CN103670017A - Mechanical reserve parachute unlocking device - Google Patents
Mechanical reserve parachute unlocking device Download PDFInfo
- 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
- Authority
- CN
- China
- Prior art keywords
- block
- reserve parachute
- purl
- soft
- brake
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Images
Landscapes
- Braking Arrangements (AREA)
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
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.
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 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201310615763.2A CN103670017A (en) | 2014-01-13 | 2014-01-13 | Mechanical reserve parachute unlocking device |
Publications (1)
Publication Number | Publication Date |
---|---|
CN103670017A true CN103670017A (en) | 2014-03-26 |
Family
ID=50308722
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201310615763.2A Pending CN103670017A (en) | 2014-01-13 | 2014-01-13 | Mechanical reserve parachute unlocking device |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN103670017A (en) |
Cited By (5)
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)
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 |
-
2014
- 2014-01-13 CN CN201310615763.2A patent/CN103670017A/en active Pending
Patent Citations (5)
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)
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 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN103670017A (en) | Mechanical reserve parachute unlocking device | |
CN103612764B (en) | A kind of parachute system of active and standby linkage | |
CN102926610A (en) | Electric vehicle window lifting device with manual opening function | |
CN204507281U (en) | Built-in umbrella storehouse opening structure | |
CN104943865B (en) | Fully mechanical microminiature is jettisoninged robot parachute automatic-separation mechanism | |
CN105688340A (en) | Novel multifunctional descent control device with cyclic lifting function | |
CN202342723U (en) | Rescuing air sac in well | |
CN108331479A (en) | A kind of sliding window emergency opening system | |
CN108394779A (en) | A kind of wisdom building elevator escape device | |
CN102030108B (en) | Aircraft lifesaving device | |
CN203829497U (en) | Novel double-control descent control device | |
CN206016753U (en) | Multifunctional pumping rod preventer | |
CN211885000U (en) | Auto-induction parachute-opening escape device in weightless state | |
CN103961814A (en) | Adjustable downhill device | |
CN107174760A (en) | Two-way speed reduction in landing device | |
CN201510658U (en) | High-rise building fire self-rescue device | |
CN201324450Y (en) | High altitude lifesaving hydraulic descent control device | |
CN102001447B (en) | Airplane lifesaving device | |
CN113932670B (en) | External detonation handle of cabin cover breaking system | |
CN102716555A (en) | Inflatable escape fire safety device | |
CN206888963U (en) | Cable perforation automatic safe relief valve | |
CN205168922U (en) | Unmanned helicopter safety parachuting system | |
CN204386652U (en) | A kind of explosion proof door | |
CN201431711Y (en) | Rescuing device | |
CN202724496U (en) | Inflatable escaping fire safety device |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20140326 |