CN103670017A - Mechanical reserve parachute unlocking device - Google Patents

Mechanical reserve parachute unlocking device Download PDF

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Publication number
CN103670017A
CN103670017A CN201310615763.2A CN201310615763A CN103670017A CN 103670017 A CN103670017 A CN 103670017A CN 201310615763 A CN201310615763 A CN 201310615763A CN 103670017 A CN103670017 A CN 103670017A
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CN
China
Prior art keywords
block
reserve parachute
purl
soft
brake
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Pending
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CN201310615763.2A
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Chinese (zh)
Inventor
陈明森
李勇华
王学锋
万汉桥
樊孝英
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Wuhan Aviation Instrument Co Ltd
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Wuhan Aviation Instrument Co Ltd
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Publication date
Application filed by Wuhan Aviation Instrument Co Ltd filed Critical Wuhan Aviation Instrument Co Ltd
Priority to CN201310615763.2A priority Critical patent/CN103670017A/en
Publication of CN103670017A publication Critical patent/CN103670017A/en
Pending legal-status Critical Current

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Abstract

The invention belongs to the field of aviation emergency escapement and particularly relates to a mechanical reserve parachute unlocking device comprising a timing mechanism, a power mechanism and a locking control mechanism. A compression spring is used as a power source. A steel cable is used as a power output part. A gear system is used as a timing mechanism simple and compact in structure. Compared to existing electronic unlocking devices, the mechanical reserve parachute unlocking device has the advantages of low cost, convenience of setting, simplicity of storage and application, availability for use just with simple learning, stable performance, no safety hazard, resistance to electromagnetic interference effect, no power consumption, reusability, long service life and the like. Compared to existing hand-pull unlocking manners, the mechanical reserve parachute unlocking device has the advantages that operating process is simple, training time for parachutists is short, safety is high, and the effect of psychological and physiological factors of parachutists is avoided.

Description

A kind of mechanical type reserve parachute lockaid gun
Technical field
The invention belongs to aviation lifesaving field, particularly relate to a kind of mechanical type reserve parachute lockaid gun.
Background technology
The mode of opening at present reserve parachute mainly contains two kinds, and the first is that parachutist pulls parachute-opening, and the second is to use electronic type lockaid gun.
Present stage is mainly used the mode of handle draw ring to open reserve parachute, and when parachutist parachutes, when main chute system breaks down can not parachute-opening time, parachutist need manually pull open reserve parachute.But the inevitably impact of the factor such as parachutist Yin Shengli, psychology under specific environment, in waking state not, can not manual unlocking reserve parachute and cause casualty accident.
Electronic type lockaid gun popularity rate is not high.Electronic type lockaid gun is experienced force value by pressure sensor, and force value converts height above sea level value to, and the height above sea level difference in the unit interval is exactly the speed of reserve parachute landing.If speed surpasses certain value, the mode that lockaid gun cuts umbrella rope by electronic cutting unit is automatically opened reserve parachute.Electronic type cutter mainly triggers initiator (fire attack product) by electricity and cuts rope, and initiator comprises control section (circuit) and operating part (fire attack product).Fire attack product storage period is short, use and store certain risk, produces, transportation, stores all very strictly, and fire attack product can only disposablely be used, whole, use cost is higher, has the risk of electromagnetic interference during use.Electronic unlocking device is only used for novel reserve parachute, the manner of packing of the inapplicable active service reserve parachute of electronic unlocking device, and the present invention can be used for the repacking that adds of all reserve parachutes.
Summary of the invention
The object of the invention is: a kind of mechanical type reserve parachute lockaid gun is provided, and the work of controlling actuating unit by locking controlling organization is to realize in predetermined time power output and displacement.
Technical scheme of the present invention is: a kind of mechanical type reserve parachute lockaid gun, comprise time movement, actuating unit and locking controlling organization, wherein:
Actuating unit comprises the piston tube 4, the brake(-holder) block 6 that are contained on casing assembly 5, is contained in power spring 2 and piston 1 in piston tube 5, power spring 2 one end withstand on piston tube 4 right sides, the other end keeps contacting with piston 1 under nature, pulley 14 for locking is housed in the lower end of piston 1, and pulley 14 stretches out the groove on 4 times faces of cylinder of piston tube and can in groove, slide; Brake(-holder) block 6 is hinged on time movement, when pulley goes to the soffit cunning of brake(-holder) block 6, brake(-holder) block 6 is rotated counterclockwise, and pulley 14 is from the soffit of brake(-holder) block 6 slips over, brake(-holder) block 6 turns clockwise under elastomeric element effect, and pulley 14 is stuck on the end face of brake(-holder) block 6;
Time movement comprises gear assembly 13, regulating wheel 11 and the stabilizer 8 that forms driving-chain, and gear assembly 13, under the promotion of actuating unit, promotes stabilizer 8 by regulating wheel 11 and swings timing;
Locking controlling organization comprises the first soft purl 9 of soft purl 7, second and block combination 10, in block combination 10, back-moving spring 12 is housed; The first soft purl 7 inserts after the soft purl 9 of time movement finger lock stabilizer 8, the second inserts block combination 10 and pushes back-moving spring 12 open.
Described power spring 2 is by one or a plurality of spring forms.
Described gear assembly 13 is one or more levels gear.
Described block combination 10 can be contained on flat sheet combination or be contained on casing assembly 5.
Described block combination 10 can act on any one-level gear.
Described back-moving spring 12 can be torsion spring or flat spring.
The first described soft purl 7 and the second soft purl 9 are flexible latch or rigidity latch.
On piston 1, be equipped with for the cable wire 3 of locking, cable wire 3 can be flexible cable or rigid posts.
Advantage of the present invention is: the present invention adopts Compress Spring as power source, adopts cable wire as the output of power, adopts gear train as time movement, simple and compact for structure; Compare with existing electronic type lockaid gun, have cost low, arrange conveniently, store, use simple, only need simple study to use, the advantage such as stable performance, without potential safety hazard, is not subject to electromagnetic interference influence, and electric consumption not can Reusability, and the life-span is long.Compare with the existing parachute-opening mode that pulls, have that operation sequence is simple, parachutist's training time is short, safe, be not subject to the advantages such as parachutist's psychology physiological factor affects.
Accompanying drawing explanation
Fig. 1 is mechanical type reserve parachute lockaid gun structural representation.
In figure: 1. piston, 2. power spring, 3. cable wire, 4. piston tube, 5. casing assembly, 6. brake(-holder) block, 7. the first soft purl, 8. stabilizer, 9. the second soft purl, 10. block combination, 11. regulating wheels, 12. back-moving springs, 13. gear assemblies, 14. pulleys.
The specific embodiment
Embodiment 1: below the present invention is described in further details.As shown in Figure 1,
A mechanical type reserve parachute lockaid gun, comprises time movement, actuating unit and locking controlling organization, wherein:
Actuating unit comprises the piston tube 4, the brake(-holder) block 6 that are contained on casing assembly 5, is contained in power spring 2 and piston 1 in piston tube 5, power spring 2 one end withstand on piston tube 4 right sides, the other end keeps contacting with piston 1 under nature, pulley 14 for locking is housed in the lower end of piston 1, and pulley 14 stretches out the groove on 4 times faces of cylinder of piston tube and can in groove, slide; Brake(-holder) block 6 is hinged on time movement, when pulley goes to the soffit cunning of brake(-holder) block 6, brake(-holder) block 6 is rotated counterclockwise, and pulley 14 is from the soffit of brake(-holder) block 6 slips over, brake(-holder) block 6 turns clockwise under elastomeric element effect, and pulley 14 is stuck on the end face of brake(-holder) block 6;
Time movement comprises gear assembly 13, regulating wheel 11 and the stabilizer 8 that forms driving-chain, and gear assembly 13, under the promotion of actuating unit, promotes stabilizer 8 by regulating wheel 11 and swings timing;
Locking controlling organization comprises the first soft purl 9 of soft purl 7, second and block combination 10, in block combination 10, back-moving spring 12 is housed; The first soft purl 7 inserts after the soft purl 9 of time movement finger lock stabilizer 8, the second inserts block combination 10 and pushes back-moving spring 12 open.
Described power spring 2 is by one or a plurality of spring forms.
Described gear assembly 13 is one or more levels gear.
Described block combination 10 can be contained on flat sheet combination or be contained on casing assembly 5.
Described block combination 10 can act on any one-level gear.
Described back-moving spring 12 can be torsion spring or flat spring.
The first described soft purl 7 and the second soft purl 9 are flexible latch or rigidity latch.
The cable wire 3 for locking being equipped with on piston 1, cable wire 3 can be flexible cable or rigid posts.
Plug after the soft purl 9 of the first soft purl 7, second, pull cable wire 3 to lock, after locking, lockaid gun is just in treating duty; After pulling out the first soft purl 7, mechanism assembly disequilibrium, fast rotational under the promotion of power spring 2 is until power spring 2 discharges (the second soft purl 9 keeps insertion state) completely; If pull out the second soft purl 9 in the process of mechanism assembly rotation, mechanism assembly stops operating, and power spring stops discharging.
Specific works principle is: after lockaid gun is locked, time movement is confining force balance between piston 1 and the soft purl 9 of the first soft purl 7, second, remains static; When pulling out the soft purl 9 of the first soft purl 7(second, do not pull out) after, time movement power spring thrust under rotate, after predetermined time, discharge power spring power output and displacement in timing course, when pulling out the second soft purl 9, mechanism stops timing.

Claims (8)

1. a mechanical type reserve parachute lockaid gun, is characterized in that, comprises time movement, actuating unit and locking controlling organization, wherein:
Actuating unit comprises the piston tube [4], the brake(-holder) block [6] that are contained on casing assembly [5], is contained in power spring [2] and piston [1] in piston tube [5], power spring [2] one end withstands on piston tube [4] right side, the other end keeps contacting with piston [1] under nature, pulley [14] for locking is housed in the lower end of piston [1], and pulley [14] stretches out the groove on the face of cylinder under piston tube [4] and also can in groove, slide; Brake(-holder) block [6] is hinged on time movement, when pulley goes to the soffit cunning of brake(-holder) block [6], brake(-holder) block [6] is rotated counterclockwise, and pulley [14] is from the soffit of brake(-holder) block [6] slips over, brake(-holder) block [6] turns clockwise under elastomeric element effect, and pulley [14] is stuck on the end face of brake(-holder) block [6];
Time movement comprises gear assembly [13], regulating wheel [11] and the stabilizer [8] that forms driving-chain, and gear assembly [13], under the promotion of actuating unit, promotes stabilizer [8] by regulating wheel [11] and swings timing;
Locking controlling organization comprises the first soft purl [7], the second soft purl [9] and block combination [10], in block combination [10], back-moving spring [12] is housed; The first soft purl [7] inserts time movement finger lock stabilizer [8], and the second soft purl [9] is pushed back-moving spring [12] open after inserting block combination [10].
2. a kind of mechanical type reserve parachute lockaid gun according to claim 1, is characterized in that: described power spring [2] is by one or a plurality of spring forms.
3. a kind of mechanical type reserve parachute lockaid gun according to claim 1, is characterized in that: described gear assembly [13] is one or more levels gear.
4. a kind of mechanical type reserve parachute lockaid gun according to claim 1, is characterized in that: described block combination [10] can be contained on flat sheet combination or be contained on casing assembly [5].
5. according to claim 1, one of 4 described a kind of mechanical type reserve parachute lockaid guns, it is characterized in that: described block combination [10] can act on any one-level gear.
6. according to claim 1, one of 4 described a kind of mechanical type reserve parachute lockaid guns, it is characterized in that: described back-moving spring [12] can be torsion spring or flat spring.
7. a kind of mechanical type reserve parachute lockaid gun according to claim 1, is characterized in that: described the first soft purl [7] and the second soft purl [9] are flexible latch or rigidity latch.
8. a kind of mechanical type reserve parachute lockaid gun according to claim 1, is characterized in that: on piston [1], be equipped with for the cable wire of locking [3], cable wire [3] can be flexible cable or rigid posts.
CN201310615763.2A 2014-01-13 2014-01-13 Mechanical reserve parachute unlocking device Pending CN103670017A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310615763.2A CN103670017A (en) 2014-01-13 2014-01-13 Mechanical reserve parachute unlocking device

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Application Number Priority Date Filing Date Title
CN201310615763.2A CN103670017A (en) 2014-01-13 2014-01-13 Mechanical reserve parachute unlocking device

Publications (1)

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CN103670017A true CN103670017A (en) 2014-03-26

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104118001A (en) * 2013-04-24 2014-10-29 武汉航空仪表有限责任公司 Mechanical cutting device
CN108033018A (en) * 2017-11-21 2018-05-15 武汉航空仪表有限责任公司 A kind of ejection escape lockaid gun and its time response adjustment method
CN110295790A (en) * 2019-08-06 2019-10-01 赣州禾盈通用零部件有限公司 A kind of Purely mechanical timing means
CN111114794A (en) * 2019-12-13 2020-05-08 武汉航空仪表有限责任公司 Mechanical waterproof unlocking device
CN111114798A (en) * 2019-12-13 2020-05-08 武汉航空仪表有限责任公司 Automatic unlocking device and installation method of steel cable assembly of automatic unlocking device

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3468502A (en) * 1967-05-08 1969-09-23 Halliburton Co Parachute release device
US6257524B1 (en) * 1999-12-23 2001-07-10 Capewell Components Company Limited Partnership Mechanical dereefer
CN202358304U (en) * 2011-10-20 2012-08-01 河海大学 Acceleration induction parachute
CN102765480A (en) * 2012-05-03 2012-11-07 同济大学 Novel automatic active device and height detection method thereof
CN103612764A (en) * 2013-11-27 2014-03-05 武汉航空仪表有限责任公司 Host and backup linked type parachute system

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3468502A (en) * 1967-05-08 1969-09-23 Halliburton Co Parachute release device
US6257524B1 (en) * 1999-12-23 2001-07-10 Capewell Components Company Limited Partnership Mechanical dereefer
CN202358304U (en) * 2011-10-20 2012-08-01 河海大学 Acceleration induction parachute
CN102765480A (en) * 2012-05-03 2012-11-07 同济大学 Novel automatic active device and height detection method thereof
CN103612764A (en) * 2013-11-27 2014-03-05 武汉航空仪表有限责任公司 Host and backup linked type parachute system

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104118001A (en) * 2013-04-24 2014-10-29 武汉航空仪表有限责任公司 Mechanical cutting device
CN104118001B (en) * 2013-04-24 2016-03-23 武汉航空仪表有限责任公司 A kind of mechanical type cutter sweep
CN108033018A (en) * 2017-11-21 2018-05-15 武汉航空仪表有限责任公司 A kind of ejection escape lockaid gun and its time response adjustment method
CN110295790A (en) * 2019-08-06 2019-10-01 赣州禾盈通用零部件有限公司 A kind of Purely mechanical timing means
CN111114794A (en) * 2019-12-13 2020-05-08 武汉航空仪表有限责任公司 Mechanical waterproof unlocking device
CN111114798A (en) * 2019-12-13 2020-05-08 武汉航空仪表有限责任公司 Automatic unlocking device and installation method of steel cable assembly of automatic unlocking device
CN111114794B (en) * 2019-12-13 2021-06-01 武汉航空仪表有限责任公司 Mechanical waterproof unlocking device
CN111114798B (en) * 2019-12-13 2021-09-03 武汉航空仪表有限责任公司 Automatic unlocking device and installation method of steel cable assembly of automatic unlocking device

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Application publication date: 20140326