Address before: Block a, building 3, Zhongguancun innovation base, No. 369, Huiyang street, Baoding City, Hebei Province, 071000 Patentee before: BAODING XUANYUN TURBOJET POWER EQUIPMENT R&D CO.,LTD. Country or region before: China |
|
CP03 | Change of name, title or address | ||
PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: An ignition structure for aircraft engines with atomizing nozzles Granted publication date: 20210720 Pledgee: Agricultural Bank of China Limited Baoding Technology Branch Pledgor: BAODING XUANYUN TURBOJET POWER EQUIPMENT R&D CO.,LTD. Registration number: Y2024980028770 |