CN209848166U - Dual-damping high-altitude descent control device - Google Patents

Dual-damping high-altitude descent control device Download PDF

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Publication number
CN209848166U
CN209848166U CN201920088171.2U CN201920088171U CN209848166U CN 209848166 U CN209848166 U CN 209848166U CN 201920088171 U CN201920088171 U CN 201920088171U CN 209848166 U CN209848166 U CN 209848166U
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CN
China
Prior art keywords
gear
cable
wheel
suspension
transmission
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Expired - Fee Related
Application number
CN201920088171.2U
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Chinese (zh)
Inventor
李宇
罗建
雷梓兴
金星
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Liuzhou Railway Vocational Technical College
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Liuzhou Railway Vocational Technical College
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Priority to CN201920088171.2U priority Critical patent/CN209848166U/en
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Publication of CN209848166U publication Critical patent/CN209848166U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

A double-damping high-altitude descent control device comprises a cable-suspension wheel mechanism, a transmission and an air damping energy dissipater; the cable suspension wheel mechanism comprises a cable suspension wheel box, a cable suspension wheel arranged in the cable suspension wheel box, a main shaft and a cable suspension; the transmission comprises a transmission box body, a ratchet mechanism, a driven shaft, a gear I, a gear II, a gear III and a gear IV, wherein the ratchet mechanism is arranged in the transmission box body; the air damping energy dissipater comprises an air damper, a rotating shaft, a pair of magnets and a rotor arranged on the rotating shaft; the main shaft can only drive the gear III to rotate in a single direction through the ratchet mechanism, the gear III drives the gear I, the gear I drives the gear II through the driven shaft, the gear II drives the gear IV, the gear IV drives the rotating shaft extending into the transmission box body to rotate, and therefore the rotating shaft drives the air damping type energy dissipater. The utility model discloses a dual damping high altitude ware of slowly falling not only can be quick retrieve the rope but also the required space of erection equipment is little, slowly fall the ability reinforce.

Description

Dual-damping high-altitude descent control device
Technical Field
The utility model relates to a rescue equipment, concretely relates to dual damping high altitude ware that slowly falls.
Background
The prior art application number is: 201310289768.0 discloses a high-altitude damping descent control device, which belongs to rescue equipment and mainly solves the self-rescue problem when disasters such as earthquake, fire and the like happen to a high-rise building. The structure of the elevator car safety rope comprises a fixed shaft, a speed changer, an impeller assembly, a spring damper, a reel, a safety rope and a car, wherein the speed changer is arranged on the fixed shaft, the impeller assembly is connected with the speed changer through gear engagement, and the tail end of the safety rope is connected with the car. When the elevator car is used, potential energy released when the elevator car and passengers descend in a gravity field is converted into air kinetic energy, the safety rope drives the scroll to rotate at a low speed, damping power is increased along with the increase of descending speed and height, the impeller set is subjected to air resistance, power consumption overcomes the gravity acceleration of the elevator car to limit the rotating speed of the scroll within a reasonable range, and the purpose that the elevator car descends at a constant speed is achieved. But the resistance is also generated by the reverse rotation of the impeller when the rope is recovered, and the recovery is difficult; and the impeller needs to be subjected to enough air resistance to rotate so as to achieve the aim of slow descent, so that the volume of the impeller is large, and the space required by the installation equipment is large.
Disclosure of Invention
The utility model aims at providing a double damping high altitude descent control device which not only can rapidly recover a rope, but also has small space required by installation equipment and strong descent control capability; to solve the above problems of the prior art.
The technical scheme for solving the problems is as follows: a double-damping high-altitude descent control device comprises a cable-suspension wheel mechanism, a transmission and an air damping energy dissipater;
the cable suspension wheel mechanism comprises a cable suspension wheel box, a cable suspension wheel arranged in the cable suspension wheel box, a main shaft and a cable suspension; the suspension cable wheel is arranged on the main shaft, and the suspension cable is wound on the suspension cable wheel; the free end of the suspension cable extends out of the suspension cable wheel box and is sequentially provided with a buffer spring and a safety hanging ring; one end of the main shaft extends out of the cable wheel box and is arranged into a square head, and the other end of the main shaft extends into the transmission; the upper part of the suspension cable wheel box is provided with a mounting hole;
the transmission comprises a transmission case, a ratchet mechanism and a driven shaft, wherein the ratchet mechanism and the driven shaft are installed inside the transmission case; the ratchet mechanism comprises a ratchet wheel and a pawl; the ratchet wheel is fixedly connected with a main shaft extending into the transmission, a gear III is sleeved outside the ratchet wheel, and the pawl is installed on the gear III; the driven shaft is fixedly connected with a gear I and a gear II; the gear III is meshed with the gear I;
the air damping energy dissipater comprises an air damper, a rotating shaft, a pair of magnets and a rotor arranged on the rotating shaft; one end of the rotating shaft extends into the transmission box body and is provided with a gear IV, and the gear IV is fixedly connected with the rotating shaft and is meshed with the gear II; the other end of the rotating shaft is positioned outside the transmission box body and is fixedly connected with the rotor and the air damper from inside to outside in sequence; the pair of magnets are mounted outside the transmission case and located on the outer peripheral surface of the rotor.
The further technical scheme is as follows: the air damper is a fan, a fan or an impeller.
The further technical scheme is as follows: and a cover plate is arranged on the cable suspension wheel box.
The further technical scheme is as follows: and a buffer spring sheath is arranged outside the buffer spring.
The further technical scheme is as follows: the rotor is composed of an iron core and a winding.
Due to the adoption of the technical scheme, the utility model relates to a dual damping high altitude descent control device has following characteristics and beneficial effect:
(1) the double-damping high-altitude descent control device of the utility model has the advantages that the ratchet mechanism is arranged in the gearbox to achieve the purpose of quickly and conveniently recovering the rope; the ratchet mechanism is added, so that the rope can be rapidly recovered, can be repeatedly and continuously used for many times, has high efficiency, and is favorable for collective escape.
(2) The rotor composed of the iron core and the winding is installed on the rotating shaft of the air damping type energy dissipater so as to achieve the purpose of reducing the volume of the air damping type energy dissipater. The brake torque of the interaction of the magnet and the rotor is increased, so that the structure is simple, the size is small, the use is convenient, the control is easy, and special training is not needed.
The technical features of a dual damping high altitude descent control device according to the present invention will be further described with reference to the accompanying drawings and embodiments.
Drawings
FIG. 1 is a schematic structural view of a dual-damping high-altitude descent control device of the present invention;
FIG. 2 is a schematic view of the ratchet mechanism of the present invention;
fig. 3 is an installation schematic diagram of the present invention.
In the figure:
1-suspension cable wheel, 2-main shaft, 3-square head, 4-cover plate, 5-ratchet wheel, 6-suspension cable wheel box, 7-gear I and 8-mounting hole;
9-a transmission box body, 10-gears II and 11-driven shafts, 12-gears III and 13-air dampers;
14. 16-a magnet; 15-rotor, 17-rotating shaft, 18-gear IV, 19-suspension cable and 20-buffer spring;
21-a buffer spring sheath, 22-a safe hanging ring, 23-a pawl, 24-a double-damping high-altitude descent control device, 25-a positioning set screw and 26-a positioning hook.
Detailed Description
As shown in fig. 1, a dual-damping high altitude descent control device comprises a rope-suspension wheel mechanism, a transmission and an air damping energy dissipater;
the cable suspension wheel mechanism comprises a cable suspension wheel box 6, a cable suspension wheel 1 arranged in the cable suspension wheel box 6, a main shaft 2 and a cable suspension 19; the suspension cable wheel 1 is arranged on the main shaft 2, and the suspension cable 19 is wound on the suspension cable wheel 1; the free end of the suspension cable 19 extends out of the suspension cable wheel box 6 and is sequentially provided with a buffer spring 20 and a safety hanging ring 22; a buffer spring sheath 21 is arranged outside the buffer spring 20. The buffer spring 20 and the buffer spring sheath 21 are used for buffering the impact force when the evacuee begins to descend, and the safety lifting ring 22 is used for being connected with a safety belt.
One end of the main shaft 2 extends out of the suspension cable wheel box 6 and is arranged into a square head 3, and the other end of the main shaft extends into the transmission box body 9; the upper part of the suspension cable wheel box 6 is provided with a mounting hole 8; the cable suspension wheel box 6 is provided with the cover plate 4, the cover plate 4 is convenient to open or close the cable suspension wheel box 6, and installation and maintenance of all parts in the cable suspension wheel box 6 are facilitated.
The transmission comprises a transmission case 9, a ratchet mechanism (see fig. 2) arranged in the transmission case and a driven shaft 11; the ratchet mechanism comprises a ratchet wheel 5 and a pawl 23; the ratchet wheel 5 is fixedly connected with the main shaft 2 extending into the transmission box body 9, a gear III 12 is sleeved outside the ratchet wheel 5, and the pawl 23 is installed on the gear III 12; a gear I7 and a gear II 10 are coaxially and fixedly connected to the driven shaft 11 side by side; the gear III 12 is meshed with the gear I7;
the air damping energy dissipater comprises an air damper 13, a rotating shaft 17, a pair of magnets 14 and 16 (an N pole and an S pole) and a rotor 15 arranged on the rotating shaft 17; one end of the rotating shaft 17 extends into the transmission box body 9 and is provided with a gear IV 18, and the gear IV 18 is fixedly connected with the rotating shaft 17 and is meshed with the gear II 10; the other end of the rotating shaft 17 is positioned outside the transmission box body 9 and is fixedly connected with the rotor 15 and the air damper 13 from inside to outside in sequence; the pair of magnets are provided outside the transmission case 9 and on the outer peripheral surface of the rotor 15.
Therefore, the main shaft 2 can only drive the gear III 12 to rotate in one direction through the ratchet wheel 5, the gear III 12 drives the gear I7, the gear I7 drives the gear II 10 through the shaft 11, the gear II 10 drives the gear IV 18, and the gear IV 18 drives the rotating shaft 17 extending into the box body of the transmission to rotate, so that the rotating shaft 17 drives the air damping type energy dissipater.
In this embodiment, the air damper 13 is either a fan, a blower, or an impeller. The air is transmitted to the air damper through the speed changer, and the air damper is used for enabling people and objects to descend at a constant speed when the air damper rotates. The rotor 15 is composed of an iron core and a winding. The rotor interacts with a pair of magnets fixed on the outer side of the gearbox casing to enable the rotating rotor to cut the magnetic lines of force of the fixed magnetic field to generate braking torque, so that resistance is further increased, and the size of the impeller is reduced.
When the fire escape device is used, as shown in fig. 3, when a fire breaks out on a floor, an escape person firstly sleeves the positioning hook 26 on the vertical low wall of the window, and the positioning hook 26 is firmly fixed on the wall by the positioning set screw 25. Then, the mounting hole 8 at the upper end of the double-damping high-altitude descent control device 24 is hung on the positioning hook 26, the safety belt is tied, and after the hook of the belt is sleeved on the safety hanging ring 22, the escape personnel can climb out of the window and slowly descend to the ground for escape. The working principle is as follows: the weight G of the escape personnel is transmitted to the suspension cable 19 through the safety lifting ring 22 and the buffer spring 20, a driving torque T is generated on the main shaft 2 to drive the ratchet wheel 5, then the gear III 12 is driven, the gear III 12 drives the gear I7, the gear II 10 and the gear I7 rotate coaxially, the gear II 10 drives the gear IV 18, and finally the gear IV 18 rotates to drive the rotating shaft 17, so that the rotating shaft 17 rotates to drive the air damper 13 and the rotor 15 to rotate, the speed of descending the human body is kept at a nearly constant speed and in a reasonable range in the interaction process, the escape personnel can safely land in a very short time range to quickly escape. Meanwhile, a rotor is arranged on the impeller shaft and interacts with a pair of magnets fixed on the outer side of the gearbox body, so that the rotating rotor cuts magnetic lines of force of a fixed magnetic field to generate braking torque, the resistance is further increased, and the size of the impeller is reduced. And because the ratchet wheel 5 is arranged, the driving torque T can drive the air damper 13 only in one specified steering direction. Therefore, after the escape person uses the handle, the ratchet wheel 5 is reversed through the square head 3 on the main shaft 2, and the suspension cable 19 is retracted to the suspension cable wheel 1 for the use of the 2 nd person. Due to the action of the unidirectional transmission torque of the ratchet wheel, the gear III 12 is not driven by the ratchet wheel 5 when the suspension cable 19 is recovered, so that great force is not needed when the suspension cable 19 is recovered, the speed of recovering the suspension cable 19 can be increased, and the time is saved.
The above only is the preferred embodiment of the present invention, not limiting the scope of the present invention, all the equivalent structure changes made by the content of the present invention or the direct or indirect application attached to the technical field of other related products are included in the patent protection scope of the present invention.

Claims (5)

1. The utility model provides a dual damping high altitude ware that slowly falls which characterized in that: the system comprises a cable suspension wheel mechanism, a speed changer and an air damping energy dissipater;
the cable suspension wheel mechanism comprises a cable suspension wheel box (6), a cable suspension wheel (1) arranged in the cable suspension wheel box (6), a main shaft (2) and a cable suspension (19); the suspension cable wheel (1) is arranged on the main shaft (2), and the suspension cable (19) is wound on the suspension cable wheel (1); the free end of the suspension cable (19) extends out of the suspension cable wheel box (6) and is sequentially provided with a buffer spring (20) and a safety lifting ring (22); one end of the main shaft (2) extends out of the suspension cable wheel box (6) and is arranged into a square head (3), and the other end of the main shaft extends into the transmission; the upper part of the suspension cable wheel box (6) is provided with a mounting hole (8);
the transmission comprises a transmission case (9), a ratchet mechanism and a driven shaft (11), wherein the ratchet mechanism is installed inside the transmission case; the ratchet mechanism comprises a ratchet wheel (5) and a pawl (23); the ratchet wheel (5) is fixedly connected with a main shaft (2) extending into the transmission, a gear III (12) is sleeved outside the ratchet wheel (5), and the pawl (23) is installed on the gear III (12); a gear I (7) and a gear II (10) are fixedly connected to the driven shaft (11); the gear III (12) is meshed with the gear I (7);
the air damping energy dissipater comprises an air damper (13), a rotating shaft (17), a pair of magnets (14, 16) and a rotor (15) arranged on the rotating shaft (17); one end of the rotating shaft (17) extends into the transmission box body (9) and is provided with a gear IV (18), and the gear IV (18) is fixedly connected with the rotating shaft (17) and is meshed with the gear II (10); the other end of the rotating shaft (17) is positioned outside the transmission box body (9) and is fixedly connected with the rotor (15) and the air damper (13) from inside to outside in sequence; the pair of magnets are mounted outside the transmission case (9) and located on the outer peripheral surface of the rotor (15).
2. The dual damping high altitude descent control device of claim 1, wherein: the air damper (13) is either a fan or a blower or an impeller.
3. The dual damping high altitude descent control device of claim 1, wherein: and a cover plate (4) is arranged on the suspension cable wheel box (6).
4. The dual damping high altitude descent control device of claim 1, wherein: a buffer spring sheath (21) is arranged outside the buffer spring (20).
5. The dual damping high altitude descent control device of claim 1, wherein: the rotor (15) is composed of an iron core and a winding.
CN201920088171.2U 2019-01-18 2019-01-18 Dual-damping high-altitude descent control device Expired - Fee Related CN209848166U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201920088171.2U CN209848166U (en) 2019-01-18 2019-01-18 Dual-damping high-altitude descent control device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201920088171.2U CN209848166U (en) 2019-01-18 2019-01-18 Dual-damping high-altitude descent control device

Publications (1)

Publication Number Publication Date
CN209848166U true CN209848166U (en) 2019-12-27

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109701171A (en) * 2019-01-18 2019-05-03 柳州铁道职业技术学院 A kind of Double damping high-altitude slow-falling device
CN113101555A (en) * 2021-04-08 2021-07-13 山东电子职业技术学院 High-rise fire escape device
CN114642838A (en) * 2022-03-10 2022-06-21 苏州普瑞川传动科技有限公司 Damping mechanism, transmission mechanism and high-altitude slow descending device

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109701171A (en) * 2019-01-18 2019-05-03 柳州铁道职业技术学院 A kind of Double damping high-altitude slow-falling device
CN113101555A (en) * 2021-04-08 2021-07-13 山东电子职业技术学院 High-rise fire escape device
CN113101555B (en) * 2021-04-08 2022-04-08 山东电子职业技术学院 High-rise fire escape device
CN114642838A (en) * 2022-03-10 2022-06-21 苏州普瑞川传动科技有限公司 Damping mechanism, transmission mechanism and high-altitude slow descending device

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

Granted publication date: 20191227

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