CN107813941A - Reduce Parachute Opening impact and the method for reducing parachute level simultaneously - Google Patents
Reduce Parachute Opening impact and the method for reducing parachute level simultaneously Download PDFInfo
- Publication number
- CN107813941A CN107813941A CN201711026537.5A CN201711026537A CN107813941A CN 107813941 A CN107813941 A CN 107813941A CN 201711026537 A CN201711026537 A CN 201711026537A CN 107813941 A CN107813941 A CN 107813941A
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- Prior art keywords
- parachute
- restraining
- canopy
- level
- reducing
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- 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.)
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Links
- 238000000034 method Methods 0.000 title claims abstract description 11
- 230000000452 restraining effect Effects 0.000 claims abstract description 34
- 239000000463 material Substances 0.000 claims description 4
- 238000010586 diagram Methods 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- TVEXGJYMHHTVKP-UHFFFAOYSA-N 6-oxabicyclo[3.2.1]oct-3-en-7-one Chemical compound C1C2C(=O)OC1C=CC2 TVEXGJYMHHTVKP-UHFFFAOYSA-N 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000004806 packaging method and process Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
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
- B64D17/02—Canopy arrangement or construction
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
The present invention relates to method that is a kind of while reducing Parachute Opening impact and reduce parachute level, connection sets several restrainings at the different height of bell, restraining prevents parachute from being fully deployed in one week around parachute, the separator for restraining to be cut off is equipped with restraining, parachute is after pack pull-out, canopy bottom, which inflates to be filled at once, completes the expansion of first order canopy, when a certain speed is surely down to, the separated device cut-out of the restraining of bottom, complete the expansion of second level canopy, restraining is cut off successively from the bottom up afterwards, canopy is set to deploy step by step from the bottom up until parachute is filled completely.The present invention makes parachute change into the expansion in order of increase step by step by all expansion when opening, simple to operate, reliability is high, meets system off-load, the requirement slowed down.
Description
Technical field
The invention belongs to the field of dropping, and in particular to a kind of to reduce Parachute Opening impact simultaneously and reduce parachute level
Method.
Background technology
Parachute be it is a kind of by made of flexible fabric, small volume after soft texture, packaging, be full of after than folding when resistance
Face big tens accompanies even hundreds of aerial delivery provisions accompanied, the object dropped to reduce decrease speed in the presence of parachute, real
Safe falling is showed.
When parachute aerial delivery system is dropped, initial velocity is typically higher, if directly deploying large-scale parachute, due to
Large-scale deployment area is big, and after moment inflation, parachute aerial delivery system can rapidly slow down, equipment, goods and materials and parachute it
Between can produce larger relative motion, bring huge impact, cause to overload.
If the initial velocity of air-drop is higher, in order to reduce Parachute Opening impact, meet off-load, the requirement slowed down, mesh
Preceding to be slowed down step by step, departed from using multistage parachute, final final stage parachute lands.This multi-layer parachute, program are lengthy and tedious multiple
Miscellaneous, reliability is low, and cost is high.
The content of the invention
It is an object of the invention to provide method that is a kind of while reducing Parachute Opening impact and reduce parachute level, make
Parachute changes into the expansion in order of increase step by step when opening by all expansion, reduces the parachute-opening that instantaneous large area expansion is brought
Impact acceleration, it can play and slow down and the requirement steadily landed, it is simple to operate, reliability is high, meet system off-load, slow down
It is required that.
The technical solution adopted in the present invention is：
Method that is a kind of while reducing Parachute Opening impact and reduce parachute level is high in the difference of bell
Connection sets several restrainings at degree, and restraining prevents parachute from being fully deployed in one week around parachute, on restraining
Provided with the separator for restraining to be cut off, for parachute after pack pull-out, canopy bottom inflates the completion that is filled at once
First order canopy deploys, and when a certain speed is surely down to, the separated device cut-out of restraining of bottom, completes second level canopy
Expansion, restraining is cut off successively from the bottom up afterwards, canopy is deployed step by step from the bottom up until parachute is filled completely.
Further, restraining passes through the retainer ring on canopy.
Further, restraining adjustable in length.
Further, it is bound and each selects mutually to fit according to parachute-opening intensity and performance requirement with the canopy not at the same level separated
The material answered.
The beneficial effects of the invention are as follows：
1. the present invention makes parachute change into the expansion in order of increase step by step by all expansion when opening, reduce instantaneous big
The opening shock load that area expansion is brought, because effective developed area increases step by step, therefore deceleration can be played and steadily fallen
The requirement on ground, it is simple to operate, reliability is high compared with multistage parachute, meet system off-load, the requirement slowed down.
2. restraining is limited by retainer ring, will not come off halfway.
3. only needing regulation constraint strip length to adjust developed area, implement simply, versatile, cost is low.
Brief description of the drawings
Fig. 1 is schematic diagram when canopy is the partially unfolded in the embodiment of the present invention.
Fig. 2 is schematic diagram when canopy is fully deployed in the embodiment of the present invention.
In figure：1- first order canopies；2- second level canopy；3- third level canopies；4- fourth stage canopies；5- restrainings；6-
Separator；7- parachutes.
Specific embodiment
Invention is further described with reference to the accompanying drawings and examples.
Method that is a kind of while reducing Parachute Opening impact and reduce parachute level, as shown in figure 1, in parachute 7
Connection sets several restrainings 5 at the different height of canopy, and restraining 5 prevents parachute 7 for 7 one weeks from complete around parachute
Deploy, the separator 6 for restraining 5 to be cut off is equipped with restraining 5, for parachute 7 after pack pull-out, canopy is most lower
Side inflates the completion first order canopy 1 that is filled and deployed at once, and when a certain speed is surely down to, the restraining 5 of bottom, which is separated, to be filled
6 cut-outs are put, second level canopy 2 is completed and deploys, restraining 5 is cut off successively from the bottom up afterwards, canopy is opened up step by step from the bottom up
Open until parachute 7 is filled (as shown in Figure 2) completely.
In the present embodiment, restraining 5 passes through the retainer ring on canopy.Restraining 5 is limited by retainer ring, will not take off halfway
Fall.
In the present embodiment, the adjustable in length of restraining 5.Only need to adjust the i.e. adjustable developed area of the length of restraining 5,
Implement simply, versatile, cost is low.
The canopy not at the same level for being bound the separation of band 5 each selects adaptable material according to parachute-opening intensity and performance requirement
(mainly Air permenbility and intensity index).
The present invention makes parachute 7 change into the expansion in order of increase step by step by all expansion when opening, and reduces instantaneous big
The opening shock load that area expansion is brought, because effective developed area increases step by step, therefore deceleration can be played and steadily fallen
The requirement on ground, it is simple to operate, reliability is high compared with multistage parachute, meet system off-load, the requirement slowed down.
It should be appreciated that for those of ordinary skills, can according to the above description be improved or converted,
And all these modifications and variations should all belong to the protection domain of appended claims of the present invention.
Claims (4)
1. method that is a kind of while reducing Parachute Opening impact and reduce parachute level, it is characterised in that：In parachute
Connection sets several restrainings at the different height of clothing, and restraining prevents parachute from being fully deployed in one week around parachute,
The separator for restraining to be cut off is equipped with restraining, parachute after pack pull-out, fill at once by canopy bottom
Gas, which is filled, completes the expansion of first order canopy, when a certain speed is surely down to, the separated device cut-out of restraining of bottom, completes
Second level canopy expansion, restraining is cut off successively from the bottom up afterwards, canopy is deployed step by step from the bottom up until parachute is complete
It is filled entirely.
2. the method as claimed in claim 1 for reducing Parachute Opening impact simultaneously and reducing parachute level, its feature exist
In：Restraining passes through the retainer ring on canopy.
3. the method as claimed in claim 1 for reducing Parachute Opening impact simultaneously and reducing parachute level, its feature exist
In：Restraining adjustable in length.
4. the method as claimed in claim 1 for reducing Parachute Opening impact simultaneously and reducing parachute level, its feature exist
In：It is bound and adaptable material is each selected according to parachute-opening intensity and performance requirement with the canopy not at the same level separated.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711026537.5A CN107813941A (en) | 2017-10-27 | 2017-10-27 | Reduce Parachute Opening impact and the method for reducing parachute level simultaneously |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711026537.5A CN107813941A (en) | 2017-10-27 | 2017-10-27 | Reduce Parachute Opening impact and the method for reducing parachute level simultaneously |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107813941A true CN107813941A (en) | 2018-03-20 |
Family
ID=61603269
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711026537.5A Pending CN107813941A (en) | 2017-10-27 | 2017-10-27 | Reduce Parachute Opening impact and the method for reducing parachute level simultaneously |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107813941A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109466776A (en) * | 2018-10-31 | 2019-03-15 | 航宇救生装备有限公司 | A kind of control large area group's umbrella opening structure |
| CN110723300A (en) * | 2019-10-29 | 2020-01-24 | 航宇救生装备有限公司 | Method for reducing parachute opening impact of ram parafoil |
| CN110723298A (en) * | 2019-10-29 | 2020-01-24 | 航宇救生装备有限公司 | Aircraft landing drag parachute main parachute with multi-stage parachute opening |
| CN110723301A (en) * | 2019-10-29 | 2020-01-24 | 航宇救生装备有限公司 | Method for accelerating inflation of parachute at low altitude and low speed |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3615156A (en) * | 1969-06-06 | 1971-10-26 | Space Ordnance Systems Inc | Reefing line cutter |
| US3908938A (en) * | 1972-04-21 | 1975-09-30 | Etudes Et Fab Aeronautiques | Parachute |
| GB2102357A (en) * | 1981-07-28 | 1983-02-02 | Secr Defence | Parachutes-reducing shock loading |
| US4513931A (en) * | 1980-12-02 | 1985-04-30 | Aero-Safe Technologies Inc. | Dereefing cutter |
| CN105329446A (en) * | 2015-11-24 | 2016-02-17 | 湖北青铜汇航空科技有限公司 | Paratrooper training parachute |
| CN205998125U (en) * | 2016-08-29 | 2017-03-08 | 航宇救生装备有限公司 | A kind of ram air parachute parachute-opening control device |
-
2017
- 2017-10-27 CN CN201711026537.5A patent/CN107813941A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3615156A (en) * | 1969-06-06 | 1971-10-26 | Space Ordnance Systems Inc | Reefing line cutter |
| US3908938A (en) * | 1972-04-21 | 1975-09-30 | Etudes Et Fab Aeronautiques | Parachute |
| US4513931A (en) * | 1980-12-02 | 1985-04-30 | Aero-Safe Technologies Inc. | Dereefing cutter |
| GB2102357A (en) * | 1981-07-28 | 1983-02-02 | Secr Defence | Parachutes-reducing shock loading |
| CN105329446A (en) * | 2015-11-24 | 2016-02-17 | 湖北青铜汇航空科技有限公司 | Paratrooper training parachute |
| CN205998125U (en) * | 2016-08-29 | 2017-03-08 | 航宇救生装备有限公司 | A kind of ram air parachute parachute-opening control device |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109466776A (en) * | 2018-10-31 | 2019-03-15 | 航宇救生装备有限公司 | A kind of control large area group's umbrella opening structure |
| CN109466776B (en) * | 2018-10-31 | 2022-03-25 | 航宇救生装备有限公司 | Control large tracts of land crowd umbrella structure of opening |
| CN110723300A (en) * | 2019-10-29 | 2020-01-24 | 航宇救生装备有限公司 | Method for reducing parachute opening impact of ram parafoil |
| CN110723298A (en) * | 2019-10-29 | 2020-01-24 | 航宇救生装备有限公司 | Aircraft landing drag parachute main parachute with multi-stage parachute opening |
| CN110723301A (en) * | 2019-10-29 | 2020-01-24 | 航宇救生装备有限公司 | Method for accelerating inflation of parachute at low altitude and low speed |
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| PB01 | Publication | ||
| PB01 | Publication | ||
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| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180320 |
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| RJ01 | Rejection of invention patent application after publication |