CN106672242A - Personnel obstructing and releasing device for parachuting - Google Patents
Personnel obstructing and releasing device for parachuting Download PDFInfo
- Publication number
- CN106672242A CN106672242A CN201610748102.0A CN201610748102A CN106672242A CN 106672242 A CN106672242 A CN 106672242A CN 201610748102 A CN201610748102 A CN 201610748102A CN 106672242 A CN106672242 A CN 106672242A
- Authority
- CN
- China
- Prior art keywords
- plate
- personnel
- connecting rod
- mounting seat
- base
- 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.)
- Granted
Links
- 230000009191 jumping Effects 0.000 claims description 14
- 241000446313 Lamella Species 0.000 claims description 9
- 229910000831 Steel Inorganic materials 0.000 abstract description 4
- 239000010959 steel Substances 0.000 abstract description 4
- 230000001681 protective effect Effects 0.000 abstract description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 231100001261 hazardous Toxicity 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
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tents Or Canopies (AREA)
- Closing And Opening Devices For Wings, And Checks For Wings (AREA)
Abstract
The invention relates to the technical field of airborne landing with parachutes, especially relates to a personnel obstructing and releasing device for parachuting. The personnel obstructing and releasing device comprises a baffle plate, a connecting rod, a bracing rod, a base, an adjusting steel cable, a mounting seat, a first mounting plate, a second mounting plate and a positioning plate, wherein one end of the connecting rod is connected with the baffle plate, and the other end of the connecting rod is connected with the base; one end of the bracing rod is connected with the second mounting plate, and the other end of the bracing rod is arranged corresponding to the connecting rod; one end of the adjusting steel cable is connected with the baffle plate, and the other end of the adjusting steel cable is connected with the mounting seat; and the first mounting plate and the positioning plate are connected with the base; and the mounting seat, the first mounting plate, the second mounting plate and the positioning plate are fixed on the side wall of the airplane by screws respectively. According to the personnel obstructing and releasing device, a baffle mechanism (the baffle) is transversely arranged at the hatch door for obstructing. The personnel obstructing and releasing device can bear certain impact force, and has a certain protective capability, and can effectively guarantee the personal safety of personnel.
Description
Technical field
The present invention relates to the airborne technical field of parachute, refers in particular to a kind of parachute jumping and separates clearance device with personnel.
Background technology
At present foreign countries' large transport airplane has personnel's break-make device to hold when parachuting for personnel in the airborne activity fashionable dress of enforcement personnel
Row cut-off or instruction of letting pass.Personnel's on-off system and like product are configured without on existing aircraft, pilot is straight before parachute jumping
Go to the station to meet somebody in parachute jumping mouth, without any stop, than relatively hazardous, be prone to accidents.
The content of the invention
For problem above, the invention provides a kind of parachute jumping separates clearance device with personnel, using a kind of baffle mechanism
It is horizontal to be used to separate at hatch door, and certain impact power can be born, possess certain protective capacities, effective guarantee personnel person peace
Entirely.
To achieve these goals, the technical solution used in the present invention is as follows：
One kind parachute jumping with personnel separate clearance device, including baffle plate, connecting rod, strut, base, adjust cable wire, mounting seat,
First installing plate, the second installing plate and location-plate, connecting rod one end is connected to baffle plate, and the other end is connected to base, strut one end
The second installing plate is connected to, the other end is correspondingly arranged with connecting rod, adjusts cable wire one end and be connected to baffle plate, the other end is connected to peace
Dress seat, the first installing plate is connected to base, mounting seat, the first installing plate, the second installing plate and location-plate point with location-plate
It is not fixed on aircraft side walls by screw.
Furthermore, described connecting rod one end is bolted to baffle plate, and the dead bolt and step for passing through connecting rod
Carry out spacing, the connecting rod other end is bolted to base.
Furthermore, described regulation cable wire one end is bolted to baffle plate, and the other end is connected by spacing bulb
In mounting seat, mounting seat is provided with anticreep locking plate, and anticreep locking plate is provided with rotatable lamella and slotted eye, and rotatable lamella is articulated with by rivet
On anticreep locking plate, anticreep locking plate is correspondingly arranged with spacing bulb.
Furthermore, the base is provided with plug, and the first installing plate is connected on plug with location-plate.
The present invention has the beneficial effect that：
The present invention adopts such structure setting, its simple structure, security performance preferably, not to affect the normal of personnel of dropping from the air
Disembark, only take up space in the cabin of very little, to crew's work influence very little, the overall structure and operation to aircraft is without shadow
Ring.
Description of the drawings
Fig. 1 is overall structure figure of the present invention；
Fig. 2 is understructure figure of the present invention；
Fig. 3 is baffle plate and connecting rod connection figure；
Fig. 4 is anticreep lock plate structure figure.
1. baffle plate；2. connecting rod；3. strut；4. base；5. cable wire is adjusted；6. mounting seat；7. the first installing plate；8. second
Installing plate；9. location-plate；10. dead bolt；20. steps；60. anticreep locking plates；61. rotatable lamellas；62. slotted eyes；63. rivets.
Specific embodiment
Below in conjunction with the accompanying drawings technical scheme is illustrated with embodiment.
As shown in Figures 1 to 4, present invention parachute jumping includes baffle plate 1, connecting rod 2, strut 3, bottom with personnel's cut-off clearance device
Seat 4, regulation cable wire 5, mounting seat 6, the first installing plate 7, the second installing plate 8 and location-plate 9.
The one end of connecting rod 2 is bolted to baffle plate 1, and carried out by the dead bolt 10 of connecting rod 2 and step 20 it is spacing,
The other end of connecting rod 2 is bolted to base 4；The one end of strut 3 is connected to the second installing plate 8, the other end and connecting rod 2 pairs
Should arrange；Adjust the one end of cable wire 5 and be bolted to baffle plate 1, the other end is connected to mounting seat 6 by spacing bulb, install
Seat 6 is provided with anticreep locking plate 60, and anticreep locking plate 60 is provided with rotatable lamella 61 and slotted eye 62, and rotatable lamella 61 is articulated with by rivet 63
On anticreep locking plate 60, anticreep locking plate 60 is correspondingly arranged with spacing bulb；Base 4 is provided with plug, the first installing plate 7 and location-plate
9 are connected on plug；Mounting seat 6, the first installing plate 7, the second installing plate 8 are fixed on respectively with location-plate 9 by screw
On aircraft side walls.
The present invention adopts purely mechanical structure, wherein baffle plate 1, connecting rod 2, regulation cable wire 5 and base 4 to connect by bolt
Connect, and can be rotated along respective bolt, dead bolt 10 and step 20 are respectively provided with connecting rod 2, line position can be entered to baffle plate 1
Locking is put, cable wire 5 is adjusted and is provided with 2 anti-spacing bulbs, mounting seat 6 is provided with can be to the anticreep locking plate of the regulation anticreep of cable wire 5
60, anticreep locking plate 60 is provided with can prevent steel to the slotted eye 62 of the regulation upper limit bulb of cable wire 5 and rotatable lamella 61, rotatable lamella 61
Rope is deviate from from mounting seat, in addition, the first installing plate 7 and the second installing plate 8 can carry out position locking to base 4 and strut 3.
Operation principle of the present invention：
In flight course, when airborne instruction is performed put umbrella person and be manually operated and turn on baffle plate 1 along hatch door column
Appropriate angle, parachute jumping passage is formed for parachute jumping personnel clearance in aircraft door mouth；After previous parachutist disembarks or assign
After cancelling airborne instruction, baffle plate 1 is horizontally placed at hatch door, is rapidly converted into cut-off state, the personnel that make subsequently to parachute stop disembarking,
Parachute jumping front and rear baffle 1 in putting between umbrella person and hatch door, to putting umbrella person certain protection is formed all the time.
Workflow of the present invention is as follows：
Baffle plate 1, connecting rod 2, base 4, regulation cable wire 5 are connected into locking with the first installing plate 7, the limit of cable wire 5 will be adjusted
Position bulb is limited on the anticreep locking plate 60 of mounting seat 6, is placed in the slotted eye 62 of anticreep locking plate 60, and now, baffle plate 1 is horizontal
State, manually horizontally rotating baffle plate 1 can realize blocking cut-off or release status at hatch door；By the vertical company of turning to of baffle plate 1
At the limited step 20 of extension bar 2, baffle plate 1 is carried out using the dead bolt 10 of connecting rod 2 spacing, strut 3 is connected with the second installing plate 8
Locking is connect, baffle plate 1 is horizontally rotated, the free end bulb of strut 3 is connected with the groove in connecting rod 2, formed triangle and fix spacing.
Embodiments of the invention are described above in conjunction with accompanying drawing, but be the invention is not limited in above-mentioned concrete
Embodiment, above-mentioned specific embodiment is only schematic, rather than restricted, one of ordinary skill in the art
Under the enlightenment of the present invention, in the case of without departing from present inventive concept and scope of the claimed protection, can also make a lot
Form, these are belonged within the protection of the present invention.
Claims (4)
1. a kind of parachute jumping separates clearance device with personnel, it is characterised in that including baffle plate (1), connecting rod (2), strut (3), bottom
Seat (4), regulation cable wire (5), mounting seat (6), the first installing plate (7), the second installing plate (8) and location-plate (9), the connecting rod
(2) one end is connected to baffle plate (1), and the other end is connected to base (4), and described strut (3) one end is connected to the second installing plate (8),
The other end is correspondingly arranged with connecting rod (2), and described regulation cable wire (5) one end is connected to baffle plate (1), and the other end is connected to mounting seat
(6), first installing plate (7) is connected to base (4), the mounting seat (6), the first installing plate with location-plate (9)
(7), the second installing plate (8) is fixed on aircraft side walls respectively with location-plate (9) by screw.
2. parachute jumping according to claim 1 separates clearance device with personnel, it is characterised in that described connecting rod (2) one end
Baffle plate (1) is bolted to, and spacing, the connecting rod is carried out by the dead bolt (10) of connecting rod (2) and step (20)
(2) other end is bolted to base (4).
3. parachute jumping according to claim 1 separates clearance device with personnel, it is characterised in that the regulation cable wire (5)
End is bolted to baffle plate (1), and the other end is connected to mounting seat (6) by spacing bulb, and the mounting seat (6) is provided with
Anticreep locking plate (60), the anticreep locking plate (60) is provided with rotatable lamella (61) and slotted eye (62), and the rotatable lamella (61) is by riveting
Nail (63) is articulated with anticreep locking plate (60), and the anticreep locking plate (60) is correspondingly arranged with spacing bulb.
4. parachute jumping according to claim 1 separates clearance device with personnel, it is characterised in that the base (4) is provided with
Plug, first installing plate (7) is connected on plug with location-plate (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610748102.0A CN106672242B (en) | 2016-08-27 | 2016-08-27 | Personnel cut-off release device for parachuting |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610748102.0A CN106672242B (en) | 2016-08-27 | 2016-08-27 | Personnel cut-off release device for parachuting |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106672242A true CN106672242A (en) | 2017-05-17 |
| CN106672242B CN106672242B (en) | 2023-07-25 |
Family
ID=58839866
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610748102.0A Active CN106672242B (en) | 2016-08-27 | 2016-08-27 | Personnel cut-off release device for parachuting |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106672242B (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR69624E (en) * | 1956-06-29 | 1958-11-10 | Etudes Et Fab Aeronautiques | Device for controlling the opening of the bag of a parachute |
| US3942227A (en) * | 1974-08-09 | 1976-03-09 | G&H Technology, Inc. | Parachute riser buckle |
| US20020162916A1 (en) * | 2001-05-02 | 2002-11-07 | Jerome Baderspach | Fast evacuation device for aircraft |
| CN204046721U (en) * | 2014-04-21 | 2014-12-24 | 哈尔滨飞机工业集团有限责任公司 | A kind of equipment gathering parachute jumping data |
| CN104477478A (en) * | 2014-11-30 | 2015-04-01 | 航宇救生装备有限公司 | Air-drop anti-turning cargo table device |
| CN204898561U (en) * | 2015-06-10 | 2015-12-23 | 佛山市盛世伟德门控科技有限公司 | Airborne banister |
| CN204937462U (en) * | 2015-08-13 | 2016-01-06 | 中国航空工业集团公司西安飞机设计研究所 | A kind of landing gate air baffle |
| CN205998139U (en) * | 2016-08-27 | 2017-03-08 | 航宇救生装备有限公司 | A kind of parachute jumping separates clearance device with personnel |
-
2016
- 2016-08-27 CN CN201610748102.0A patent/CN106672242B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR69624E (en) * | 1956-06-29 | 1958-11-10 | Etudes Et Fab Aeronautiques | Device for controlling the opening of the bag of a parachute |
| US3942227A (en) * | 1974-08-09 | 1976-03-09 | G&H Technology, Inc. | Parachute riser buckle |
| US20020162916A1 (en) * | 2001-05-02 | 2002-11-07 | Jerome Baderspach | Fast evacuation device for aircraft |
| CN204046721U (en) * | 2014-04-21 | 2014-12-24 | 哈尔滨飞机工业集团有限责任公司 | A kind of equipment gathering parachute jumping data |
| CN104477478A (en) * | 2014-11-30 | 2015-04-01 | 航宇救生装备有限公司 | Air-drop anti-turning cargo table device |
| CN204898561U (en) * | 2015-06-10 | 2015-12-23 | 佛山市盛世伟德门控科技有限公司 | Airborne banister |
| CN204937462U (en) * | 2015-08-13 | 2016-01-06 | 中国航空工业集团公司西安飞机设计研究所 | A kind of landing gate air baffle |
| CN205998139U (en) * | 2016-08-27 | 2017-03-08 | 航宇救生装备有限公司 | A kind of parachute jumping separates clearance device with personnel |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106672242B (en) | 2023-07-25 |
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