CN108163210A - Using the pack harness system of active and standby integral structure - Google Patents
Using the pack harness system of active and standby integral structure Download PDFInfo
- Publication number
- CN108163210A CN108163210A CN201711424058.9A CN201711424058A CN108163210A CN 108163210 A CN108163210 A CN 108163210A CN 201711424058 A CN201711424058 A CN 201711424058A CN 108163210 A CN108163210 A CN 108163210A
- Authority
- CN
- China
- Prior art keywords
- pack
- main chute
- harness system
- backup
- shoulder strap
- 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
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D17/00—Parachutes
- B64D17/40—Packs
Abstract
The invention discloses a kind of pack harness system using active and standby integral structure, main chute packet, backup pack are placed in behind, and backup pack is placed in the position that main chute wraps portion.The space of front is released, more weaponrys easy to carry are conducive to parachutist and keep good posture in the air, and the visual field of parachutist is also broader.
Description
Technical field
It drops from the air the invention belongs to personnel the parachute field used, specifically a kind of pack using active and standby integral structure is carried on the back
Band system.
Background technology
Troop parachute is the stabilization deceleration device of parachutist, for the airborne operation and training of parachutist.Main chute is born mainly
Stabilization deceleration, Redundancy Design of the reserve parachute as main chute is in main parachute malfunction, to save parachutist's life, really
Protect the backup life preserver of its safe landing.The universal troop parachute of active service splits mode using active and standby, main chute rearward, reserve parachute
Hang over front.Because reserve parachute is two fixed with front is hung, in parachute jumping, parachutist's posture product can be influenced；Reserve parachute
After packaging, highly in 180mm or so, the visual field of parachutist can be blocked with the reserve parachute for hanging over front.
Invention content
The purpose of the present invention is to provide a kind of pack harness systems of active and standby integral structure.
Realize the object of the invention technical solution be：A kind of pack harness system using active and standby integral structure, it is main
Pack, backup pack are placed in behind, and backup pack is placed in the position that main chute wraps portion.
The main chute packet is sewn on shoulder strap, and there are three the rectangular carbine phases buckled a, wrapped with reserve parachute for shoulder strap back side seam
Even, main chute is wrapped equipped with connection sheet, and connection sheet is isosceles trapezoid, and trapezoidal bottom is sewn to main chute and wraps protective cloth package position
The lower section put is sewed with reinforcing strip among connection sheet, and rectangular button b, the connection ring that rectangular button b is wrapped with reserve parachute are connected in reinforcing strip
It is fixedly connected.
The reserve parachute is wrapped and is sewed with connection ring below protective cloth lock conical ring, and connection ring is fixed with the connection sheet that main chute is wrapped
Connection；Carbine, backup pack to be connect by carbine with the rectangular a that buckles on shoulder strap there are three seams in the middle part of backup pack.
Compared with prior art, the present invention its remarkable advantage：Main chute, reserve parachute are placed in parachutist behind by the present invention,
The space of front is released, more weaponrys easy to carry are conducive to parachutist and keep good posture in the air, parachute jumping
The visual field of member is also broader.
Description of the drawings
Fig. 1 is the harness system of the present invention.
Fig. 2 is the main chute pack of the present invention.
Fig. 3 is the reserve parachute pack of the present invention.
Fig. 4 is the figure after main chute of the present invention, backup parachute pack.
Specific embodiment
Invention is described further with reference to the accompanying drawings of the specification.
The pack harness system of the active and standby integral structure of the present invention is to be placed in main chute, reserve parachute behind, reserve parachute pack
The position that main chute wraps portion is placed in, space is provided with main battle weaponries such as harness packets with operation is hung for front.
The shoulder strap of the present invention is made of 44-1600 bright and beautiful silk ribbons.Harness system is shown in Fig. 1, and main chute pack 1 is sewn to shoulder strap 2
On, 2 back side of shoulder strap seam buckles a3 there are three rectangular, is connected with the carbine 7 on reserve parachute pack.Main chute and reserve parachute are placed in carrying on the back
Afterwards, reserve parachute pack is placed in main chute packet upper position.Because of the limitation of human body behind height, after main chute packaging is packed into parachute sleeve,
Parachute sleeve it is laterally disposed with main chute packet in.
Main chute, reserve parachute are placed in parachutist behind, release the space of front, more weaponrys easy to carry,
Be conducive to parachutist and keep good posture in the air, the visual field of parachutist is also broader.
Main chute structure is shown in Fig. 2.
Main chute pack 1 is sewn in 2 system of shoulder strap, and rectangular button a3 is fixed with the connection ring 6 on reserve parachute in connection sheet connects
It connects.Connection sheet 4 is isosceles trapezoid, and trapezoidal bottom is sewn to the lower section of protective cloth package position on main chute pack 1, connection sheet
Reinforcing strip is sewed among 4, rectangular button b5 is connected in reinforcing strip.
Reserve parachute umbrella structure packet is shown in Fig. 3.
Reserve parachute is wrapped and connection ring 6 is sewed with below protective cloth lock conical ring, and connection ring 6 and the connection sheet 4 on main chute pack are solid
Fixed connection.Carbine 7 there are three seams, reserve parachute pack to pass through the side on these three carbines 7 and shoulder strap in the middle part of reserve parachute pack
The a3 connections of shape button.
See Fig. 4 after main chute, backup parachute pack.
The present invention have passed through the verification of dummy's airdrop test and true man's trial jump, work well.
Claims (4)
1. a kind of pack harness system using active and standby integral structure, it is characterised in that：Main chute packet（1）, backup pack is placed in
Behind, backup pack is placed in main chute packet（1）The position on top.
2. pack harness system according to claim 1, it is characterised in that：The main chute packet（1）It is sewn to shoulder strap（2）
On, shoulder strap（2）There are three rectangular button a for back side seam（3）, the carbine wrapped with reserve parachute（7）It is connected, main chute packet（1）It is equipped with
Connection sheet（4）, connection sheet（4）For isosceles trapezoid, trapezoidal bottom is sewn to main chute packet（1）Under upper protective cloth package position
Side, connection sheet（4）Centre is sewed with reinforcing strip, and rectangular button b is connected in reinforcing strip（5）, rectangular button b（5）The company wrapped with reserve parachute
Connect ring（6）It is fixedly connected.
3. pack harness system according to claim 2, it is characterised in that：The reserve parachute is wrapped under protective cloth lock conical ring
Side is sewed with connection ring（6）, connection ring（6）With main chute packet（1）On connection sheet（4）It is fixedly connected；Three are sewed in the middle part of backup pack
A carbine（7）, backup pack passes through carbine（7）With shoulder strap（2）On rectangular button a（3）Connection.
4. the pack harness system according to Claims 2 or 3, it is characterised in that：The shoulder strap（2）Using 44-1600 brocades
Silk ribbon is made.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711424058.9A CN108163210A (en) | 2017-12-25 | 2017-12-25 | Using the pack harness system of active and standby integral structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711424058.9A CN108163210A (en) | 2017-12-25 | 2017-12-25 | Using the pack harness system of active and standby integral structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108163210A true CN108163210A (en) | 2018-06-15 |
Family
ID=62520585
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711424058.9A Pending CN108163210A (en) | 2017-12-25 | 2017-12-25 | Using the pack harness system of active and standby integral structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108163210A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112607034A (en) * | 2020-12-31 | 2021-04-06 | 宏光空降装备有限公司 | Pressure-dividing back cushion |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0941924A1 (en) * | 1998-03-11 | 1999-09-15 | Irvin Aerospace S.p.A. | Improved system for extraction and unfolding of reserve parachute |
| US7118073B2 (en) * | 2002-12-27 | 2006-10-10 | Booth William R | Skyhook reserve parachute deployment system |
| US20110168846A1 (en) * | 2010-01-08 | 2011-07-14 | Edward Strong | Static line piggyback parachute system |
| 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 |
| CN106143923A (en) * | 2015-03-18 | 2016-11-23 | 李昭容 | A kind of overhead escape device |
-
2017
- 2017-12-25 CN CN201711424058.9A patent/CN108163210A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0941924A1 (en) * | 1998-03-11 | 1999-09-15 | Irvin Aerospace S.p.A. | Improved system for extraction and unfolding of reserve parachute |
| US7118073B2 (en) * | 2002-12-27 | 2006-10-10 | Booth William R | Skyhook reserve parachute deployment system |
| US20110168846A1 (en) * | 2010-01-08 | 2011-07-14 | Edward Strong | Static line piggyback parachute system |
| 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 |
| CN106143923A (en) * | 2015-03-18 | 2016-11-23 | 李昭容 | A kind of overhead escape device |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112607034A (en) * | 2020-12-31 | 2021-04-06 | 宏光空降装备有限公司 | Pressure-dividing back cushion |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180615 |
|
| RJ01 | Rejection of invention patent application after publication |