CN205418142U - Aircraft combination equipment that shiies is lifted to formula of bowing - Google Patents

Aircraft combination equipment that shiies is lifted to formula of bowing Download PDF

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Publication number
CN205418142U
CN205418142U CN201620108278.5U CN201620108278U CN205418142U CN 205418142 U CN205418142 U CN 205418142U CN 201620108278 U CN201620108278 U CN 201620108278U CN 205418142 U CN205418142 U CN 205418142U
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China
Prior art keywords
trailer
aircraft
lifts
facedown
unit equipment
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Active
Application number
CN201620108278.5U
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Chinese (zh)
Inventor
檀俊飞
许永泉
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Fujian Sizhan Aviation Equipment Co ltd
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Fujian Aviation Equipment Maintenance Center
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 CN201620108278.5U priority Critical patent/CN205418142U/en
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Publication of CN205418142U publication Critical patent/CN205418142U/en
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Abstract

The utility model relates to an aircraft combination equipment that shiies is lifted to formula of bowing, including preceding trailer, transition dolly, the trailer that sets gradually, through pull rod hookup combination between preceding trailer, transition dolly, the trailer, it is used for lifting the lifting devices who holds up the aircraft all to be provided with on preceding trailer and the trailer. This aircraft combination equipment that shiies is lifted to formula of bowing mainly used implements the operations of suing and labouring such as the jacking holds up, transportation to the trouble aircraft, pull at the quilt and can drag the trouble aircraft away from runway or peripheral danger zone fast under the state, avoids causing secondary damage to the aircraft, and it was detained in the time of runway or peripheral danger zone to reduce the aircraft, guaranteed normally taking off and land of follow -up aircraft.

Description

Facedown lifts carrying aircraft unit equipment
Technical field
This utility model relates to a kind of facedown and lifts carrying aircraft unit equipment.
Background technology
At aviation field, aircraft may variable interval, damage at random on runway, aircraft once damages and is necessary for being towed off the runway by breakdown plane or periphery danger zone, avoid aircraft is caused secondary damage, reduce aircraft and be trapped in runway or the time of periphery danger zone, it is ensured that the Normal Take-Off And Landing of follow-up aircraft.Traditional device structure is complicated, motor-driven dumb, and job insecurity operates the most cumbersome, inefficient, it is difficult to undertaking breakdown plane must tow off the runway or the task of periphery danger zone rapidly, safely.
Utility model content
In view of the deficiencies in the prior art, technical problem to be solved in the utility model is to provide a kind of facedown and lifts carrying aircraft unit equipment.
In order to solve above-mentioned technical problem, the technical solution of the utility model is: a kind of facedown lifts carrying aircraft unit equipment, including the front trailer set gradually, transfer ear, trailer, couple combination through pull bar between described front trailer, transfer ear, trailer, described front trailer and trailer are provided with for lifting the lifting device holding up aircraft.
Preferably, described lifting device is made up of with the rear lifting device being positioned on trailer the front lifting device being positioned on front trailer.
Preferably, described front lifting device includes several piston rods of being fixed on front trailer hydraulic cylinder upward, the tailpiece of the piston rod of described hydraulic cylinder is the most up installed with L-type cushion block, front supporting frame, and the top of described front supporting frame is installed with the front lift stand for contacting with aircraft.
Preferably, described front lift stand is made up of four pieces of small-sized lift stands, front supporting frame offers several for the screwed hole being spirally connected with small-sized lift stand, described small-sized lift stand top is provided with arc and lifts a layer A, and it is rubber that described arc lifts the material of layer A.
Preferably, described rear lifting device includes several piston rods of being fixed on trailer hydraulic cylinder upward, the tailpiece of the piston rod of described hydraulic cylinder is the most up installed with L-type cushion block, rear holding frame, and the top of described rear holding frame is installed with the rear lift stand for contacting with aircraft.
Preferably, the quantity of described rear lift stand is two, rear holding frame offers several for the screwed hole being spirally connected with rear lift stand, described rear lift stand top is provided with arc and lifts a layer B, and it is rubber that described arc lifts the material of layer B.
Preferably, the quantity of described trailer is two, connects side by side through back stay between two trailers, and described front trailer, trailer and transfer ear all include that vehicle frame, described bottom of frame are provided with several universal wheels, and described universal wheel is provided with damping spring.
Preferably, described transfer ear also includes the workbox being positioned at bottom of frame.
Preferably, it is additionally provided with for linking up with, with towing motorcar, the draw bar being connected on described front trailer, described draw bar be shaped as triangle, described draw bar include for towing motorcar link up with is connected front knock-off joint, before knock-off joint be point symmetry outside two tilt extension two connecting rods, connect through pull bar A, pull bar B between two connecting rods, two connecting rods are provided with anchor ear.
Preferably, also include the brakes being positioned on front trailer, transfer ear, trailer, realize the banding mechanism that aircraft is stable for bundling aircraft, described banding mechanism includes nylon bandage, hangers, is provided with some for firm tension cable wire between described lifting device and front trailer, trailer.
Compared with prior art, this utility model has the advantages that this facedown is lifted carrying aircraft unit equipment and is mainly used in implementing breakdown plane the operations of suing and labouring such as jacking picking-up, transport, rapidly breakdown plane can be towed off the runway or periphery danger zone under by traction state, avoid aircraft is caused secondary damage, reduce aircraft and be trapped in runway or the time of periphery danger zone, it is ensured that the Normal Take-Off And Landing of follow-up aircraft;This device structure is simple, maneuverability, easy and simple to handle, working stability.
The utility model is described in more detail with detailed description of the invention below in conjunction with the accompanying drawings.
Accompanying drawing explanation
Fig. 1 is front view of the present utility model.
Fig. 2 is top view of the present utility model.
Fig. 3 is the structural representation one of front lifting device.
Fig. 4 is the structural representation two of front lifting device.
Fig. 5 is the structural representation one of rear lifting device.
Fig. 6 is the structural representation two of rear lifting device.
Fig. 7 is the structural representation of transfer ear.
Fig. 8 is the structural representation of draw bar.
In figure: trailer before 1-, 2-transfer ear, 3-trailer, 4-pull bar, lifting device before 5-, lifting device after 6-, 7-hydraulic cylinder, 8-L type cushion block, 9-front supporting frame, lift stand before 10-, the small-sized lift stand of 11-, 12-screwed hole, 13-arc lifts a layer A, holding frame after 14-, lift stand after 15-, 16-arc lifts a layer B, 17-back stay, 18-vehicle frame, 19-universal wheel, 20-damping spring, 21-workbox, 22-draw bar, knock-off joint before 23-, 24-connecting rod, 25-pull bar A, 26-pull bar B, 27-anchor ear, 28-strains cable wire.
Detailed description of the invention
For features described above of the present utility model and advantage can be become apparent, special embodiment below, and coordinate accompanying drawing, it is described in detail below.
As shown in Fig. 1 ~ 8, a kind of facedown lifts carrying aircraft unit equipment, including the front trailer 1 set gradually, transfer ear 2, trailer 3, couple combination through pull bar 4 between described front trailer, transfer ear, trailer, described front trailer and trailer are provided with for lifting the lifting device holding up aircraft.
In this utility model embodiment, described lifting device is made up of with the rear lifting device 6 being positioned on trailer the front lifting device 5 being positioned on front trailer.
In this utility model embodiment, described front lifting device includes several piston rods of being fixed on front trailer hydraulic cylinder 7 upward, the tailpiece of the piston rod of described hydraulic cylinder is the most up installed with L-type cushion block 8, front supporting frame 9, and the top of described front supporting frame is installed with the front lift stand 10 for contacting with aircraft.
In this utility model embodiment, described front lift stand is made up of four pieces of small-sized lift stands 11, offer on front supporting frame several for the screwed hole 12 being spirally connected with small-sized lift stand, described small-sized lift stand top is provided with arc and lifts a layer A13, and it is rubber that described arc lifts the material of layer A.
In this utility model embodiment, described rear lifting device includes several piston rods of being fixed on trailer hydraulic cylinder upward, the tailpiece of the piston rod of described hydraulic cylinder is the most up installed with L-type cushion block, rear holding frame 14, and the top of described rear holding frame is installed with the rear lift stand 15 for contacting with aircraft.
In this utility model embodiment, the quantity of described rear lift stand is two, rear holding frame offers several for the screwed hole being spirally connected with rear lift stand, described rear lift stand top is provided with arc and lifts a layer B16, and it is rubber that described arc lifts the material of layer B.
In this utility model embodiment, the quantity of described trailer is two, connect side by side through back stay 17 between two trailers, described front trailer, trailer and transfer ear all include vehicle frame 18, described bottom of frame is provided with several universal wheels 19, and described universal wheel is provided with damping spring 20.
In this utility model embodiment, described transfer ear also includes the workbox 21 being positioned at bottom of frame, can be used for placing random device, attachment tools and loading part adnexa etc..
In this utility model embodiment, it is additionally provided with for linking up with, with towing motorcar, the draw bar 22 being connected on described front trailer, described draw bar be shaped as triangle, described draw bar include for towing motorcar link up with is connected front knock-off joint 23, before knock-off joint be point symmetry outside two tilt extension two connecting rods 24, connect through pull bar A25, pull bar B26 between two connecting rods, two connecting rods are provided with anchor ear 27.
In this utility model embodiment, also include the brakes being positioned on front trailer, transfer ear, trailer, realize the banding mechanism that aircraft is stable for bundling aircraft, described banding mechanism is nylon bandage, hangers, airframe walked around by nylon bandage, two ends are hooked on hangers respectively, tighten up nylon bandage and realize fixing, be provided with some between described lifting device and front trailer, trailer for firm tension cable wire 28.
This utility model is not limited to above-mentioned preferred forms, and anyone can show that under enlightenment of the present utility model other various forms of facedown lift carrying aircraft unit equipment.All impartial changes done according to this utility model claim and modification, all should belong to covering scope of the present utility model.

Claims (10)

1. a facedown lifts carrying aircraft unit equipment, it is characterized in that: the front trailer that includes setting gradually, transfer ear, trailer, couple combination through pull bar between described front trailer, transfer ear, trailer, described front trailer and trailer are provided with for lifting the lifting device holding up aircraft.
Facedown the most according to claim 1 lifts carrying aircraft unit equipment, it is characterised in that: described lifting device is made up of with the rear lifting device being positioned on trailer the front lifting device being positioned on front trailer.
Facedown the most according to claim 2 lifts carrying aircraft unit equipment, it is characterized in that: described front lifting device includes several piston rods of being fixed on front trailer hydraulic cylinder upward, the tailpiece of the piston rod of described hydraulic cylinder is the most up installed with L-type cushion block, front supporting frame, and the top of described front supporting frame is installed with the front lift stand for contacting with aircraft.
Facedown the most according to claim 3 lifts carrying aircraft unit equipment, it is characterized in that: described front lift stand is made up of four pieces of small-sized lift stands, several are offered for the screwed hole being spirally connected with small-sized lift stand on front supporting frame, described small-sized lift stand top is provided with arc and lifts a layer A, and it is rubber that described arc lifts the material of layer A.
Facedown the most according to claim 2 lifts carrying aircraft unit equipment, it is characterized in that: described rear lifting device includes several piston rods of being fixed on trailer hydraulic cylinder upward, the tailpiece of the piston rod of described hydraulic cylinder is the most up installed with L-type cushion block, rear holding frame, and the top of described rear holding frame is installed with the rear lift stand for contacting with aircraft.
Facedown the most according to claim 5 lifts carrying aircraft unit equipment, it is characterized in that: the quantity of described rear lift stand is two, several are offered for the screwed hole being spirally connected with rear lift stand in rear holding frame, described rear lift stand top is provided with arc and lifts a layer B, and it is rubber that described arc lifts the material of layer B.
Facedown the most according to claim 1 lifts carrying aircraft unit equipment, it is characterized in that: the quantity of described trailer is two, connect side by side through back stay between two trailers, described front trailer, trailer and transfer ear all include vehicle frame, described bottom of frame is provided with several universal wheels, and described universal wheel is provided with damping spring.
Facedown the most according to claim 7 lifts carrying aircraft unit equipment, it is characterised in that: described transfer ear also includes the workbox being positioned at bottom of frame.
Facedown the most according to claim 1 lifts carrying aircraft unit equipment, it is characterized in that: be additionally provided with for linking up with, with towing motorcar, the draw bar being connected on described front trailer, described draw bar be shaped as triangle, described draw bar include for towing motorcar link up with is connected front knock-off joint, before knock-off joint be point symmetry outside two tilt extension two connecting rods, connect through pull bar A, pull bar B between two connecting rods, two connecting rods are provided with anchor ear.
Facedown the most according to claim 1 lifts carrying aircraft unit equipment, it is characterized in that: also include the brakes being positioned on front trailer, transfer ear, trailer, realize the banding mechanism that aircraft is stable for bundling aircraft, described banding mechanism includes nylon bandage, hangers, is provided with some for firm tension cable wire between described lifting device and front trailer, trailer.
CN201620108278.5U 2016-02-03 2016-02-03 Aircraft combination equipment that shiies is lifted to formula of bowing Active CN205418142U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620108278.5U CN205418142U (en) 2016-02-03 2016-02-03 Aircraft combination equipment that shiies is lifted to formula of bowing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620108278.5U CN205418142U (en) 2016-02-03 2016-02-03 Aircraft combination equipment that shiies is lifted to formula of bowing

Publications (1)

Publication Number Publication Date
CN205418142U true CN205418142U (en) 2016-08-03

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620108278.5U Active CN205418142U (en) 2016-02-03 2016-02-03 Aircraft combination equipment that shiies is lifted to formula of bowing

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Country Link
CN (1) CN205418142U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106608357A (en) * 2016-08-31 2017-05-03 马宏 Application of boom trolley
CN110406454A (en) * 2019-06-29 2019-11-05 芜湖航翼集成设备有限公司 Aircraft emergency management and rescue fast removal equipment

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106608357A (en) * 2016-08-31 2017-05-03 马宏 Application of boom trolley
CN110406454A (en) * 2019-06-29 2019-11-05 芜湖航翼集成设备有限公司 Aircraft emergency management and rescue fast removal equipment
CN110406454B (en) * 2019-06-29 2022-04-01 芜湖航翼集成设备有限公司 Quick carrying equipment for emergency rescue of airplane

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Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
TR01 Transfer of patent right

Effective date of registration: 20221027

Address after: No. 168, Jinda Road, Jianxin Town, Cangshan District, Fuzhou City, Fujian Province, 350007

Patentee after: Fujian Sizhan Aviation Equipment Co.,Ltd.

Address before: No. 168, Jinda Road, Jinshan Industrial Zone, Fuzhou City, Fujian Province 350007

Patentee before: FUJIAN AVIATION EQUIPMENT MAINTENANCE CENTER

TR01 Transfer of patent right