CN106628230B - Safe traction hanger - Google Patents
Safe traction hanger Download PDFInfo
- Publication number
- CN106628230B CN106628230B CN201610932452.2A CN201610932452A CN106628230B CN 106628230 B CN106628230 B CN 106628230B CN 201610932452 A CN201610932452 A CN 201610932452A CN 106628230 B CN106628230 B CN 106628230B
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- traction
- clamping
- safety
- fixedly connected
- hanger
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- 230000009471 action Effects 0.000 claims description 10
- 210000000078 claw Anatomy 0.000 claims description 9
- 238000000034 method Methods 0.000 abstract description 7
- 230000008569 process Effects 0.000 abstract description 7
- 238000012423 maintenance Methods 0.000 abstract description 3
- 230000008878 coupling Effects 0.000 description 3
- 238000010168 coupling process Methods 0.000 description 3
- 238000005859 coupling reaction Methods 0.000 description 3
- 230000001681 protective effect Effects 0.000 description 3
- 241001391944 Commicarpus scandens Species 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/22—Ground or aircraft-carrier-deck installations for handling aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Emergency Lowering Means (AREA)
Abstract
The invention provides a safe traction hanger, which comprises a traction band group, wherein one end of the traction band group is fixedly connected with a first landing gear tethering band through an overload protection device, and the other end of the traction band group is fixedly connected with a second landing gear tethering band through a dynamometer; the middle part of the traction band group is matched with the fixed pulley; the overload protection device comprises a first quick lock joint fixedly connected with the first falling frame tying belt and a second quick lock joint fixedly connected with the traction belt group, and the first quick lock joint and the second quick lock joint are respectively clamped with two ends of the safety pin. The safe traction hanger disclosed by the invention is safe to use and convenient to maintain, and ensures that the whole aircraft is stably and safely pulled. The traction force can be displayed and recorded by the invention during traction through the dynamometer. In addition, through the second quick lock joint and the first quick lock joint with the shear pin joint, under the prerequisite of guaranteeing to connect firmly, simplified the operation process of changing the shear pin, reduced operator's work load, improved maintenance efficiency.
Description
Technical Field
The invention belongs to the field of aviation auxiliary equipment, and particularly relates to a traction hanger.
Background
Aircraft, which are indispensable vehicles in modern life, require traction devices such as tractors to be used for traction once their own power systems cannot work due to their large volumes and weights. In the prior art, the traction hanger does not have a traction reading function, and in the traction process, the safety of the traction hanger can be ensured only by means of the overload protection device. Once the overload protection device is in a problem, accidents are likely to occur in the traction process, and the personal safety of equipment and field personnel cannot be ensured.
Disclosure of Invention
In view of the above, the present invention aims to provide a safe traction hanger, so as to solve the problem of lower safety in the prior art because the traction hanger cannot accurately monitor the traction force.
In order to achieve the above purpose, the technical scheme of the invention is realized as follows:
a safe traction hanger comprises a traction band group, wherein one end of the traction band group is fixedly connected with a first landing gear tethering band through an overload protection device, and the other end of the traction band group is fixedly connected with a second landing gear tethering band through a dynamometer; the middle part of the traction band group is matched with the fixed pulley; the overload protection device comprises a first quick lock joint fixedly connected with the first falling frame tying belt and a second quick lock joint fixedly connected with the traction belt group, and the first quick lock joint and the second quick lock joint are respectively clamped with two ends of the safety pin.
Further, the dynamometer is of an integrated structure, an LCD screen is arranged on the dynamometer, and the dynamometer is provided with an infrared remote controller.
Further, the second quick lock connector and the first quick lock connector have the same structure and comprise a barrel body, the outer circular side wall of the barrel body is provided with a plurality of containing holes communicated with the outside and the inside of the barrel body, and each containing hole is internally provided with a clamping block moving along the radial direction of the barrel body; the outer circular side wall of the safety pin is provided with a clamping groove matched with the clamping block in a clamping way.
Further, the accommodating hole is a stepped hole and comprises an upper layer hole and a lower layer hole arranged at the bottom of the upper layer hole; the clamping block is arranged in the upper layer hole, and a spring is fixedly connected between the clamping block and the bottom of the upper layer hole; the push ring is sleeved on the outer side of the barrel body, and a push block matched with the clamping block is arranged on the push ring.
Further, the fixture block is close to the side wall upper end edge of ejector pad is equipped with the chamfer, and the side wall lower extreme edge that the ejector pad is close to the fixture block is equipped with the fillet.
Further, the lower end of the clamping block is provided with a plurality of clamping claws which are distributed along the axial direction of the barrel body, and the lengths of the clamping claws are larger than the depth of the lower layer hole.
Further, the safety pin comprises an action section, two ends of the action section are fixedly connected with a clamping joint respectively, and the outer diameter of the action section is smaller than that of the clamping joint; the clamping groove is arranged on the clamping joint.
Further, a breakage protection rope is connected between the first landing frame tying belt and the traction belt group.
Further, the traction band group comprises a plurality of traction bands, and two adjacent traction bands are connected through shackles.
Further, the fixed pulley comprises a traction pulley, and a groove matched with the traction belt is formed in the outer circular side wall of the traction pulley; the traction pulley is rotationally connected with the traction pulley frame through a pulley shaft.
Compared with the prior art, the safe traction hanger has the following advantages:
the safe traction hanger disclosed by the invention is safe to use and convenient to maintain, and ensures that the whole aircraft is stably and safely pulled. The traction force can be displayed and recorded by the invention during traction through the dynamometer. Meanwhile, the dynamometer is monitored by means of the remote controller, so that the personal safety of on-site workers is guaranteed. In addition, through the second quick lock joint and the first quick lock joint with the shear pin joint, under the prerequisite of guaranteeing to connect firmly, simplified the operation process of changing the shear pin, reduced operator's work load, improved maintenance efficiency.
Drawings
The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the invention. In the drawings:
FIG. 1 is a top view of a safety traction hanger according to an embodiment of the present invention;
FIG. 2 is an enlarged view of section I of FIG. 1;
FIG. 3 is an isometric view of a second quick lock coupling and a safety pin of a safety traction device according to an embodiment of the present invention;
FIG. 4 is an isometric view of a second quick lock coupling of a safety traction hanger with a push ring removed according to an embodiment of the present invention;
FIG. 5 is a front view in cross section of a second quick lock coupling and safety pin of a safety traction hanger according to an embodiment of the present invention in an unlocked state;
fig. 6 is a front view in cross section of a second quick lock joint and a safety pin of the safety traction hanger according to an embodiment of the present invention;
fig. 7 is an exploded isometric view of a fixed sheave of a safety traction hanger according to an embodiment of the present invention.
Reference numerals illustrate:
1-a fixed pulley; 11-traction sheave; 111-groove; 12-pulley shafts; 13-traction sheave frame; 2-a traction belt; 3-shackle; 4-a load cell; 5-a second quick lock joint; 51-a first quick lock connector; 52-push ring; 521-pushing blocks; 53-clamping blocks; 531-jaws; 54-safety pin; 541-snap fitting; 542-a clamping groove; 543-action segment; 55-barrel body; 56-lower layer holes; 561-upper layer holes; 57-springs; 6-breaking the protective rope; 7-tying the tie strap on the first landing rack; 8-a second landing gear tie-down strap.
Detailed Description
It should be noted that, without conflict, the embodiments of the present invention and features of the embodiments may be combined with each other.
In the description of the present invention, it should be understood that the terms "center", "longitudinal", "lateral", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, are merely for convenience in describing the present invention and simplifying the description, and do not indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the present invention. Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first", "a second", etc. may explicitly or implicitly include one or more such feature. In the description of the present invention, unless otherwise indicated, the meaning of "a plurality" is two or more.
In the description of the present invention, it should be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be either fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present invention can be understood by those of ordinary skill in the art in a specific case.
The invention will be described in detail below with reference to the drawings in connection with embodiments.
1-2, the present invention proposes a safety traction hanger, comprising a traction band group, one end of which is fixedly connected with a first landing gear tying band 7 through an overload protection device, and the other end of which is fixedly connected with a second landing gear tying band 8 through a dynamometer 4; the middle part of the traction band group is matched with the fixed pulley 1; the overload protection device comprises a first quick locking connector 51 fixedly connected with the first falling frame tying belt 7 and a second quick locking connector 5 fixedly connected with the traction belt group, and the first quick locking connector and the second quick locking connector are respectively clamped with two ends of the safety pin 54.
The dynamometer 4 is of an integrated structure, an LCD screen is arranged on the dynamometer 4, and an infrared remote controller is arranged on the dynamometer 4. The infrared remote controller is used for controlling the dynamometer 4, so that various functions such as zero setting, peeling, accumulated inquiry, unit switching, voltage inquiry, shutdown and the like can be realized. The maximum measuring range of the dynamometer 4 can be 300KN (30T) to 3000KN (300T), and the traction force measurement requirement of a common aircraft is met.
As shown in fig. 3-5, the second quick lock connector 5 has the same structure as the first quick lock connector 51, and includes a tub body 55, a plurality of receiving holes communicating the outside with the inside of the tub body 55 are provided on the outer sidewall of the tub body 55, and a clamping block 53 moving radially along the tub body 55 is provided in each receiving hole; the outer sidewall of the safety pin 54 is provided with a clamping groove 542 engaged with the clamping block 53.
The accommodating hole is a stepped hole, and comprises an upper layer hole 561 and a lower layer hole 56 arranged at the bottom of the upper layer hole 561; the clamping block 53 is arranged in the upper layer hole 561, and a spring 57 is fixedly connected between the clamping block 53 and the bottom of the upper layer hole 561; the push ring 52 is sleeved outside the barrel body 55, and a push block 521 matched with the clamping block 53 is arranged on the push ring 52. The push block 521 is disposed within the upper bore 561 and slides within the upper bore 561 via the push ring 52. When the pushing block 521 is matched with the clamping block 53, the pushing block 53 is pressed down, the spring 57 is contracted, and the clamping block 53 locks the safety pin 54; when moving away from the latch 53, the latch 53 is disengaged from the safety pin 54 by the spring force of the spring 57.
The edge of the upper end of the side wall of the clamping block 53, which is close to the pushing block 521, is provided with a chamfer, and the edge of the lower end of the side wall of the pushing block 521, which is close to the clamping block 53, is provided with a fillet. This structure makes the pushing block 521 more convenient and smooth in the process of pressing down the clamping block 53.
The lower end of the clamping block 53 is provided with a plurality of claws 531 distributed along the axial direction of the barrel 55, and the length of the claws 531 is greater than the depth of the lower layer hole 56. When the push block 521 presses the clamping block 53, the claw 531 passes through the lower hole 56 to extend into the barrel 55 and is matched with the clamping groove 542 on the safety pin 54; when the pushing block 521 is separated from the clamping block 53, the claw 531 is separated from the clamping groove 542 under the action of the spring 57, and is retracted into the lower hole 56.
The safety pin 54 includes an active section 543, two ends of the active section 543 are fixedly connected with a clamping joint 541 respectively, and an outer diameter of the active section 543 is smaller than an outer diameter of the clamping joint 541; the clamping groove 542 is provided on the clamping connector 541. The action section 543 is a stress concentration part of the safety pin 54, and when a certain load is born, the action section 543 is easy to break, so that the overload protection function is realized. At the same time, the first and second quick-lock joints 51 and 5 are protected due to the fixed breaking position of the safety pin 54.
A breakage protection rope 6 is also connected between the first landing gear tie 7 and the traction belt group. The breakage protecting string 6 can prevent the separated first and second quick-lock joints 51 and 5 from injuring the apparatus due to rebound after the breaking of the safety pin 54.
The traction band group comprises a plurality of traction bands 2, and two adjacent traction bands 2 are connected through a shackle 3. The traction belt 2 is a flexible annular sling and comprises a bearing core and a traction belt protective sleeve sleeved on the outer side of the bearing core, wherein the bearing core is arranged in a stepless encircling and parallel mode, the traction belt protective sleeve is butted into an annular shape by a special wear-resistant sleeve, two annular eye belts made of wear-resistant materials are sewn on the traction belt 2, and the annular eye belts are used as traction points to be connected with the shackle 3.
As shown in fig. 7, the fixed pulley 1 comprises a traction pulley 11, and a groove 111 matched with the traction belt 2 is formed on the outer circular side wall of the traction pulley 11; the traction sheave 11 is rotatably connected to a traction sheave frame 13 via a sheave shaft 12. The grooves 111 cooperate with the profile of the traction belt 2 to facilitate movement of the traction belt 2 over the traction sheave 11. The traction belt 2, by moving over the traction sheave 11, balances the forces experienced by the present invention during traction.
In use, the first landing gear tether 7 and the second landing gear tether 8 are secured to the aircraft landing gear and the crown block 1 is secured to the towing apparatus. The safety pin 54 is selected and is respectively clamped and fixed with the first quick lock connector 51 and the second quick lock connector 5. When the present invention is subjected to excessive traction forces, the active segment 543 of the shear pin 54 breaks to protect the aircraft landing gear.
During traction, the dynamometer 4 can be controlled through infrared remote control, and the traction force can be monitored in real time. When the traction force is too large and the safety pin 54 is not broken, the traction can be stopped in time, so that the aircraft and traction equipment are protected.
When the shear pin 54 needs to be replaced, the push ring 52 is slid to move the push block 521 away from the latch 53. The latch 53 is disengaged from the latch groove 542 on the shear pin 54 (as shown in fig. 5) under the action of the spring 57, and the shear pin 54 can be removed.
Thereafter, the catching 541 portion of the new safety pin 54 is inserted into the tub 55 and pushes the push ring 52, so that the push block 521 contacts and presses down the catch 53. At this time, the claw 531 on the clamping block 53 extends into the clamping groove 542 through the lower hole 56 (as shown in fig. 6), and the safety pin 54 is clamped and fixed with the first quick lock connector 51 (the second quick lock connector 5).
The safe traction hanger disclosed by the invention is safe to use and convenient to maintain. The traction force can be displayed and recorded by the load cell 4 during the traction process. Meanwhile, the dynamometer 4 is monitored by means of a remote controller, so that the personal safety of on-site workers is guaranteed. In addition, through the second quick lock connector 5 and the first quick lock connector 51 which are clamped with the safety pin 54, on the premise of ensuring stable connection, the operation process of replacing the safety pin 54 is simplified, the workload of operators is reduced, and the maintenance efficiency is improved.
The foregoing description of the preferred embodiments of the invention is not intended to be limiting, but rather is intended to cover all modifications, equivalents, alternatives, and improvements that fall within the spirit and scope of the invention.
Claims (8)
1. A safety traction hanger, comprising:
one end of the traction band group is fixedly connected with the first landing gear tying belt (7) through an overload protection device, and the other end of the traction band group is fixedly connected with the second landing gear tying belt (8) through a dynamometer (4); the middle part of the traction band group is matched with the fixed pulley (1);
the overload protection device comprises a first quick locking connector (51) fixedly connected with a first falling frame tying belt (7) and a second quick locking connector (5) fixedly connected with a traction belt group, and the first quick locking connector and the second quick locking connector are respectively clamped with two ends of a safety pin (54); the dynamometer (4) is of an integrated structure, an LCD screen is arranged on the dynamometer (4), and the dynamometer (4) is provided with an infrared remote controller; the second quick lock connector (5) and the first quick lock connector (51) have the same structure and comprise a barrel body (55), a plurality of containing holes communicated with the outside and the inside of the barrel body (55) are formed in the outer circular side wall of the barrel body (55), and a clamping block (53) moving along the radial direction of the barrel body (55) is arranged in each containing hole;
and a clamping groove (542) which is matched with the clamping block (53) in a clamping way is formed in the outer circular side wall of the safety pin (54).
2. The safety traction hanger of claim 1, wherein: the accommodating hole is a stepped hole and comprises an upper layer hole (561) and a lower layer hole (56) arranged at the bottom of the upper layer hole (561); the clamping block (53) is arranged in the upper layer hole (561), and a spring (57) is fixedly connected between the clamping block (53) and the bottom of the upper layer hole (561);
the push ring (52) is sleeved on the outer side of the barrel body (55), and a push block (521) matched with the clamping block (53) is arranged on the push ring (52).
3. The safety traction hanger of claim 2, wherein: the clamping block (53) is provided with a chamfer near the edge of the upper end of the side wall of the pushing block (521), and the pushing block (521) is provided with a fillet near the edge of the lower end of the side wall of the clamping block (53).
4. The safety traction hanger of claim 2, wherein: the lower end of the clamping block (53) is provided with a plurality of clamping claws (531) which are axially distributed along the barrel body (55), and the length of each clamping claw (531) is greater than the depth of the lower layer hole (56).
5. The safety traction hanger of claim 1, wherein: the safety pin (54) comprises an action section (543), two ends of the action section (543) are fixedly connected with a clamping joint (541) respectively, and the outer diameter of the action section (543) is smaller than the outer diameter of the clamping joint (541);
the clamping groove (542) is arranged on the clamping connector (541).
6. The safety traction hanger of claim 1, wherein: and a breakage protection rope (6) is also connected between the first falling frame tying belt (7) and the traction belt group.
7. The safety traction hanger of claim 1, wherein: the traction band group comprises a plurality of traction bands (2), and two adjacent traction bands (2) are connected through a shackle (3).
8. The safety traction hanger of claim 7, wherein: the fixed pulley (1) comprises a traction pulley (11), and a groove (111) matched with the traction belt (2) is formed in the outer circular side wall of the traction pulley (11); the traction pulley (11) is rotationally connected with the traction pulley frame (13) through a pulley shaft (12).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610932452.2A CN106628230B (en) | 2016-10-31 | 2016-10-31 | Safe traction hanger |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610932452.2A CN106628230B (en) | 2016-10-31 | 2016-10-31 | Safe traction hanger |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106628230A CN106628230A (en) | 2017-05-10 |
| CN106628230B true CN106628230B (en) | 2023-09-12 |
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ID=58820897
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610932452.2A Active CN106628230B (en) | 2016-10-31 | 2016-10-31 | Safe traction hanger |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106628230B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3079821B1 (en) * | 2018-04-10 | 2020-05-08 | Airbus Operations | AIRCRAFT TOWING SYSTEM COMPRISING AN IMPROVED AIRCRAFT STEERING CONTROL DEVICE |
| CN116080922B (en) * | 2023-04-12 | 2023-07-25 | 四川航泰航空装备有限公司 | Movable hydraulic skid tractor mechanism |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2041113C1 (en) * | 1992-06-18 | 1995-08-09 | Конструкторское бюро транспортного машиностроения | Bicycle cart-trailer |
| TWM313849U (en) * | 2007-01-03 | 2007-06-11 | Enermax Technology Corp | Fastener structure |
| CN202320799U (en) * | 2011-09-28 | 2012-07-11 | 李荣田 | Special rescue traction hanger for aircraft |
| CN102846346A (en) * | 2012-09-29 | 2013-01-02 | 北京中法派尔特医疗设备有限公司 | Driving and locking device, and cutter stapler using same |
| CN103241080A (en) * | 2012-02-01 | 2013-08-14 | 迪尔公司 | Draft force sensor assembly |
| CN203924271U (en) * | 2014-06-27 | 2014-11-05 | 厦门瑞尔特卫浴科技股份有限公司 | A kind of water inlet valve for water tank mechanism easy to assemble |
| CN204124222U (en) * | 2014-08-08 | 2015-01-28 | 约斯特（中国）汽车部件有限公司 | A kind of trailer traction base |
| CN206494141U (en) * | 2016-10-31 | 2017-09-15 | 中安（天津）航空设备有限公司 | A kind of safety traction hanger |
-
2016
- 2016-10-31 CN CN201610932452.2A patent/CN106628230B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2041113C1 (en) * | 1992-06-18 | 1995-08-09 | Конструкторское бюро транспортного машиностроения | Bicycle cart-trailer |
| TWM313849U (en) * | 2007-01-03 | 2007-06-11 | Enermax Technology Corp | Fastener structure |
| CN202320799U (en) * | 2011-09-28 | 2012-07-11 | 李荣田 | Special rescue traction hanger for aircraft |
| CN103241080A (en) * | 2012-02-01 | 2013-08-14 | 迪尔公司 | Draft force sensor assembly |
| CN102846346A (en) * | 2012-09-29 | 2013-01-02 | 北京中法派尔特医疗设备有限公司 | Driving and locking device, and cutter stapler using same |
| CN203924271U (en) * | 2014-06-27 | 2014-11-05 | 厦门瑞尔特卫浴科技股份有限公司 | A kind of water inlet valve for water tank mechanism easy to assemble |
| CN204124222U (en) * | 2014-08-08 | 2015-01-28 | 约斯特（中国）汽车部件有限公司 | A kind of trailer traction base |
| CN206494141U (en) * | 2016-10-31 | 2017-09-15 | 中安（天津）航空设备有限公司 | A kind of safety traction hanger |
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| Publication number | Publication date |
|---|---|
| CN106628230A (en) | 2017-05-10 |
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