CN102008789A - Air landing device - Google Patents

Air landing device Download PDF

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Publication number
CN102008789A
CN102008789A CN 201010173509 CN201010173509A CN102008789A CN 102008789 A CN102008789 A CN 102008789A CN 201010173509 CN201010173509 CN 201010173509 CN 201010173509 A CN201010173509 A CN 201010173509A CN 102008789 A CN102008789 A CN 102008789A
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CN
China
Prior art keywords
tumbler
rope
supporting seat
transmission
bearing
Prior art date
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Granted
Application number
CN 201010173509
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Chinese (zh)
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CN102008789B (en
Inventor
何少敦
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Individual
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Individual
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Publication date
Application filed by Individual filed Critical Individual
Priority to CN2010101735098A priority Critical patent/CN102008789B/en
Priority to PCT/CN2011/000490 priority patent/WO2011131022A1/en
Publication of CN102008789A publication Critical patent/CN102008789A/en
Application granted granted Critical
Publication of CN102008789B publication Critical patent/CN102008789B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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    • AHUMAN NECESSITIES
    • A62LIFE-SAVING; FIRE-FIGHTING
    • A62BDEVICES, APPARATUS OR METHODS FOR LIFE-SAVING
    • A62B1/00Devices for lowering persons from buildings or the like
    • A62B1/06Devices for lowering persons from buildings or the like by making use of rope-lowering devices
    • A62B1/08Devices for lowering persons from buildings or the like by making use of rope-lowering devices with brake mechanisms for the winches or pulleys

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  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Emergency Lowering Means (AREA)

Abstract

An air landing device. In order to overcome the disadvantage of causing potential hazards to the users as a result of the unreasonable stress structure of the crankshaft of existing air landing devices which adopt a crankshaft and a speed limit piston, the present invention provides an air landing device, the technical scheme of which is that the gravity member is supported by a carrier; the carrier is fixedly connected with a rope; the rope is enwound on a winding disc; the winding disc is fixed on a rotation shaft; the rotation shaft is mounted on a bearer by a shaft base; a rotating member is disposed on the rotation shaft; a crankshaft is disposed on the rotating member; the crankshaft is connected with the piston rod of the speed limit piston; the speed limit piston is fixed on the bearer. The invention is characterized in that a supporting pedestal, which is muff-coupled on the outer side of the rotating member, is disposed; when rotating the rotating member, the inner surface of the supporting pedestal cooperates with the outer surface of the rotating member and the supporting pedestal plays a supporting role to the rotating member. The beneficial effect of the present invention is to provide a more reasonable stress structure of the crankshaft and ensure safe use.

Description

A kind of aerial landing-gear
Technical field
The present invention relates to a kind of landing-gear, relate in particular to a kind of aerial landing-gear.
Background technology
In daily life or work, people face a danger aloft through regular meeting, if when not having other method to escape, need be by aerial landing-gear escape, known aerial landing-gear is to comprise friction speed-limited, hand brake speed-limited and hydraulic damping speed-limited, the above two shortcomings are poor reliability, the latter is relatively simple for structure, performance is also reliable, CN87216143 discloses a kind of aerial landing-gear that plays the speed limit effect with piston and cam, but cam only bears pressure, does not bear pulling force, exists speed limit inhomogeneous in the landing process; ZL2003101127389 discloses a kind of principle that adopts bent axle to be connected with Hydraulic Adjustable Speed formula controller respectively with ZL2003201232361, but owing to adopt chain ladder, descent altitude is restricted; ZL2007202016917 discloses the aerial downfall equipment of a kind of hydraulic pressure speed-limited, and its structure was the rope formula, must at first correctly put on the lifesaving rope during use, causes certain trouble to the user; In the disclosed file of ZL2007201397042, because diagram is indeterminate, be difficult to determine the canoe of life line, do not know that its structure was the rope formula or hid the rope formula; In the aerial downfall equipment that adopts bent axle and speed limit piston now, because the speed limit piston is a Passive part, therefore the discontinuity of crankshaft two end, exists the irrational problem of bent axle force structure, causes certain potential danger to the user.
Summary of the invention
Exist the bent axle force structure unreasonable in order to overcome the aerial downfall equipment that adopts bent axle and speed limit piston now, cause the shortcoming of potential danger to the user, the present invention proposes a kind of aerial landing-gear, its principle is: bent axle is connected with the piston rod of speed limit piston, bent axle is mounted on the tumbler, tumbler is installed on the turning cylinder of rope drum, the rotation of rope drum drives turning cylinder and rotates, the moving axis revolution thereby the drive bent axle rotates, drive the piston operation thus, it is characterized in that: supporting seat of socket also in the outside of tumbler, supporting seat is fixed on the bearing.
The technical solution adopted for the present invention to solve the technical problems is, mainly comprise weight member, carry part, rope, the rope drum, turning cylinder, tumbler, bent axle, axle bed, bearing and speed limit piston, weight member is carried the part carrying by one, carrying part and rope is connected and fixed, lanyard also is wrapped on the rope drum, the rope drum is fixed on the turning cylinder, turning cylinder is installed on the bearing by axle bed, a tumbler is installed on turning cylinder, a bent axle is installed on tumbler, bent axle is connected with the piston rod of speed limit piston, and the speed limit piston is fixed on the bearing, when weight member descends, rope drives the rope drum and rotates, the rope drum drives and drives the tumbler rotation when turning cylinder rotates, thereby drives crank up, drives the piston rod operation during crank up, it is characterized in that: a supporting seat also is set, supporting seat is socketed in the outside of tumbler and supporting seat inner surface and tumbler outer surface and works in coordination, and when tumbler rotated, supporting seat played a supportive role to tumbler.
The invention has the beneficial effects as follows that a kind of aerial landing-gear that the present invention proposes is owing to adopt the structure of socket supporting seat outside tumbler, when tumbler rotates, supporting seat plays a supportive role to tumbler, makes the force structure of bent axle more reasonable, guarantees the safety of using.
Description of drawings
Fig. 1 is a kind of structural shape of existing product.
Fig. 2 is the another kind of structural shape of existing product.
Fig. 3, Fig. 4, Fig. 5, Fig. 6 are the structure charts of first embodiment of the invention.
Fig. 7, Fig. 8 are the structure charts of second embodiment of the invention.
Fig. 9, Figure 10 are the structure charts of third embodiment of the invention.
Among the figure: 1. weight member, 2. year part, 3. rope, 4. rope drum, 5. turning cylinder, 5.1 bent axles, 5.2 tumblers, 5.2.1 tumbler outer surface, 6.1,6.2 axle beds, 7 pistons, 7.1 piston rods, 8. bearing, 9. supporting seat, 9.1 supporting seat inner surfaces, 10 built-in parts, 10.1 built-in part inner surfaces, 11 transmissions, 11.1A, 11.1B transmission driving member, 11.2 power transmission shafts, 11.3A, 11.3B transmission axle bed.
The specific embodiment
Fig. 1 is a kind of structural shape of existing product, show among the figure, weight member 1 is by carrying part 2 carryings, carrying part 2 is connected and fixed with rope 3, rope 3 is wrapped on the rope drum 4, rope drum 4 is fixed on the turning cylinder 5, turning cylinder 5 is installed on the bearing 8 by axle bed 6.1 and 6.2, the piston rod 7.1 of piston 7 is connected with bent axle 5.1, rope 3 drives rope drum 4 and rotates, and rotates and drive bent axle 5.1 revolutions thereby drive turning cylinder 5, drives piston rod 7.1 operations during bent axle 5.1 revolutions, in this structure, because rope drum 4 is driving links and piston 7 is Passive parts, bent axle 5.1 two ends discontinuity, so the force structure of bent axle 5.1 is unreasonable, because the unreasonable problem of bent axle force structure causes certain potential danger to the user; This structure is different with the automobile engine crankshaft structure, and the automobile engine piston is a driving link with respect to bent axle, so the automobile engine crankshaft two ends are stressed evenly.
Fig. 2 is the another kind of structural shape of existing product, show among the figure, a tumbler 5.2 is installed on the turning cylinder 5, a bent axle 5.1 is installed on the tumbler 5.2, therefore, rope 3 drives rope drum 4 and rotates, and rotates thereby drive turning cylinder 5, and turning cylinder 5 drives tumbler 5.2 and rotates when rotating, thereby drive bent axle 5.1 revolutions, the piston rod 7.1 of piston 7 is connected with bent axle 5.1, drives piston rod 7.1 operations during bent axle 5.1 revolutions, in this structure, because tumbler 5.2 is mounted in the axle head of rotating shaft 5, be a kind of hanging structure, cause mounted thereto bent axle 5.1 force structures unreasonable, cause certain potential danger to the user.
The structural representation of Fig. 3, Fig. 4, Fig. 5, Fig. 6 first embodiment of the invention;
Show among Fig. 3, weight member 1 is by carrying part 2 carryings, carrying part 2 is connected and fixed with rope 3, rope 3 is fixing and is wrapped on the rope drum 4, rope drum 4 is fixed on the turning cylinder 5, turning cylinder 5 is installed on the bearing 8 by axle bed 6.1 and 6.2, a tumbler 5.2 is installed on the turning cylinder 5, a bent axle 5.1 is installed on the tumbler 5.2, and the piston rod 7.1 of piston 7 is connected with bent axle 5.1, when weight member 1 descends, rope 3 drives rope drum 4 and rotates, rotate thereby drive turning cylinder 5, turning cylinder 5 drives tumbler 5.2 and rotates when rotating, thereby drives bent axle 5.1 revolutions, drive piston rod 7.1 operations during bent axle 5.1 revolutions, it is characterized in that, supporting seat 9 of socket also in tumbler 5.2 outsides, supporting seat 9 is fixed on the bearing 8;
Fig. 4 is the structural representation behind local the amplification, show among the figure that when supporting seat 9 was socketed in tumbler 5.2 outsides, the outer surface 5.2.1 of the inner surface of supporting seat 9 and tumbler 5.2 worked in coordination, when tumbler 5.2 rotated, 9 pairs of tumblers 5.2 of supporting seat played a supportive role;
Fig. 5 is the three-dimensional effect diagram after tumbler 5.2 is taken apart with supporting seat 9;
Fig. 6 is that supporting seat 9 is socketed in the three-dimensional effect diagram on the tumbler 5.2;
In first embodiment, rope 3 is fixing and is wrapped on the rope drum 4, is to hide rope-like structure, 1 of gravity can be people or object, and bearing 8 can be a housing, during use, bearing 8 is fixed on eminence, and weight member 1 can be by carrying part 2 from the eminence safe falling.
The structure chart of Fig. 7, Fig. 8 second embodiment of the invention, wherein Fig. 7 is a structural representation, Fig. 8 is the structural representation behind local the amplification, show among the figure that different with first embodiment is, in the present embodiment, supporting seat 9 inside also are provided with a built-in part 10, the inner surface 10.1 of built-in part 10 is worked in coordination with the outer surface 5.2.1 of tumbler 5.2, and when tumbler 5.2 rotated, supporting seat 9 played a supportive role by 10 pairs of tumblers 5.2 of built-in part; Built-in part 10 can be a bearing, also can be axle sleeve.
Fig. 9, Figure 10 is the structure chart of third embodiment of the invention, wherein Fig. 9 is a structural representation, Figure 10 is the structural representation behind local the amplification, show among the figure, different with first embodiment is, in the present embodiment, also set up a transmission 11, mainly comprise transmission driving member 11.1A and 11.1B, power transmission shaft 11.2, transmission axle bed 11.3A and 11.3B, wherein, transmission driving member 11.1A is installed on the turning cylinder 5, and transmission driving member 11.1B is installed on the power transmission shaft 11.2, power transmission shaft 11.2 is installed on the bearing 8 by transmission axle bed 11.3A and 11.3B, in the present embodiment, tumbler 5.2 is mounted on the power transmission shaft 11.2, bent axle 5.1 is installed on the tumbler 5.2, supporting seat 9 of socket also in tumbler 5.2 outsides, supporting seat 9 is fixed on the bearing 8, the outer surface 5.2.1 of the inner surface of supporting seat 9 and tumbler 5.2 works in coordination, when weight member 1 descends, rope 3 drives rope drum 4 and rotates, thereby driving turning cylinder 5 rotates, the driving member 11.1A of drive transmission 11 rotated when turning cylinder 5 rotated, thereby drive driving member 11.1B rotates, and then drove power transmission shaft 11.2 rotations and drive tumbler 5.2 rotations, make bent axle 5.1 revolutions, drive piston rod 7.1 operations during bent axle 5.1 revolutions, when tumbler 5.2 rotated, 9 pairs of tumblers 5.2 of supporting seat played a supportive role;
In the 3rd embodiment, transmission can be the chain transmission, also can be band transmission or gear drive, or known other transmission;
In the 3rd embodiment, transmission driving member 11.1A also can select directly to be fixed on the rope drum 4;
In the 3rd embodiment, can also increase by second feature among the embodiment, in supporting seat 9 inside built-in part is set.

Claims (6)

1. aerial landing-gear, mainly comprise weight member, carry part, rope, the rope drum, turning cylinder, tumbler, bent axle, axle bed, bearing and speed limit piston, weight member is carried the part carrying by one, carrying part and rope is connected and fixed, lanyard also is wrapped on the rope drum, the rope drum is fixed on the turning cylinder, turning cylinder is installed on the bearing by axle bed, a tumbler is installed on turning cylinder, a bent axle is installed on tumbler, bent axle is connected with the piston rod of speed limit piston, and the speed limit piston is fixed on the bearing, under the effect of weight member, rope drives the rope drum and rotates, the rope drum drives and drives the tumbler rotation when turning cylinder rotates, thereby drives crank up, drives the piston rod operation during crank up, it is characterized in that: a supporting seat also is set, described supporting seat is socketed in the outside of tumbler and supporting seat inner surface and tumbler outer surface and works in coordination, and when tumbler rotated, supporting seat played a supportive role to tumbler.
2. aerial landing-gear according to claim 1 is characterized in that: described supporting seat is fixed on the bearing.
3. aerial landing-gear according to claim 1, it is characterized in that: described supporting seat inside also is provided with a built-in part, described built-in part is socketed in the outside of tumbler and built-in part inner surface and tumbler outer surface and works in coordination, when tumbler rotated, supporting seat played a supportive role to tumbler by built-in part.
4. aerial landing-gear according to claim 3 is characterized in that: described built-in part can be a bearing, also can be axle sleeve.
5. aerial landing-gear according to claim 1, it is characterized in that: also set up a transmission, described transmission mainly comprises transmission driving member, power transmission shaft and transmission axle bed, a driving member of transmission is installed on the turning cylinder of described rope drum, and another driving member of transmission is installed on the power transmission shaft of described transmission, power transmission shaft is installed on the bearing by the transmission axle bed, described tumbler is mounted on the power transmission shaft, bent axle is installed on tumbler, bent axle is connected with the piston rod of speed limit piston, and the speed limit piston is fixed on the bearing.
6. aerial according to claim 1 or 5 landing-gear, it is characterized in that: a driving member of transmission is installed on the described rope drum, and another driving member of transmission is installed on the power transmission shaft of described transmission.
CN2010101735098A 2010-04-24 2010-04-24 Air landing device Expired - Fee Related CN102008789B (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
CN2010101735098A CN102008789B (en) 2010-04-24 2010-04-24 Air landing device
PCT/CN2011/000490 WO2011131022A1 (en) 2010-04-24 2011-03-23 Descent device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2010101735098A CN102008789B (en) 2010-04-24 2010-04-24 Air landing device

Publications (2)

Publication Number Publication Date
CN102008789A true CN102008789A (en) 2011-04-13
CN102008789B CN102008789B (en) 2012-05-30

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WO (1) WO2011131022A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012065396A1 (en) * 2010-11-19 2012-05-24 He Shaodun Descent apparatus
CN102814009A (en) * 2011-06-08 2012-12-12 何少敦 Aerial landing device
CN103656882A (en) * 2013-12-20 2014-03-26 陈洪灿 Shared type speed-adjustable descent control device

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3924218A1 (en) * 1989-07-21 1991-01-24 Alfred Dipl Phys Seeger Cable lowering appts. for e.g. loads - has automatic braking system with piston cylinder units on both sides of the roller
CN1597015A (en) * 2004-07-26 2005-03-23 王成鹏 High altitude self-saving device
CN2734256Y (en) * 2004-09-14 2005-10-19 周成方 High-building life-saving rope
CN101254330A (en) * 2007-03-02 2008-09-03 项敏 Non-mechanical friction damping automatically controlling speed method and device thereof thereof
CN101279121A (en) * 2008-06-03 2008-10-08 吴育添 Life saving device in high building
CN201676419U (en) * 2010-04-24 2010-12-22 何少敦 Air landing device

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1082932A (en) * 1992-08-27 1994-03-02 刘安源 Escape device for high-rise buildings
CN2446999Y (en) * 2000-10-31 2001-09-12 吴喆 Self-life-saving device for fire-fighting in high building
CN2468512Y (en) * 2001-03-19 2002-01-02 罗忠 Hydraulic and lower speed life-saving device
JP2006305013A (en) * 2005-04-27 2006-11-09 Nhk Spring Co Ltd Slowly descending apparatus used for escaping from high place

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3924218A1 (en) * 1989-07-21 1991-01-24 Alfred Dipl Phys Seeger Cable lowering appts. for e.g. loads - has automatic braking system with piston cylinder units on both sides of the roller
CN1597015A (en) * 2004-07-26 2005-03-23 王成鹏 High altitude self-saving device
CN2734256Y (en) * 2004-09-14 2005-10-19 周成方 High-building life-saving rope
CN101254330A (en) * 2007-03-02 2008-09-03 项敏 Non-mechanical friction damping automatically controlling speed method and device thereof thereof
CN101279121A (en) * 2008-06-03 2008-10-08 吴育添 Life saving device in high building
CN201676419U (en) * 2010-04-24 2010-12-22 何少敦 Air landing device

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012065396A1 (en) * 2010-11-19 2012-05-24 He Shaodun Descent apparatus
CN102814009A (en) * 2011-06-08 2012-12-12 何少敦 Aerial landing device
WO2012167501A1 (en) * 2011-06-08 2012-12-13 He Shaodun Aerial landing device
CN102814009B (en) * 2011-06-08 2015-04-22 何少敦 Aerial landing device
CN103656882A (en) * 2013-12-20 2014-03-26 陈洪灿 Shared type speed-adjustable descent control device

Also Published As

Publication number Publication date
WO2011131022A1 (en) 2011-10-27
CN102008789B (en) 2012-05-30

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