CN209617522U - Vertical flame-proof explosion-proof fuel tank for unmanned helicopter - Google Patents

Vertical flame-proof explosion-proof fuel tank for unmanned helicopter Download PDF

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Publication number
CN209617522U
CN209617522U CN201920132372.8U CN201920132372U CN209617522U CN 209617522 U CN209617522 U CN 209617522U CN 201920132372 U CN201920132372 U CN 201920132372U CN 209617522 U CN209617522 U CN 209617522U
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China
Prior art keywords
shell
aluminium alloy
oil
aramid fiber
glass liner
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Active
Application number
CN201920132372.8U
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Chinese (zh)
Inventor
祁正岩
李树森
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Anhui Xinglong Steel Structure Co.,Ltd.
Original Assignee
Qianmei Aviation Technology Xingtai Co Ltd
Priority date (The priority date 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 date listed.)
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Priority to CN201920132372.8U priority Critical patent/CN209617522U/en
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Publication of CN209617522U publication Critical patent/CN209617522U/en
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Abstract

Vertical flame-proof explosion-proof fuel tank for unmanned helicopter is related to a kind of fuel tank applied on unmanned helicopter.It is mainly to solve the problem of that the fuel tank fuel easy to damage on existing unmanned helicopter is easily overflowed and designed.It includes shell, there is shell in aluminium alloy in aramid fiber shell, glass liner is equipped in aluminium alloy in shell, filled with carbon dioxide gas between shell in aramid fiber shell and aluminium alloy, fire retardant is filled in aluminium alloy between shell and glass liner, software oil sac is in glass liner, oil resistant sponge is filled in software oil sac, valve is installed on the disengaging oil pipe of software oil sac, valve is equipped with oil inlet and oil outlet, air inlet-outlet pipe is equipped at the top of glass liner, air inlet-outlet pipe shell, aramid fiber shell from aluminium alloy stretch out.Advantage is to be hardly damaged, and fuel is not spilt over.

Description

Vertical flame-proof explosion-proof fuel tank for unmanned helicopter
Technical field:
The utility model relates to a kind of fuel tanks applied on unmanned helicopter.
Background technique:
The existing cabinet for applying the fuel tank on unmanned helicopter is single layer structure, and fuel is in cabinet.This combustion Hopper is easy to damage, once damage fuel leakage can cause danger.In addition fuel rocks easily in fuel tank when helicopter flight It overflows.
Summary of the invention:
The technical problem to be solved by the utility model is to provide a kind of fuel not to overflow, and is hardly damaged, and can guarantee peace The complete vertical flame-proof explosion-proof fuel tank for unmanned helicopter.
Above-mentioned purpose is achieved in that it includes aramid fiber shell, is equipped with shell in aluminium alloy in aramid fiber shell, There are gap between shell in aramid fiber shell and aluminium alloy, glass liner, shell and glass in aluminium alloy are equipped in aluminium alloy in shell There are gap between fine liner, filled with carbon dioxide gas between shell in aramid fiber shell and aluminium alloy, in aluminium alloy shell and Fire retardant or carbon tetrachloride are filled between glass liner, software oil sac is in glass liner, filled with resistance in software oil sac Oily sponge, valve is equipped on the disengaging oil pipe of software oil sac, and valve is equipped with oil inlet and oil outlet, sets at the top of glass liner There is air inlet-outlet pipe, air inlet-outlet pipe shell, aramid fiber shell from aluminium alloy stretch out.Fuel is in software oil sac.
The utility model has the advantages that: the cabinet of this fuel tank is multilayered structure, is hardly damaged.Due to outside aramid fiber Carbon dioxide is filled in shell and aluminium alloy between shell, fire retardant is filled between shell in aluminium alloy and glass liner, works as oil When case is breakdown, fire retardant and carbon dioxide can play the role of preventing burning, isolation air, and helicopter is prevented to be burned out.By In by fuel, in software oil sac, software oil sac is interior equipped with oil resistant sponge, so can prevent fuel from overflowing.
Detailed description of the invention:
Fig. 1 is the structural schematic diagram of the utility model.
Specific embodiment:
Referring to Fig.1, it includes aramid fiber shell 1, is equipped with shell 2 in aluminium alloy in aramid fiber shell, outside aramid fiber There are gap between shell in shell and aluminium alloy, it is equipped with glass liner 3 in aluminium alloy in shell, in aluminium alloy between shell and glass liner There are gap, filled with carbon dioxide gas between shell in aramid fiber shell and aluminium alloy, in aluminium alloy shell and glass liner it Between be filled with fire retardant 4 or carbon tetrachloride, software oil sac 5 is filled with oil resistant sponge 6 in the glass liner in software oil sac, Valve 8 is installed, valve is equipped with oil inlet 9 and oil outlet 10, is equipped at the top of glass liner on the disengaging oil pipe 7 of software oil sac Air inlet-outlet pipe 11, air inlet-outlet pipe shell, aramid fiber shell from aluminium alloy stretch out.Fuel is in software oil sac.

Claims (1)

1. being used for the vertical flame-proof explosion-proof fuel tank of unmanned helicopter, it is characterized in that: including aramid fiber shell (1), aramid fiber is fine It ties up and is equipped with shell (2) in aluminium alloy in shell, there are gap between shell in aramid fiber shell and aluminium alloy, set in shell in aluminium alloy Have glass liner (3), there are gap between shell and glass liner in aluminium alloy, is filled between shell in aramid fiber shell and aluminium alloy There is carbon dioxide gas, be filled with fire retardant (4) between shell and glass liner in aluminium alloy, software oil sac (5) is in glass In gallbladder, oil resistant sponge (6) are filled in software oil sac, are equipped with valve (8) on the disengaging oil pipe (7) of software oil sac, on valve Equipped with oil inlet (9) and oil outlet (10), be equipped with air inlet-outlet pipe (11) at the top of glass liner, air inlet-outlet pipe from aluminium alloy shell, Aramid fiber shell stretches out.
CN201920132372.8U 2019-01-25 2019-01-25 Vertical flame-proof explosion-proof fuel tank for unmanned helicopter Active CN209617522U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201920132372.8U CN209617522U (en) 2019-01-25 2019-01-25 Vertical flame-proof explosion-proof fuel tank for unmanned helicopter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201920132372.8U CN209617522U (en) 2019-01-25 2019-01-25 Vertical flame-proof explosion-proof fuel tank for unmanned helicopter

Publications (1)

Publication Number Publication Date
CN209617522U true CN209617522U (en) 2019-11-12

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201920132372.8U Active CN209617522U (en) 2019-01-25 2019-01-25 Vertical flame-proof explosion-proof fuel tank for unmanned helicopter

Country Status (1)

Country Link
CN (1) CN209617522U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112849419A (en) * 2021-04-23 2021-05-28 西安羚控电子科技有限公司 Complete oxygen isolation fuel tank for airplane

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112849419A (en) * 2021-04-23 2021-05-28 西安羚控电子科技有限公司 Complete oxygen isolation fuel tank for airplane
CN112849419B (en) * 2021-04-23 2021-08-03 西安羚控电子科技有限公司 Complete oxygen isolation fuel tank for airplane

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GR01 Patent grant
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TR01 Transfer of patent right

Effective date of registration: 20210827

Address after: 231323 west side of Qiantai Road, Hengshan Town, Huoshan County, Lu'an City, Anhui Province

Patentee after: Anhui Xinglong Steel Structure Co.,Ltd.

Address before: 054000 room 602, building 7, science and Technology Park (Xingtai) of Hebei University of technology, No. 1889, Zhongxing East Street, Qiaodong District, Xingtai City, Hebei Province

Patentee before: QIANMEI AVIATION TECHNOLOGY XINGTAI Co.,Ltd.