CN202379300U - Fuel tank of plane refueller - Google Patents

Fuel tank of plane refueller Download PDF

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Publication number
CN202379300U
CN202379300U CN2011205493740U CN201120549374U CN202379300U CN 202379300 U CN202379300 U CN 202379300U CN 2011205493740 U CN2011205493740 U CN 2011205493740U CN 201120549374 U CN201120549374 U CN 201120549374U CN 202379300 U CN202379300 U CN 202379300U
Authority
CN
China
Prior art keywords
tank body
tank
postcentrum
fuel tank
precentrum
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.)
Expired - Fee Related
Application number
CN2011205493740U
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Chinese (zh)
Inventor
杜志远
姜志军
孙东博
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.)
Weihai Guangtai Airport Equipment Co Ltd
Original Assignee
Weihai Guangtai Airport Equipment 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.)
Filing date
Publication date
Application filed by Weihai Guangtai Airport Equipment Co Ltd filed Critical Weihai Guangtai Airport Equipment Co Ltd
Priority to CN2011205493740U priority Critical patent/CN202379300U/en
Application granted granted Critical
Publication of CN202379300U publication Critical patent/CN202379300U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model relates to the technical field of vehicles or aviation and ground equipment and particularly relates to a fuel tank of a plane refueller. The fuel tank of the plane refueller is provided with a tank body, wherein a safe seat and a manhole are arranged on the upper end surface of the tank body, a blowdown valve and an oil filling port are arranged on a lower bottom surface of the tank body, a crawling ladder is arranged at the rear end of the tank body, and an observation window is arranged on a side surface. The fuel tank of the plane refueller is characterized in that the tank body comprises a front vertebral body, a transitional vertebral body and a rear vertebral body, the large opening end of the transitional vertebral body is connected with a large opening end of the rear vertebral body, a supporting and drawing seat is arranged on the lower bottom surface of the front vertebral body, a rotary support mechanism is arranged on the supporting and drawing seat, the front part of the tank body is connected with a trailer through the rotary support mechanism, and the rear end of the tank body is connected with a tire set through a fixed support seat. According to the utility model, due to the adoption of the structure, an automobile chassis is dispensed, the loading capacity of the fuel tank is increased, and the diameter and the fuel reserves of the tank body of the fuel tank can be increased under the condition that the height of the fuel tank is not increased. Therefore, the length of a vehicle body is reduced; and due to the adoption of the double-vertebral body structure, the structural rigidity of the tank body is ensured.

Description

A kind of aircraft bowser oil tank
Technical field
The utility model relates to vehicle or Air Ground Equipment technical field, specifically a kind of aircraft bowser oil tank.
Background technology
As everyone knows, oil tank is the major part of fuel tanker, filling car, and it mainly acts on is oil vessel, and the size of oil tank is the principal parameter of fuel tanker, filling car.
Tank body by its cross sectional shape difference can be divided into cuboid, cylinder, ellipsoid, to go up lower plane curved etc., in the majority with the latter at present.
Means of conveyance are used autotruck more, and especially middle-size and small-size fuel tanker, filling car are fixed on tank body on the car chassis through subframe; The tank body upper surface is provided with emergency seat and manhole; The lower end is provided with foul valve and oil filling port, and the rear end is provided with cat ladder, and the side is provided with observation window.Since the width of vehicle be limited highly; Large-scale fuel tanker, filling car are for the increase capacity, and common way is the length that increases tank body, selects the more chassis of long vehicle body for use; Cause large-scale fuel tanker, filling car to exist the oil tank volume degree of utilization low, the deficiency that vehicle body is long.
Summary of the invention
The purpose of the utility model is the deficiency that solves above-mentioned prior art, provide a kind of rational in infrastructure, increase oil tankage, shorten car load length, reduce the no chassis aircraft bowser oil tank of integral vehicle cost.
The utility model solves the technical scheme that its technical matters adopted:
A kind of aircraft bowser oil tank is provided with tank body, and the tank body upper surface is provided with emergency seat and manhole; Bottom surface is provided with foul valve and oil filling port, and the rear end is provided with cat ladder, and the side is provided with observation window; It is characterized in that tank body is to be made up of precentrum, transition centrum and postcentrum, the big opening end of transition centrum is connected with the big opening end of postcentrum, and the osculum end is connected with the big opening end of precentrum; The upper surface of precentrum, transition centrum and postcentrum at grade, and the transversal surface of the upper surface of precentrum, transition centrum and postcentrum and lower surface is respectively curved, the transition centrum is provided with foul valve with the innermost that postcentrum joins; The postcentrum bottom surface is provided with fixed mounting base, and to bear the main support of oil tank, the precentrum bottom surface is provided with the supporting traction seat; The supporting traction seat is provided with rotary support mechanism, supports and turns to function with the part of bearing oil tank, and the tank body front portion is connected with tractor truck through rotary support mechanism; The rear portion is connected with tire sets through fixed mounting base, has save car chassis, has increased the stowage capacity of oil tank container; Make oil tank under the situation that does not increase height, increase the diameter and the oil reserve of oil tank body; Thereby reduce length over ends of body, and, guaranteed the rigidity of structure of tank body owing to adopt two vertebral body structures.
The beneficial effect of the utility model is: not only consider to satisfy the demand of volume during owing to Oil Tank Design, taken into full account the bear main body of oil tank as the vehicle basic load again, not only bear load own and bear the shearing twist moment that impact load produces oil tank when advancing again; Application of finite element method of calculating during design; The framing member rigidity is optimized, thus the rigidity of raising oil tank, and the shaped design upper tank body has adopted the biconial design; Not only satisfied the volume designing requirement; Improve the capacity of container again, shortened the length of oil tank effectively, and then shortened car load length.
Description of drawings
Accompanying drawing is the structural representation of the utility model.
Reference numeral: supporting traction seat 1, emergency seat 2, manhole 3, cat ladder 5, postcentrum 6, fixed mounting base 7, observation window 8, oil filling port 9, foul valve 10, transition centrum 11, precentrum 12, rotary support mechanism 13.
The specific embodiment:
Below in conjunction with accompanying drawing the utility model is further specified:
Shown in accompanying drawing, a kind of aircraft bowser oil tank is provided with tank body; The tank body upper surface is provided with emergency seat 2 and manhole 3, and bottom surface is provided with foul valve 10 and oil filling port 9, and the rear end is provided with cat ladder 5; The side is provided with observation window 8, it is characterized in that tank body is to be made up of precentrum 12, transition centrum 11 and postcentrum 6, and the big opening end of transition centrum 11 is connected with the big opening end of postcentrum 6; The osculum end is connected with the big opening end of precentrum 12, the upper surface of precentrum 12, transition centrum 11 and postcentrum 6 at grade, and the transversal surface of the upper surface of precentrum 12, transition centrum 11 and postcentrum 6 and lower surface is respectively curved; Transition centrum 11 is provided with foul valve 10 with the innermost of postcentrum 6 handing-over, and postcentrum 6 bottom surfaces are provided with fixed mounting base 7, to bear the main support of oil tank; Precentrum 12 bottom surfaces are provided with supporting traction seat 1, and supporting traction seat 1 is provided with rotary support mechanism 13, support and turn to function with the part of bearing oil tank; The oil tank front portion is connected with tractor truck through rotary support mechanism 13, and the rear portion is connected with tire sets through fixed mounting base 7, has save car chassis; Increased the stowage capacity of oil tank container, made oil tank under the situation that does not increase height, increase the diameter and the oil reserve of oil tank body, thereby reduce length over ends of body; And, guaranteed the rigidity of structure of tank body owing to adopt two vertebral body structures.
The beneficial effect of the utility model is: not only consider to satisfy the demand of volume during owing to Oil Tank Design, taken into full account the bear main body of oil tank as the vehicle basic load again, not only bear load own and bear the shearing twist moment that impact load produces oil tank when advancing again; Application of finite element method of calculating during design; The framing member rigidity is optimized, thus the rigidity of raising oil tank, and the shaped design upper tank body has adopted the biconial design; Not only satisfied the volume designing requirement; Improve the capacity of container again, shortened the length of oil tank effectively, and then shortened car load length.

Claims (1)

1. an aircraft bowser oil tank is provided with tank body, and the tank body upper surface is provided with emergency seat and manhole; Bottom surface is provided with foul valve and oil filling port, and the rear end is provided with cat ladder, and the side is provided with observation window; It is characterized in that tank body is to be made up of precentrum, transition centrum and postcentrum, the big opening end of transition centrum is connected with the big opening end of postcentrum, and the osculum end is connected with the big opening end of precentrum; The upper surface of precentrum, transition centrum and postcentrum at grade; And the upper surface of precentrum, transition centrum and postcentrum and the transversal surface of lower surface are curved respectively, and the innermost of transition centrum and postcentrum handing-over is provided with foul valve, and the postcentrum bottom surface is provided with fixed mounting base; The precentrum bottom surface is provided with the supporting traction seat; The supporting traction seat is provided with rotary support mechanism, and the tank body front portion is connected with tractor truck through rotary support mechanism, and the rear portion is connected with tire sets through fixed mounting base.
CN2011205493740U 2011-12-26 2011-12-26 Fuel tank of plane refueller Expired - Fee Related CN202379300U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2011205493740U CN202379300U (en) 2011-12-26 2011-12-26 Fuel tank of plane refueller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2011205493740U CN202379300U (en) 2011-12-26 2011-12-26 Fuel tank of plane refueller

Publications (1)

Publication Number Publication Date
CN202379300U true CN202379300U (en) 2012-08-15

Family

ID=46627818

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2011205493740U Expired - Fee Related CN202379300U (en) 2011-12-26 2011-12-26 Fuel tank of plane refueller

Country Status (1)

Country Link
CN (1) CN202379300U (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105923283A (en) * 2016-06-07 2016-09-07 航天晨光股份有限公司 Bearing multi-segment variable-section fuel tank of fuelling vehicle
CN106043985A (en) * 2016-07-21 2016-10-26 山东梁山通亚汽车制造有限公司 Remaining-oil-free self-supporting oil tank body and monocoque oil tank truck with same
CN106586299A (en) * 2017-02-13 2017-04-26 平罗县龙江液化气有限责任公司 Compressed natural gas tank type container
CN108584179A (en) * 2018-05-18 2018-09-28 海安县石油科研仪器有限公司 A kind of petroleum storage tank
CN112677863A (en) * 2020-12-31 2021-04-20 中国航空油料集团有限公司 Tank and tank fuelling vehicle

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105923283A (en) * 2016-06-07 2016-09-07 航天晨光股份有限公司 Bearing multi-segment variable-section fuel tank of fuelling vehicle
CN105923283B (en) * 2016-06-07 2019-02-12 航天晨光股份有限公司 A kind of bearing-type multistage variable cross-section tank service truck oil tank
CN106043985A (en) * 2016-07-21 2016-10-26 山东梁山通亚汽车制造有限公司 Remaining-oil-free self-supporting oil tank body and monocoque oil tank truck with same
CN106586299A (en) * 2017-02-13 2017-04-26 平罗县龙江液化气有限责任公司 Compressed natural gas tank type container
CN108584179A (en) * 2018-05-18 2018-09-28 海安县石油科研仪器有限公司 A kind of petroleum storage tank
CN112677863A (en) * 2020-12-31 2021-04-20 中国航空油料集团有限公司 Tank and tank fuelling vehicle

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20120815

Termination date: 20191226

CF01 Termination of patent right due to non-payment of annual fee