CN111232231B - Wing built-in aviation oil tank pressurizing device - Google Patents
Wing built-in aviation oil tank pressurizing device Download PDFInfo
- Publication number
- CN111232231B CN111232231B CN202010081306.XA CN202010081306A CN111232231B CN 111232231 B CN111232231 B CN 111232231B CN 202010081306 A CN202010081306 A CN 202010081306A CN 111232231 B CN111232231 B CN 111232231B
- Authority
- CN
- China
- Prior art keywords
- inner cavity
- pipe
- pressurizing
- aviation
- fuel tank
- 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
- 238000003780 insertion Methods 0.000 claims abstract description 40
- 230000037431 insertion Effects 0.000 claims abstract description 40
- 239000002828 fuel tank Substances 0.000 claims abstract description 22
- 239000007788 liquid Substances 0.000 claims description 5
- 230000003139 buffering effect Effects 0.000 abstract description 7
- 238000000034 method Methods 0.000 abstract description 7
- 238000009434 installation Methods 0.000 abstract description 4
- 244000309464 bull Species 0.000 description 5
- 239000012530 fluid Substances 0.000 description 4
- 238000007789 sealing Methods 0.000 description 4
- 238000004891 communication Methods 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000010992 reflux Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000001502 supplementing effect Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/005—Accessories not provided for in the groups B64D37/02 - B64D37/28
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
- B64D37/06—Constructional adaptations thereof
- B64D37/10—Constructional adaptations thereof to facilitate fuel pressurisation
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/32—Safety measures not otherwise provided for, e.g. preventing explosive conditions
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/32—Safety measures not otherwise provided for, e.g. preventing explosive conditions
- B64D2037/325—Fuel tanks with provisions for reduction hydraulic ram shocks due to projectile impacts
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Supply Devices, Intensifiers, Converters, And Telemotors (AREA)
- Loading And Unloading Of Fuel Tanks Or Ships (AREA)
Abstract
Description
Claims (9)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202010081306.XA CN111232231B (en) | 2020-02-06 | 2020-02-06 | Wing built-in aviation oil tank pressurizing device |
CN202011007266.0A CN112124603A (en) | 2020-02-06 | 2020-02-06 | Aviation oil tank pressurization control method suitable for airplane flight |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202010081306.XA CN111232231B (en) | 2020-02-06 | 2020-02-06 | Wing built-in aviation oil tank pressurizing device |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202011007266.0A Division CN112124603A (en) | 2020-02-06 | 2020-02-06 | Aviation oil tank pressurization control method suitable for airplane flight |
Publications (2)
Publication Number | Publication Date |
---|---|
CN111232231A CN111232231A (en) | 2020-06-05 |
CN111232231B true CN111232231B (en) | 2020-12-08 |
Family
ID=70868865
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202011007266.0A Withdrawn CN112124603A (en) | 2020-02-06 | 2020-02-06 | Aviation oil tank pressurization control method suitable for airplane flight |
CN202010081306.XA Active CN111232231B (en) | 2020-02-06 | 2020-02-06 | Wing built-in aviation oil tank pressurizing device |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202011007266.0A Withdrawn CN112124603A (en) | 2020-02-06 | 2020-02-06 | Aviation oil tank pressurization control method suitable for airplane flight |
Country Status (1)
Country | Link |
---|---|
CN (2) | CN112124603A (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114044152B (en) * | 2021-12-17 | 2023-11-28 | 中国航空工业集团公司西安飞机设计研究所 | Bidirectional oil supply balance system and correction method for internal combustion oil tanks of left and right wings of aircraft |
CN115596555B (en) * | 2022-10-26 | 2024-08-23 | 中国船舶集团有限公司第七〇四研究所 | Fuel system for high-balance-precision large-capacity small turbojet engine |
CN116353836B (en) * | 2023-04-19 | 2023-09-29 | 南京儒一航空机械装备有限公司 | Pressure maintaining oil tank for aircraft |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0840394A (en) * | 1994-07-28 | 1996-02-13 | Mitsubishi Heavy Ind Ltd | Fuel transport device of aircraft |
DE4436747C1 (en) * | 1994-10-14 | 1996-05-15 | Daimler Benz Aerospace Airbus | Method for storing fuel in aircraft tank |
CN201350974Y (en) * | 2008-12-23 | 2009-11-25 | 江西洪都航空工业集团有限责任公司 | Oil tank supercharged oil supply device |
CN102192065A (en) * | 2010-03-18 | 2011-09-21 | 上海航新航宇机械技术有限公司 | Device for detecting function of oil fuel booster pump of civil aircraft |
CN106741984B (en) * | 2017-01-03 | 2019-01-29 | 南京航空航天大学 | A kind of system and its working method of catalytic reforming inerting aircraft fuel tank |
CN107954001B (en) * | 2017-12-20 | 2023-07-25 | 南京航空航天大学 | Fireproof device of pressurized nitrogen-making oil tank and working method thereof |
CN109625297A (en) * | 2018-12-11 | 2019-04-16 | 石家庄飞机工业有限责任公司 | A kind of fuel system for Small General Aircraft |
-
2020
- 2020-02-06 CN CN202011007266.0A patent/CN112124603A/en not_active Withdrawn
- 2020-02-06 CN CN202010081306.XA patent/CN111232231B/en active Active
Also Published As
Publication number | Publication date |
---|---|
CN112124603A (en) | 2020-12-25 |
CN111232231A (en) | 2020-06-05 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant | ||
TA01 | Transfer of patent application right |
Effective date of registration: 20201125 Address after: Room 1130, 1 / F, building 7, No. 135 Yanxing Road, Yangyi street, Lucheng District, Wenzhou City, Zhejiang Province Applicant after: Wenzhou gaoweitong Industrial Design Co.,Ltd. Address before: 314500 no.218, Zhongshan East Road, Chongfu Industrial Zone, Tongxiang City, Jiaxing City, Zhejiang Province Applicant before: Chen Zhilin |
|
TA01 | Transfer of patent application right | ||
TR01 | Transfer of patent right |
Effective date of registration: 20211209 Address after: 314500 room 431, 4th floor, building 5, No. 299, Hangfu Road, Chongfu Town, Tongxiang City, Jiaxing City, Zhejiang Province Patentee after: Jiaxing shunkailu Technology Co.,Ltd. Address before: 325000 room 1130, 1st floor, building 7, No. 135, Yanxing Road, Yangyi street, Lucheng District, Wenzhou City, Zhejiang Province Patentee before: Wenzhou gaoweitong Industrial Design Co.,Ltd. |
|
TR01 | Transfer of patent right | ||
TR01 | Transfer of patent right |
Effective date of registration: 20230707 Address after: 1-7-1, No. 16-7, Jinsha River Street, Huanggu District, Shenyang, Liaoning 110031 Patentee after: Wang Yihan Address before: 314500 room 431, 4th floor, building 5, No. 299, Hangfu Road, Chongfu Town, Tongxiang City, Jiaxing City, Zhejiang Province Patentee before: Jiaxing shunkailu Technology Co.,Ltd. |
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TR01 | Transfer of patent right |