CN205998139U - A kind of parachute jumping separates clearance device with personnel - Google Patents

A kind of parachute jumping separates clearance device with personnel Download PDF

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Publication number
CN205998139U
CN205998139U CN201620960603.0U CN201620960603U CN205998139U CN 205998139 U CN205998139 U CN 205998139U CN 201620960603 U CN201620960603 U CN 201620960603U CN 205998139 U CN205998139 U CN 205998139U
Authority
CN
China
Prior art keywords
plate
installing plate
connecting rod
personnel
mounting seat
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.)
Withdrawn - After Issue
Application number
CN201620960603.0U
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Chinese (zh)
Inventor
张鹍
邹长庚
陈涛
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
AVIC Aerospace Life Support Industries Ltd
Original Assignee
AVIC Aerospace Life Support Industries Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by AVIC Aerospace Life Support Industries Ltd filed Critical AVIC Aerospace Life Support Industries Ltd
Priority to CN201620960603.0U priority Critical patent/CN205998139U/en
Application granted granted Critical
Publication of CN205998139U publication Critical patent/CN205998139U/en
Withdrawn - After Issue legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model is related to the airborne technical field of parachute, refer in particular to a kind of parachute jumping and separate clearance device with personnel, including baffle plate, connecting rod, strut, base, adjust cable wire, mounting seat, first installing plate, second installing plate and location-plate, connecting rod one end is connected to baffle plate, the other end is connected to base, strut one end is connected to the second installing plate, the other end is correspondingly arranged with connecting rod, adjust cable wire one end and be connected to baffle plate, the other end is connected to mounting seat, first installing plate is connected to base with location-plate, mounting seat, first installing plate, second installing plate is fixed on aircraft side walls by screw respectively with location-plate.The utility model utilizes baffle mechanism horizontal for separating at hatch door, and can bear certain impact power, possesses certain protective capacities, effective guarantee personnel's personal safety.

Description

A kind of parachute jumping separates clearance device with personnel
Technical field
The utility model is related to the airborne technical field of parachute, refers in particular to a kind of parachute jumping and separates clearance device with personnel.
Background technology
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 at present Row cut-off or instruction of letting pass.Personnel's on-off system and like product is configured without on existing aircraft, and 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.
Content of the invention
For problem above, the utility model provides a kind of parachute jumping and separates clearance device with personnel, using a kind of baffle plate Mechanism is horizontal to be used at hatch door separating, and can bear certain impact power, possesses certain protective capacities, the effective guarantee personnel person Safety.
To achieve these goals, the technical solution adopted in the utility model is as follows:
A kind of parachute jumping separates clearance device with personnel, 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 are 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 baffle plate is connected to, the other end is connected to peace Dress seat, the first installing plate are connected to base with location-plate, and mounting seat, the first installing plate, the second installing plate and location-plate divide 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 by connecting rod and step 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 utility model has the beneficial effect that:
The utility model adopts such structure setting, and its simple structure, security performance preferably, do not affect to drop from the air personnel's Normally disembark, space in the cabin of very little is only taken up, to crew's work influence very little, the overall structure to aircraft and operation are equal Nothing affects.
Description of the drawings
Fig. 1 is the utility model overall structure figure;
Fig. 2 is the utility model understructure figure;
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
The technical solution of the utility model is illustrated with embodiment below in conjunction with the accompanying drawings.
As shown in Figures 1 to 4, the utility model parachute jumping includes baffle plate 1, connecting rod 2, strut with personnel's cut-off clearance device 3rd, base 4, regulation cable wire 5, mounting seat 6, the first installing plate 7, the second installing plate 8 and location-plate 9.
2 one end of connecting rod is bolted to baffle plate 1, and carried out by the dead bolt 10 of connecting rod 2 and step 20 spacing, 2 other end of connecting rod is bolted to base 4;3 one end of strut is connected to the second installing plate 8, the other end and connecting rod 2 pairs Should arrange;Adjust 5 one end of cable wire and baffle plate 1 is bolted to, 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 by screw respectively with location-plate 9 On aircraft side walls.
The utility model adopts purely mechanical structure, and wherein baffle plate 1, connecting rod 2, regulation cable wire 5 and base 4 passes through bolt Connection, and can be rotated along respective bolt, dead bolt 10 and step 20 is respectively provided with connecting rod 2, baffle plate 1 can be carried out Position locks, and adjusts cable wire 5 and is provided with 2 anti-spacing bulbs, and mounting seat 6 is provided with can be to the anti-lock-off of regulation 5 anticreep of cable wire Piece 60, anticreep locking plate 60 is provided be able to can be prevented to the slotted eye 62 of regulation 5 upper limit bulb of cable wire and rotatable lamella 61, rotatable lamella 61 Cable wire 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.
Utility model works principle:
In flight course, umbrella person is put when airborne instruction is executed and be manually operated baffle plate 1 is turned on along hatch door column Appropriate angle, forms parachute jumping passage in aircraft door mouth and lets pass for parachute jumping personnel;After previous parachutist disembarks or assign After cancelling airborne instruction, baffle plate 1 is horizontally placed at hatch door, cut-off state is rapidly converted into, the personnel that make subsequently to parachute stop disembarking, Parachute jumping front and rear baffle 1 forms certain protection all the time in putting between umbrella person and hatch door to putting umbrella person.
Utility model works flow process is as follows:
Baffle plate 1, connecting rod 2, base 4, regulation cable wire 5 are connected 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, now, and 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, horizontally rotates baffle plate 1,3 free end bulb of strut is connected with the groove in connecting rod 2, form triangle fixation spacing.
Embodiment of the present utility model is described above in conjunction with accompanying drawing, but the utility model is not limited to The specific embodiment that states, above-mentioned specific embodiment be only schematically, rather than restricted, this area common Technical staff of the present utility model enlightenment under, without departing from the utility model objective and scope of the claimed protection situation Under, also a lot of forms can be made, these are belonged within protection of the present utility model.

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 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), described first installing plate (7) and location-plate (9) is connected to base (4), mounting seat (6), the first installing plate (7), the second installing plate (8) is fixed on aircraft side walls by screw respectively with location-plate (9).
2. parachute jumping according to claim 1 separates clearance device with personnel, it is characterised in that connecting rod (2) one end Baffle plate (1) is bolted to, and spacing, the connecting rod is carried out with step (20) by the dead bolt (10) of connecting rod (2) (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 mounting seat (6) are provided with Anticreep locking plate (60), anticreep locking plate (60) are provided with rotatable lamella (61) and slotted eye (62), and described rotatable lamella (61) pass through riveting Nail (63) is articulated with anticreep locking plate (60), and anticreep locking plate (60) are correspondingly arranged with spacing bulb.
4. parachute jumping according to claim 1 separates clearance device with personnel, it is characterised in that base (4) are provided with Plug, the first installing plate (7) are connected on plug with location-plate (9).
CN201620960603.0U 2016-08-27 2016-08-27 A kind of parachute jumping separates clearance device with personnel Withdrawn - After Issue CN205998139U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620960603.0U CN205998139U (en) 2016-08-27 2016-08-27 A kind of parachute jumping separates clearance device with personnel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620960603.0U CN205998139U (en) 2016-08-27 2016-08-27 A kind of parachute jumping separates clearance device with personnel

Publications (1)

Publication Number Publication Date
CN205998139U true CN205998139U (en) 2017-03-08

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ID=58197631

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620960603.0U Withdrawn - After Issue CN205998139U (en) 2016-08-27 2016-08-27 A kind of parachute jumping separates clearance device with personnel

Country Status (1)

Country Link
CN (1) CN205998139U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106672242A (en) * 2016-08-27 2017-05-17 航宇救生装备有限公司 Personnel obstructing and releasing device for parachuting

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106672242A (en) * 2016-08-27 2017-05-17 航宇救生装备有限公司 Personnel obstructing and releasing device for parachuting

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C14 Grant of patent or utility model
GR01 Patent grant
AV01 Patent right actively abandoned
AV01 Patent right actively abandoned
AV01 Patent right actively abandoned

Granted publication date: 20170308

Effective date of abandoning: 20230725

AV01 Patent right actively abandoned

Granted publication date: 20170308

Effective date of abandoning: 20230725