CN204297118U - A kind of Small General Aircraft draw bar - Google Patents

A kind of Small General Aircraft draw bar Download PDF

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Publication number
CN204297118U
CN204297118U CN201420696308.XU CN201420696308U CN204297118U CN 204297118 U CN204297118 U CN 204297118U CN 201420696308 U CN201420696308 U CN 201420696308U CN 204297118 U CN204297118 U CN 204297118U
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CN
China
Prior art keywords
axle
bar
draw bar
strut
connecting cylinder
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Active
Application number
CN201420696308.XU
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Chinese (zh)
Inventor
刘剑
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.)
Xian Aircraft Design and Research Institute of AVIC
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Xian Aircraft Design and Research Institute of AVIC
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Priority to CN201420696308.XU priority Critical patent/CN204297118U/en
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Abstract

The utility model belongs to plane draw bar design, particularly a kind of Small General Aircraft draw bar.Described draw bar comprises the first bar (8), the second bar (10), sleeve (13), the first connecting cylinder (1), the second connecting cylinder (17), the first strut (3), the second strut (15), connecting rod (4), auricle (5), handle (7), Quick-release pin (9), the first axle (2), the second axle (11), the 3rd axle (12), the 4th axle (14), the 5th axle (16), bolt (6).The utility model structure is simple, lightweight, has quick locking function, can be connected with aircraft tow attachment safely and reliably.There is length adjustment function, flight crew can be made in use can not to interfere with head, when depositing aboard, can parking space be reduced.

Description

A kind of Small General Aircraft draw bar
Technical field
The utility model belongs to plane draw bar design, particularly a kind of Small General Aircraft draw bar.
Background technology
The draw bar of usual Small General Aircraft all carries with aircraft, by the restriction of space in aircraft cabin and load-carrying, require that the lightweight and volume of draw bar is little, this just makes its structure necessary simple, therefore draw bar can be caused not firm or connect complexity when being connected with aircraft tow attachment, and because draw bar volume is too little, flight crew when towing aircraft easily and head interfere.
Utility model content
The purpose of this utility model: the Small General Aircraft draw bar that a kind of structure is simple, lightweight, convenient and reliable is provided.
The technical solution of the utility model is: a kind of Small General Aircraft draw bar, is characterized by: described draw bar comprises the first bar 8, second bar 10, sleeve 13, first connecting cylinder 1, second connecting cylinder 17, first strut 3, second strut 15, connecting rod 4, auricle 5, handle 7, Quick-release pin 9, first axle 2, second axle 11, the 3rd axle 12, the 4th axle 14, the 5th axle 16, bolt 6, wherein said sleeve 13 to be arranged on the first bar 8, described auricle 5 is fixed on the first bar 8 by bolt 6, described second bar 10 is arranged on the first bar 8 by Quick-release pin 9, described first connecting cylinder 1 is arranged on 5, ear by bolt 6, described first connecting cylinder 1 is connected with the first strut 3 by the first axle 2, described first strut 3 is connected with sleeve 13 by the first axle 2, described second connecting cylinder 17 is connected with the second strut 15 by the 5th axle 16, described second strut 15 is connected with sleeve 13 by the 5th axle 16, described connecting rod 4 is connected with sleeve 13 by the 4th axle 14, described connecting rod 4 is connected with handle 7 by the second axle 11, described handle 7 is connected with auricle 5 by the 3rd axle 12, handle 7 is connected with the first connecting cylinder 1, second connecting cylinder 17 by double leval jib transmission mechanism.
The utility model beneficial effect is: a kind of Small General Aircraft draw bar of the utility model structure is simple, lightweight, has quick locking function, can be connected with aircraft tow attachment safely and reliably.There is length adjustment function, flight crew can be made in use can not to interfere with head, when depositing aboard, can parking space be reduced.
Accompanying drawing explanation
Fig. 1 is a kind of Small General Aircraft draw bar of the utility model structural representation;
Fig. 2 is a kind of Small General Aircraft draw bar of the utility model partial structurtes schematic diagrames;
Fig. 3 is a kind of Small General Aircraft draw bar of the utility model connecting cylinder schematic diagram when opening;
Fig. 4 is a kind of Small General Aircraft draw bar of the utility model connecting cylinder local structural representation when opening;
Schematic diagram when Fig. 5 is the draw bar transport of the utility model one Small General Aircraft,
Wherein, 1-first connecting cylinder, 2-first axle, 3-first strut, 4-connecting rod, 5-auricle, 6-bolt, 7-handle, 8-first bar, 9-Quick-release pin, 10-second bar, 11-second axle, 12-the 3rd axle, 13-sleeve, 14-the 4th axle, 15-second strut, 16-the 5th axle, 17-second connecting cylinder.
Detailed description of the invention
Below by detailed description of the invention, the utility model is further described:
Refer to Fig. 1, Fig. 2, it is a kind of Small General Aircraft draw bar of the utility model structural representation.A kind of Small General Aircraft draw bar of the utility model comprises the first connecting cylinder 1, first axle 2, first strut 3, connecting rod 4, auricle 5, bolt 6, handle 7, first bar 8, Quick-release pin 9, second bar 10, second axle 11, the 3rd axle 12, sleeve 13, the 4th axle 14, second strut 15, the 5th axle 16, second connecting cylinder 17.Wherein, described sleeve 13 is arranged on bar 8, auricle 5 is fixed on the first bar 8 by bolt 6, second bar 10 is arranged on the first bar 8 by Quick-release pin 9, first connecting cylinder 1 is arranged on auricle 5 by bolt 6, first connecting cylinder 1 is connected with the first strut 3 by the first axle 2, first strut 3 is connected with sleeve 13 by the first axle 2, second connecting cylinder 17 is connected with the second strut 15 by the 5th axle 16, second strut 15 is connected with sleeve 13 by the 5th axle 16, connecting rod 4 is connected with sleeve 13 by the 4th axle 14, connecting rod 4 is connected with handle 7 by the second axle 11, handle 7 is connected with auricle 5 by the 3rd axle 12.
Please refer to Fig. 3 and Fig. 5, wherein, Fig. 3 is a kind of Small General Aircraft draw bar of the utility model sleeve schematic diagram when opening, schematic diagram when Fig. 5 is a kind of Small General Aircraft draw bar transport of the utility model.During the utility model one Small General Aircraft draw bar towing aircraft, first towards draw bar top driving handle 7, handle 7 rotates around the 3rd axle 12, meanwhile handle 7 passes through the second axle 11 drivening rod 4 to draw bar top movements, connecting rod 4 is with moving sleeve 13 to draw bar top movements by the 4th axle 14, sleeve 13 is respectively by the first axle 2, 5th axle 16 drives the first strut 3, second strut 15 moves, first strut 3 and the second strut 15 are again respectively by the first axle 2, 5th axle 16 promotes the first connecting cylinder 1, second connecting cylinder 17 outwards moves, draw bar is opened.Take off Quick-release pin 9, extract the second bar 10, then insert Quick-release pin 9, length of draw bar is increased.When a kind of Small General Aircraft draw bar of the utility model transports, pull up Quick-release pin 9, push back the second bar 10, then insert Quick-release pin 9, length of draw bar is shortened.Driving handle 7 bottom draw bar, handle 7 rotates around the 3rd axle 12, meanwhile handle 7 is moved bottom draw bar by the second axle 11 drivening rod 4, connecting rod 4 is moved with the bottom of moving sleeve 13 to draw bar by the 4th axle 14, sleeve 13 drives the first strut 3, second strut 15 to move respectively by the first axle 2, the 5th axle 16, first strut 3 and the second strut 15 promote the first connecting cylinder 1, second connecting cylinder 17 inwardly move respectively by the first axle 2, the 5th axles 16 again, make draw bar closed and locked.
The utility model realizes the opening of draw bar connector, closed locked by the quadric chain of handle, connecting rod, sleeve, auricle, strut, realize elongation and the shortening of draw bar by the first bar and the second shank diameter difference, when realizing length of draw bar change by Quick-release pin, the second bar is fixing.Its structure is simple, lightweight, reliably easy to connect with aircraft, and body of rod length can regulate, and makes to operate during flight crew's towing aircraft comfortable.

Claims (1)

1. a Small General Aircraft draw bar, is characterized by: described draw bar comprises the first bar (8), the second bar (10), sleeve (13), the first connecting cylinder (1), the second connecting cylinder (17), the first strut (3), the second strut (15), connecting rod (4), auricle (5), handle (7), Quick-release pin (9), the first axle (2), the second axle (11), the 3rd axle (12), the 4th axle (14), the 5th axle (16), bolt (6), wherein said sleeve (13) is arranged on (8) on the first bar, described auricle (5) is fixed on the first bar (8) by bolt (6), described second bar (10) is arranged on the first bar (8) by Quick-release pin (9), described first connecting cylinder (1) is arranged on auricle (5) by bolt (6), described first connecting cylinder (1) is connected with the first strut (3) by the first axle (2), described first strut (3) is connected with sleeve (13) by the first axle (2), described second connecting cylinder (17) is connected with the second strut (15) by the 5th axle (16), described second strut (15) is connected with sleeve (13) by the 5th axle (16), described connecting rod (4) is connected with sleeve (13) by the 4th axle (14), described connecting rod (4) is connected with handle (7) by the second axle (11), described handle (7) is connected with auricle (5) by the 3rd axle (12), handle (7) is connected with the first connecting cylinder (1), the second connecting cylinder (17) by double leval jib transmission mechanism.
CN201420696308.XU 2014-11-19 2014-11-19 A kind of Small General Aircraft draw bar Active CN204297118U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420696308.XU CN204297118U (en) 2014-11-19 2014-11-19 A kind of Small General Aircraft draw bar

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420696308.XU CN204297118U (en) 2014-11-19 2014-11-19 A kind of Small General Aircraft draw bar

Publications (1)

Publication Number Publication Date
CN204297118U true CN204297118U (en) 2015-04-29

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420696308.XU Active CN204297118U (en) 2014-11-19 2014-11-19 A kind of Small General Aircraft draw bar

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CN (1) CN204297118U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104627382A (en) * 2015-01-27 2015-05-20 江苏中陆航星航空工业有限公司 Small airplane draw bar

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104627382A (en) * 2015-01-27 2015-05-20 江苏中陆航星航空工业有限公司 Small airplane draw bar

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