CN206359180U - A kind of aircraft maintenance jack - Google Patents
A kind of aircraft maintenance jack Download PDFInfo
- Publication number
- CN206359180U CN206359180U CN201720011522.0U CN201720011522U CN206359180U CN 206359180 U CN206359180 U CN 206359180U CN 201720011522 U CN201720011522 U CN 201720011522U CN 206359180 U CN206359180 U CN 206359180U
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- CN
- China
- Prior art keywords
- pressurized strut
- base
- hand pump
- piston rod
- jack
- 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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Abstract
A kind of aircraft maintenance jack, it includes:Base, pressurized strut, fuel tank, hand pump, commutator, start cover;Base, is placed on ground, for playing a supportive role;Pressurized strut, is fixedly mounted on the base by screw, is internally provided with the telescopic piston rod of level Four, and the pressurized strut top is provided with screw switch, for controlling the lift when piston rod is moved up;Fuel tank, is placed on the base, for providing working solution to hand pump;Hand pump, is connected by pipeline road with the hydraulic oil container, for when the piston rod is lifted and is declined, working solution to be supplied to the pressurized strut.Aircraft maintenance of the present utility model jack small volume, is easy to carry;Working condition is full manual mode, easy to operate;Equipment reliable operation is easy to maintenance;Loading capacity is big, safe and reliable;It is lightweight, conveniently moving;Fault rate is low.
Description
Technical field
The utility model is related to a kind of aircraft maintenance device, more particularly, to a kind of aircraft maintenance jack.
Background technology
Main wheel jack is the special equipment that support top aircraft main unit of landing gear change main airplane wheel.The equipment
It is an innovative product, its innovation and application solve the problem for being not required to the full machine of support top aircraft just replaceable airplane wheel, carry
The high maintenance work efficiency of outfield undercarriage, has particularly significant meaning to the rate of attendance for improving aircraft.If to main wheel thousand
Jin top push rod is repaired and to supporting stand size redefinition, the equipment application can be made to carry out tearing open for wheel on polytype aircraft
Work is unloaded, therefore, this innovative technology has very big market value.
In the prior art, it is necessary to very heavy before the main jack of aircraft and aircraft particularly when dismounting nose-gear wheel
Topmast top aircraft, so its maintenance procedures is complicated, maintenance time is long, and maintenance cost is high, in addition, existing wheel jack volume
Greatly, weight weight, it has not been convenient to use, it is therefore necessary to improve.
Utility model content
1. the technical problem to be solved
Based on the above-mentioned problems in the prior art, the purpose of this utility model is that providing a kind of aircraft maintenance uses thousand
Jin top.
2. technical scheme
The purpose of this utility model is mainly realized by following technical scheme.
A kind of aircraft maintenance jack, it includes:Base, pressurized strut, fuel tank, hand pump, commutator, start cover;
Base, is placed on ground, for playing a supportive role;Pressurized strut, is fixedly mounted on the base by screw, is internally provided with
The telescopic piston rod of level Four, the pressurized strut top is provided with screw switch, during for controlling the piston rod to move up
Lift;Fuel tank, is placed on the base, for providing working solution to hand pump;Hand pump, passes through pipeline road and the liquid
Case connection is pressed oil, for when the piston rod is lifted and is declined, working solution to be supplied to the pressurized strut;Commutator, fixed peace
On base, inside sets and is provided with switch operation on reversal valve, the flow direction for controlling oil circuit working solution, the commutator
Bar, for determining that the piston rod rises or falls;Choke valve, is arranged on the pipeline road being connected with hand pump, the hand
The hydraulic oil for shaking pump outflow enters the pressurized strut along the choke valve.
Preferably, the pressurized strut has start cover, when jack when not in use, the pressurized strut cover buckle is in pressurized strut
Top.
Preferably, the base two ends respectively set leader, in order to carry.
3. beneficial effect
Compared with prior art, a kind of aircraft maintenance of the present utility model is with the beneficial effect of jack:
Jack is in use, the bottom that replacing wheel jack is placed on into airplane wheel is fixed, and adjustable change valve exists
Jack-up position, is moved back and forth with hand pump, aircraft fluid is squeezed into pressurized strut, jack-up frame;After reaching a certain height, adjust
Whole screw switch, makes pressurized strut be fixed on certain altitude constant;Wheel is changed, after the completion of replacing, adjustable change valve makes jack
It is slowly declined to be less than frame, removes jack wheel and change completion.
Aircraft maintenance of the present utility model jack small volume, is easy to carry;Working condition is full manual mode, operation
It is convenient;Equipment reliable operation is easy to maintenance;Loading capacity is big, safe and reliable;It is lightweight, conveniently moving;Fault rate is low.
Brief description of the drawings
Fig. 1 is a kind of signal of the structure of the aircraft maintenance jack constituted according to the utility model preferred embodiment
Figure.
In figure:
1- bases, 2- pressurized struts, 3- fuel tanks, 4- hand pumps, 5- commutators, 6- starts cover, 7- oil fillers, 8- fuel tanks
Mouth, 9- oil pipes, 10- winds, 11- handles, 12- switch operations bar, 13- screw switch, 14- pressurized struts top.
Embodiment
Hereinafter, specific embodiment of the utility model is described in detail refer to the attached drawing, it is detailed according to these
Thin description, one of ordinary skill in the art can implement the utility model it can be clearly understood that the utility model.Do not disobeying
In the case of carrying on the back the utility model principle, the feature in each different embodiment can be combined to obtain new embodiment party
Formula, or some of some embodiments feature is substituted, acquisition is other preferred embodiment.
Fig. 1 shows a kind of structure of the aircraft maintenance jack constituted according to the utility model preferred embodiment.Such as
Shown in Fig. 1, a kind of aircraft maintenance jack, it includes:Base 1, pressurized strut 2, fuel tank 3, hand pump 4, commutator 5, start
Cover 6;Base 1 is placed on ground, for playing a supportive role;Pressurized strut 2 is fixedly mounted on the base by screw, internal
Be provided with the telescopic piston rod of level Four, the top of pressurized strut 2 is provided with screw switch 13, for control the piston rod to
Lift when upper mobile;Fuel tank 3, is placed on the base 1, for providing working solution to hand pump 4;Hand pump 4, passes through oil transportation
Pipeline is connected with the fuel tank 3, for when the piston rod is lifted and is declined, working solution to be supplied to the pressurized strut 2;Commutation
Device 5, is fixedly mounted on base 1, and inside sets and set on reversal valve, the flow direction for controlling oil circuit working solution, the commutator
Switch operation bar 12 is equipped with, for determining that the piston rod rises or falls;Choke valve, is arranged on be connected with hand pump 4 defeated
On oil pipe line, the hydraulic oil that the hand pump 4 flows out enters the pressurized strut 2 along the choke valve.
In a further preferred embodiment, the pressurized strut 2 have start cover 6, when jack when not in use, it is described
Start cover 6 is buckled in pressurized strut top 14.
In a further preferred embodiment, the two ends of base 1 respectively set leader 11, in order to carry.
Although the utility model is described above by referring to specific embodiment, art technology people
Member for the utility model is disclosed it should be appreciated that in the utility model principle disclosed and scope, can configure and details
Make many modifications.Protection domain of the present utility model is determined by appended claim, and claim is intended to
Whole modifications that the equivalent literal meaning or scope of technical characteristic are included in claim.
Claims (3)
1. a kind of aircraft maintenance jack, it is characterised in that including:Base, pressurized strut, fuel tank, hand pump, commutator, work
Dynamic cover;Base, is placed on ground, for playing a supportive role;Pressurized strut, is fixedly mounted on the base by screw, interior
Portion is provided with the telescopic piston rod of level Four, and the pressurized strut top is provided with screw switch, for control the piston rod to
Lift when upper mobile;Fuel tank, is placed on the base, for providing working solution to hand pump;Hand pump, passes through pipeline road
It is connected with the fuel tank, for when the piston rod is lifted and is declined, working solution to be supplied to the pressurized strut;Commutator, Gu
Dingan County is on base, and inside sets and is provided with commutation on reversal valve, the flow direction for controlling oil circuit working solution, the commutator
Action bars, for determining that the piston rod rises or falls;Choke valve, is arranged on the pipeline road being connected with hand pump, institute
The hydraulic oil for stating hand pump outflow enters the pressurized strut along the choke valve.
2. a kind of aircraft maintenance jack as claimed in claim 1, it is characterised in that the pressurized strut has pressurized strut
Lid.
3. a kind of aircraft maintenance jack as claimed in claim 1 or 2, it is characterised in that the base two ends are respectively set
Leader.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201720011522.0U CN206359180U (en) | 2017-01-05 | 2017-01-05 | A kind of aircraft maintenance jack |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201720011522.0U CN206359180U (en) | 2017-01-05 | 2017-01-05 | A kind of aircraft maintenance jack |
Publications (1)
Publication Number | Publication Date |
---|---|
CN206359180U true CN206359180U (en) | 2017-07-28 |
Family
ID=59379145
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201720011522.0U Active CN206359180U (en) | 2017-01-05 | 2017-01-05 | A kind of aircraft maintenance jack |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN206359180U (en) |
-
2017
- 2017-01-05 CN CN201720011522.0U patent/CN206359180U/en active Active
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