CN110723300A - Method for reducing parachute opening impact of ram parafoil - Google Patents
Method for reducing parachute opening impact of ram parafoil Download PDFInfo
- Publication number
- CN110723300A CN110723300A CN201911037023.9A CN201911037023A CN110723300A CN 110723300 A CN110723300 A CN 110723300A CN 201911037023 A CN201911037023 A CN 201911037023A CN 110723300 A CN110723300 A CN 110723300A
- Authority
- CN
- China
- Prior art keywords
- rope
- air chamber
- constraint
- ram
- air chambers
- 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
- IBSREHMXUMOFBB-JFUDTMANSA-N 5u8924t11h Chemical compound O1[C@@H](C)[C@H](O)[C@@H](OC)C[C@@H]1O[C@@H]1[C@@H](OC)C[C@H](O[C@@H]2C(=C/C[C@@H]3C[C@@H](C[C@@]4(O3)C=C[C@H](C)[C@@H](C(C)C)O4)OC(=O)[C@@H]3C=C(C)[C@@H](O)[C@H]4OC\C([C@@]34O)=C/C=C/[C@@H]2C)/C)O[C@H]1C.C1=C[C@H](C)[C@@H]([C@@H](C)CC)O[C@]11O[C@H](C\C=C(C)\[C@@H](O[C@@H]2O[C@@H](C)[C@H](O[C@@H]3O[C@@H](C)[C@H](O)[C@@H](OC)C3)[C@@H](OC)C2)[C@@H](C)\C=C\C=C/2[C@]3([C@H](C(=O)O4)C=C(C)[C@@H](O)[C@H]3OC\2)O)C[C@H]4C1 IBSREHMXUMOFBB-JFUDTMANSA-N 0.000 title claims abstract description 38
- 238000000034 method Methods 0.000 title claims abstract description 24
- 230000000149 penetrating effect Effects 0.000 claims abstract description 14
- 230000000452 restraining effect Effects 0.000 claims description 11
- 239000004677 Nylon Substances 0.000 claims description 3
- 229920001778 nylon Polymers 0.000 claims description 3
- 230000003014 reinforcing effect Effects 0.000 claims description 3
- 230000001934 delay Effects 0.000 description 5
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D17/00—Parachutes
- B64D17/62—Deployment
- B64D17/72—Deployment by explosive or inflatable means
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D17/00—Parachutes
- B64D17/62—Deployment
- B64D17/74—Sequential deployment of a plurality of canopies
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
The invention discloses a method for reducing parachute opening impact of a ram parafoil, wherein a plurality of rope penetrating holes are uniformly distributed on front edge notches of a side air chamber and a constraint air chamber, the constraint air chamber and the side air chamber on the same side are overlapped and then use a constraint rope, one end of the constraint rope penetrates through the rope penetrating holes in the side air chamber and all the constraint air chambers on the same side in an S-shaped penetrating sequence, the other end of the constraint rope penetrates through the rope penetrating holes in the side air chamber and all the constraint air chambers on the same side and finally penetrates through the outer sides of the side air chambers and is fixedly connected, the middle section of the constraint rope also penetrates through a cutting hole of a separator; when the ram parafoil is out of the bag, the reserved air chamber is unfolded and a timer on the separator is started at the same time, after the timer reaches a set time, the separator works, the restraint rope is cut off from the middle, the air flow of the reserved air chamber flows to the restraint air chamber and the side air chamber, and the ram parafoil is gradually unfolded until the ram parafoil is fully inflated and starts to work. The method changes the instantaneous one-time large impact overload into multiple-time small impact overload, and is simple to implement.
Description
Technical Field
The invention belongs to the field of air drop, and particularly relates to a method for reducing parachute opening impact of a ram parafoil.
Background
The ram parafoil is a parafoil which is inflated by ram air to fully form wings, and can be instantaneously unfolded in the whole area under the condition of a certain parachute opening speed, the parachute opening impact is higher than that of a conventional parachute by more than 50%, and the strength of a micro-breathable material used by the upper and lower wing surfaces of a common ram parafoil is difficult to bear the parachute opening impact force, so that canopy damage is easily caused, the parafoil fails, meanwhile, equipment carried by the ram parafoil is not allowed to overload too much parachute opening, and the equipment is easily damaged.
Disclosure of Invention
The invention aims to provide a method for reducing parachute opening impact of a ram parafoil, which delays the time of inflating and fully opening a ram parafoil air chamber, changes instant larger impact overload into multiple small impact overload, improves the reliability of parachute opening procedures, does not need to carry out deep improvement on the ram parafoil, and has simple implementation and strong universality.
The technical scheme adopted by the invention is as follows:
a method for reducing parachute opening impact of a stamping parafoil comprises the steps that a plurality of air chambers in the middle are reserved air chambers, a plurality of air chambers between a side air chamber and the reserved air chambers are constraint air chambers, the constraint air chambers on two sides are symmetrical, a plurality of rope penetrating holes are uniformly distributed in front edge notches of the side air chamber and the constraint air chambers, the constraint air chambers on the same side and the side air chambers are overlapped, then a constraint rope is used, one end of the constraint rope is fixedly connected with the outer side of the side air chamber, the other end of the constraint rope penetrates through the rope penetrating holes in the side air chambers and all the constraint air chambers on the same side in an S-shaped penetrating sequence and finally penetrates through the outer sides of the side air chambers and is fixedly connected, the middle section of the constraint; when the ram parafoil is out of the bag, the reserved air chamber is unfolded and a timer on the separator is started at the same time, after the timer reaches a set time, the separator works, the restraint rope is cut off from the middle, the air flow of the reserved air chamber flows to the restraint air chamber and the side air chamber, and the ram parafoil is gradually unfolded until the ram parafoil is fully inflated and starts to work.
Furthermore, a timer on the separator is matched with the pulling pin, the pulling pin is connected with a pulling pin rope, and when the ram parafoil is taken out of the bag, the pulling pin rope pulls out the pulling pin to start the timer.
Furthermore, a plurality of fixing tabs are sewn near the rope penetrating holes on the outer side of the side air chamber, two ends of the restraint rope are tied on the corresponding fixing tabs, and the separator is hung on the corresponding fixing tabs.
Further, the ends of the restraining cord are tied to the securing tabs using a plain knot.
Further, the stringing hole is sewed on the reinforcing lining belt at the front edge cut.
Furthermore, the restraining rope is a smooth nylon wire rope.
The invention has the beneficial effects that:
the method changes the instantaneous and complete unfolding and inflation of all air chambers of the ram parafoil into the time-interval inflation of the air chambers, delays the time for the inflation and the full inflation of the air chambers of the ram parafoil, changes the instantaneous one-time larger impact overload into multiple-time small impact overload, reduces the instantaneous impact of parachute opening, reduces the strength design requirement of a canopy, and improves the reliability of a parachute opening procedure; the method only needs to additionally arrange the rope threading hole, the restraint rope and the separator, does not need to carry out depth improvement on the ram parafoil, and is simpler to implement; the method can adopt separators with different time delays according to the need of opening the umbrella, and has strong universality.
Drawings
Fig. 1 is a schematic view showing an initial state of a ram parafoil in the embodiment of the present invention.
FIG. 2 is a schematic view showing the connection of the constraining air cells, the side air cells, the constraining ropes and the separators in the initial state in the embodiment of the present invention.
In the figure: 1-a confinement gas chamber; 2-reserving an air chamber; 3-side air chamber; 4-a fastening tab; 5-a restraint rope; 6-a separator; 7-stringing holes.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings and examples.
As shown in figures 1 and 2, a method for reducing parachute opening impact of a ram parafoil, which takes a plurality of air chambers in the middle as reserved air chambers 2 (in the embodiment, five reserved air chambers 2 are arranged and can be adjusted according to actual requirements), a plurality of air chambers between a side air chamber 3 and the reserved air chambers 2 as constraint air chambers 1, and the constraint air chambers 1 on two sides are symmetrical, a plurality of rope penetrating holes 7 are uniformly distributed on front edge notches of the side air chamber 3 and the side air chamber 1, the restraining rope 5 is used after the restraining air chamber 1 and the side air chamber 3 on the same side are overlapped, one end of the restraining rope 5 is fixedly connected with the outer side of the side air chamber 3, the other end of the restraining rope passes through the rope penetrating holes 7 on the side air chamber 3 and all the restraining air chambers 1 on the same side in an S-shaped passing sequence and finally penetrates out of the outer side of the side air chamber 3 and is fixedly connected, the middle section of the restraining rope 5 also passes through a cutting hole of the separator 6, and the separator 6 is fixedly connected with the outer; when the ram parafoil is out of the bag, the timer on the separator 6 is started while the reserved air chamber 2 is unfolded, after the timer is timed to a set time, the separator 6 works, the restraint rope 5 is cut off from the middle, the airflow of the reserved air chamber 2 flows to the restraint air chamber 1 and the side air chamber 3, and the ram parafoil is gradually unfolded until the ram parafoil is fully inflated and starts to work.
The method changes the instantaneous and complete unfolding and inflation of all air chambers of the ram parafoil into the time-interval inflation of the air chambers, delays the time for the inflation and the full inflation of the air chambers of the ram parafoil, changes the instantaneous one-time larger impact overload into multiple-time small impact overload, reduces the instantaneous impact of parachute opening, reduces the strength design requirement of a canopy, and improves the reliability of a parachute opening procedure; the method only needs to additionally arrange the rope threading hole 7, the restraint rope 5 and the separator 6, does not need to carry out depth improvement on the ram parafoil, and is simpler to implement; the method can adopt separators 6 with different time delays according to the need of opening the umbrella, and has strong universality.
As shown in fig. 2, in the present embodiment, a plurality of fixing tabs 4 are sewn near the rope threading holes 7 outside the side air chambers 3, two ends of the constraining rope 5 are tied (or tied with flat knots) on the respective corresponding fixing tabs 4, and the separator 6 is hung on the corresponding fixing tabs 4. The restraint rope 5 and the separator 6 are fixedly connected with the outer side of the side air chamber 3 through the fixing loop 4, and the use of the side air chamber 3 is not influenced.
In this embodiment, the timer on the separator 6 is matched with the pulling pin, the pulling pin is connected with the pulling pin rope, and when the ram parafoil is taken out of the bag, the pulling pin rope pulls out the pulling pin to start the timer.
In this embodiment, the lacing holes 7 are sewn to the reinforcing backing strip at the front edge cut.
In the embodiment, the restraining rope 5 is made of smooth nylon ropes, so that the side air chamber 3 and the restraining air chamber 1 are not scratched.
It will be understood that modifications and variations can be made by persons skilled in the art in light of the above teachings and all such modifications and variations are intended to be included within the scope of the invention as defined in the appended claims.
Claims (6)
1. A method for reducing the parachute opening impact of a ram parafoil is characterized in that: the method comprises the following steps of taking a plurality of air chambers in the middle as reserved air chambers, taking a plurality of air chambers between a side air chamber and the reserved air chambers as constraint air chambers, wherein the constraint air chambers on two sides are symmetrical, uniformly distributing a plurality of rope penetrating holes on front edge notches of the side air chamber and the constraint air chambers, overlapping the constraint air chambers on the same side and the side air chambers, using a constraint rope, enabling one end of the constraint rope to be fixedly connected with the outer side of the side air chamber, enabling the other end of the constraint rope to penetrate through the rope penetrating holes in the side air chambers and all the constraint air chambers on the same side in an S-shaped penetrating sequence and finally penetrate through the outer sides of the side air chambers and are fixedly connected; when the ram parafoil is out of the bag, the reserved air chamber is unfolded and a timer on the separator is started at the same time, after the timer reaches a set time, the separator works, the restraint rope is cut off from the middle, the air flow of the reserved air chamber flows to the restraint air chamber and the side air chamber, and the ram parafoil is gradually unfolded until the ram parafoil is fully inflated and starts to work.
2. A method of reducing the parachute opening impact of a ram-winged umbrella as set forth in claim 1, wherein: the timer on the separator is matched with the pulling pin, the pulling pin is connected with a pulling pin rope, and when the ram parafoil is taken out of the bag, the pulling pin is pulled out by the pulling pin rope, and the timer is started.
3. A method of reducing the parachute opening impact of a ram-winged umbrella as set forth in claim 1, wherein: a plurality of fixing tabs are sewn near the rope penetrating holes on the outer side of the side air chamber, two ends of the restraint rope are tied on the corresponding fixing tabs, and the separators are hung on the corresponding fixing tabs.
4. A method of reducing the parachute opening impact of a ram parafoil as recited in claim 3, further comprising: the end of the restraining rope is tied to the fixing loop by using a flat knot.
5. A method of reducing the parachute opening impact of a ram-winged umbrella as set forth in claim 1, wherein: the rope-threading hole is sewed on the reinforcing lining belt at the front edge cut.
6. A method of reducing the parachute opening impact of a ram-winged umbrella as set forth in claim 1, wherein: the restraint rope is a smooth nylon wire rope.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911037023.9A CN110723300A (en) | 2019-10-29 | 2019-10-29 | Method for reducing parachute opening impact of ram parafoil |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911037023.9A CN110723300A (en) | 2019-10-29 | 2019-10-29 | Method for reducing parachute opening impact of ram parafoil |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110723300A true CN110723300A (en) | 2020-01-24 |
Family
ID=69222460
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201911037023.9A Pending CN110723300A (en) | 2019-10-29 | 2019-10-29 | Method for reducing parachute opening impact of ram parafoil |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110723300A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114162333A (en) * | 2021-12-23 | 2022-03-11 | 航宇救生装备有限公司 | Method for controlling parachute opening performance of ram parafoil by using rib |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20100032527A1 (en) * | 2008-08-07 | 2010-02-11 | Fox Jr Roy L | Parachute inlet control system and method |
| US20150053822A1 (en) * | 2013-08-21 | 2015-02-26 | We Designs, Llc | System and method for reserve parachute deployment |
| CN106114855A (en) * | 2016-08-29 | 2016-11-16 | 航宇救生装备有限公司 | A kind of ram air parachute parachute-opening controls device |
| CN107813941A (en) * | 2017-10-27 | 2018-03-20 | 航宇救生装备有限公司 | Reduce Parachute Opening impact and the method for reducing parachute level simultaneously |
| CN109250123A (en) * | 2018-10-19 | 2019-01-22 | 航宇救生装备有限公司 | A kind of split inflation ram air parachute |
| CN109335000A (en) * | 2018-11-16 | 2019-02-15 | 航宇救生装备有限公司 | A kind of restriction rope control open umbrella type ram air parachute |
-
2019
- 2019-10-29 CN CN201911037023.9A patent/CN110723300A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20100032527A1 (en) * | 2008-08-07 | 2010-02-11 | Fox Jr Roy L | Parachute inlet control system and method |
| US20150053822A1 (en) * | 2013-08-21 | 2015-02-26 | We Designs, Llc | System and method for reserve parachute deployment |
| CN106114855A (en) * | 2016-08-29 | 2016-11-16 | 航宇救生装备有限公司 | A kind of ram air parachute parachute-opening controls device |
| CN107813941A (en) * | 2017-10-27 | 2018-03-20 | 航宇救生装备有限公司 | Reduce Parachute Opening impact and the method for reducing parachute level simultaneously |
| CN109250123A (en) * | 2018-10-19 | 2019-01-22 | 航宇救生装备有限公司 | A kind of split inflation ram air parachute |
| CN109335000A (en) * | 2018-11-16 | 2019-02-15 | 航宇救生装备有限公司 | A kind of restriction rope control open umbrella type ram air parachute |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114162333A (en) * | 2021-12-23 | 2022-03-11 | 航宇救生装备有限公司 | Method for controlling parachute opening performance of ram parafoil by using rib |
| CN114162333B (en) * | 2021-12-23 | 2023-07-21 | 航宇救生装备有限公司 | Method for controlling opening performance of stamped parafoil by utilizing wing ribs |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206107574U (en) | But gas filled cluster is expanded fast in low latitude | |
| US8096509B2 (en) | Parachute inlet control system and method | |
| US10407175B2 (en) | Parachute deployment system using decoupled tow and release lines | |
| CN109335000B (en) | Restraint rope controlled umbrella-opening type stamping parafoil | |
| US5893536A (en) | Parafoil assembly | |
| US5205517A (en) | Large parachute with means to positively expand and circularize the inlet area to facilitate deployment thereof | |
| CN110723300A (en) | Method for reducing parachute opening impact of ram parafoil | |
| CN107618669B (en) | A kind of parachute with apical pore lid | |
| JP5022113B2 (en) | Parachute leafing device | |
| US7584927B2 (en) | Pre-chute deployment skydiver deceleration device | |
| CN107600433B (en) | Parachute canopy protective sleeve by means of back-pull method and mounting method thereof | |
| EP1752378B1 (en) | Multi-grommet retained slider for parachutes | |
| CN107826256B (en) | Method for reducing parachute opening impact of ram parafoil | |
| CN107757923A (en) | Ram air parachute parachute-opening control method | |
| US4955563A (en) | Apparatus and method for controlled simultaneous opening of clustered parachutes | |
| CN109250122A (en) | A kind of traction parachute-opening inflatable ram air parachute | |
| US4678145A (en) | Removable slider for parachute deployment | |
| US3525491A (en) | Parachute | |
| CN109250123B (en) | Slit type inflatable ram parafoil | |
| CN213008770U (en) | Air blowing pocket type secondary unfolding parachute | |
| CN110723296A (en) | Method for improving parachute opening reliability of large-scale stamping parafoil | |
| CN110723297A (en) | Control method for assisting parachute opening of ram parafoil | |
| CN106114855A (en) | A kind of ram air parachute parachute-opening controls device | |
| CN205998125U (en) | A kind of ram air parachute parachute-opening control device | |
| US2583905A (en) | Parachute pack and container |
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 | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20200124 |