CN212685915U - Seat anti-collision device of navigation aircraft - Google Patents
Seat anti-collision device of navigation aircraft Download PDFInfo
- Publication number
- CN212685915U CN212685915U CN202021193576.1U CN202021193576U CN212685915U CN 212685915 U CN212685915 U CN 212685915U CN 202021193576 U CN202021193576 U CN 202021193576U CN 212685915 U CN212685915 U CN 212685915U
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- seat
- base
- bedplate
- fixed mounting
- threaded rod
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- 238000005096 rolling process Methods 0.000 claims description 2
- 235000017166 Bambusa arundinacea Nutrition 0.000 abstract description 6
- 235000017491 Bambusa tulda Nutrition 0.000 abstract description 6
- 235000015334 Phyllostachys viridis Nutrition 0.000 abstract description 6
- 241001330002 Bambuseae Species 0.000 abstract description 5
- 239000011425 bamboo Substances 0.000 abstract description 5
- 208000027418 Wounds and injury Diseases 0.000 abstract description 3
- 230000006378 damage Effects 0.000 abstract description 3
- 208000014674 injury Diseases 0.000 abstract description 3
- 241000209128 Bambusa Species 0.000 abstract 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
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Abstract
The utility model belongs to the technical field of anticollision equipment, especially, be a navigation aircraft seat buffer stop, mostly lack the crashproof function to current aircraft seat, thereby make the problem to the injury of passenger's health easily when meetting vibrations, the scheme is presented as follows now, it includes the bedplate, top one side of bedplate is rotated and is installed the back, and the top of installing two dwangs is rotated to the bottom of bedplate, and two dwangs rotate to be connected, and the equal fixed mounting in bottom both sides of bedplate has the top of montant, and the equal movable mounting in the outside of two montants has the inboard of a cavity section of thick bamboo, and the bottom of two montants extends to the inside of a corresponding cavity section of thick bamboo respectively, and the bottom fixed mounting of two cavity sections of thick bamboos. The utility model discloses broken traditional seat immovable shortcoming, through the threaded rod that sets up, the rotation of threaded rod drives the screw cap and obtains the horizontally removal to make the back take place the slope, thereby satisfy different passengers' rest demand.
Description
Technical Field
The utility model relates to a anticollision device technical field especially relates to a navigation aircraft seat buffer stop.
Background
Aircraft seats, seats for flight personnel and passengers on board an aircraft. A pneumatic or mechanical mechanism is provided to operate the seat back to recline to allow the occupant to lie supine for maximum comfort and endurance.
Most of the existing aircraft seats lack an anti-collision function, so that the defects that the injury to the bodies of passengers is easily caused when the seats are in vibration are overcome, and therefore the anti-collision device for the aircraft seats for the navigation is provided for solving the problems.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the current aircraft seat and mostly lacking crashproof function, thereby causing the shortcoming to the injury of passenger's health easily when meetting vibrations, and the aircraft seat buffer stop that leads to the fact that proposes.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides a navigation aircraft seat buffer stop, the punch comprises a seat board, top one side of bedplate is rotated and is installed the back, the bottom of bedplate is rotated and is installed the top of two dwangs, two dwangs are rotated and are connected, the equal fixed mounting in bottom both sides of bedplate has the top of montant, the equal movable mounting in the outside of two montants has the inboard of cavity section of thick bamboo, the bottom of two montants extends to the inside of the cavity section of thick bamboo that corresponds respectively, the bottom fixed mounting of two cavity sections of thick bamboo has same base, the bottom of two dwangs all extends to the inside of base, the bottom of two dwangs all rotates and installs the runner, two runners all with the bottom inner wall roll connection of base, one side fixed mounting that the bottom of two dwangs is close to each other has same second spring, the bottom fixed mounting of bedplate has the top of two first springs.
Preferably, the top fixed mounting of base has the riser, and the outside top of riser is rotated and is installed the threaded rod, thereby is the riser through the setting and provides the rotation support point for the threaded rod.
Preferably, the outside threaded connection of threaded rod has the screw cap, and screw cap slidable mounting is in the outside of riser, and through the screw cap that sets up, the screw cap drives the connecting rod and removes to make the back take place to incline.
Preferably, the outside of back is rotated and is installed the one end of connecting rod, and the other end of connecting rod is rotated and is installed at the outside top of screw cap, and through the connecting rod that sets up, the removal of connecting rod makes the back slope to satisfy different passengers' rest demand.
Preferably, two through-holes have been seted up at the top of base, the outside of two dwang respectively with the inboard swing joint of the through-hole that corresponds, thereby make the dwang rotate through the through-hole that sets up.
Preferably, the one end fixed mounting of threaded rod has one side of carousel, and the opposite side fixed mounting of carousel has the handle, and is more laborsaving when making artifical rotation threaded rod through the handle that sets up.
In the utility model, the seat anti-collision device for the navigation aircraft can rotate two rotating rods through the rotating rods arranged when the seat vertically vibrates, so that two rotating wheels fixedly installed at the bottom ends of the two rotating rods roll in the base, and the seat is protected to a certain extent through the first spring and the second spring arranged;
the utility model discloses a threaded rod that sets up, the rotation of threaded rod drives the screw cap and obtains the horizontally removal to make the back take place the slope, thereby satisfy different passengers' rest demand.
Drawings
Fig. 1 is a schematic structural view of a seat anti-collision device of a navigable aircraft provided by the utility model;
fig. 2 is a schematic structural view of a portion a of the seat anti-collision device for a navigable aircraft according to the present invention;
fig. 3 is the utility model provides a structural schematic diagram of part B of navigation aircraft seat buffer stop.
In the figure: 1. a seat plate; 2. a backrest; 3. a vertical rod; 4. a hollow cylinder; 5. a first spring; 6. rotating the rod; 7. a second spring; 8. a base; 9. a vertical plate; 10. a threaded rod; 11. a threaded cap; 12. a connecting rod.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
Referring to fig. 1-3, a seat anti-collision device for a navigation aircraft comprises a seat plate 1, wherein a backrest 2 is rotatably installed on one side of the top of the seat plate 1, the bottom of the seat plate 1 is rotatably installed with the top ends of two rotating rods 6, the two rotating rods 6 are rotatably connected, the top ends of the two vertical rods 3 are fixedly installed on both sides of the bottom of the seat plate 1, the inner sides of hollow cylinders 4 are movably installed on the outer sides of the two vertical rods 3, the bottom ends of the two vertical rods 3 respectively extend into the corresponding hollow cylinders 4, the same base 8 is fixedly installed on the bottom of the two hollow cylinders 4, the bottom ends of the two rotating rods 6 both extend into the base 8, rotating wheels are rotatably installed on the bottom ends of the two rotating rods 6, the two rotating wheels are respectively in rolling connection with the inner wall of the bottom of the base 8, the same second spring 7 is fixedly installed on the side, which, the bottom ends of the two first springs 5 are fixedly arranged at the top of the base 8.
The utility model discloses in, base 8's top fixed mounting has riser 9, and the outside top of riser 9 is rotated and is installed threaded rod 10, thereby is riser 9 through the setting and provides the rotation strong point for threaded rod 10.
The utility model discloses in, threaded rod 10's outside threaded connection has screw cap 11, and screw cap 11 slidable mounting is in the outside of riser 9, and through the screw cap 11 that sets up, screw cap 11 drives connecting rod 12 and removes to make back 2 take place to incline.
The utility model discloses in, the outside of back 2 is rotated and is installed the one end of connecting rod 12, and the other end of connecting rod 12 is rotated and is installed at the outside top of screw cap 11, and through the connecting rod 12 that sets up, the removal of connecting rod 12 makes back 2 slope to satisfy different passengers's rest demand.
The utility model discloses in, two through-holes have been seted up at base 8's top, thereby the outside of two dwang 6 respectively with the inboard swing joint of the through-hole that corresponds, thereby make dwang 6 can rotate through the through-hole that sets up.
The utility model discloses in, the one end fixed mounting of threaded rod 10 has one side of carousel, and the opposite side fixed mounting of carousel has the handle, and is more laborsaving when making artifical rotation threaded rod 10 through the handle that sets up.
The working principle of the anti-collision device is as follows: through two dwang 6 that set up, when vertical vibrations take place for the seat, two dwang 6 can take place to rotate, thereby make two runners of two dwang 6's bottom fixed mounting roll in the inside of base 8, make first spring 5 compressed, second spring 7 is stretched, thereby play certain guard action to the seat, because first spring 5 and second spring 7 need carry out the reset function, thereby make bedplate 1 can reply initial condition, secondly through the threaded rod 10 that sets up, artifical rotation threaded rod 10, thereby drive the threaded cap 11 and obtain the horizontally and remove, make the same function of connecting rod 12, thereby make back 2 take place the slope, thereby satisfy different passenger's rest demand.
Claims (6)
1. The anti-collision device for the seat of the navigable aircraft comprises a seat plate (1) and is characterized in that a backrest (2) is rotatably installed on one side of the top of the seat plate (1), the top ends of two rotating rods (6) are rotatably installed on the bottom of the seat plate (1), the two rotating rods (6) are rotatably connected, the top ends of vertical rods (3) are fixedly installed on two sides of the bottom of the seat plate (1), the inner sides of hollow cylinders (4) are movably installed on the outer sides of the two vertical rods (3), the bottom ends of the two vertical rods (3) respectively extend into the corresponding hollow cylinders (4), the same base (8) is fixedly installed on the bottom of the two hollow cylinders (4), the bottom ends of the two rotating rods (6) both extend into the base (8), rotating wheels are rotatably installed on the bottom ends of the two rotating rods (6), and are both in rolling connection with the inner wall of the bottom of the base, one side fixed mounting that the bottom of two dwang (6) is close to each other has same second spring (7), and the bottom fixed mounting of bedplate (1) has the top of two first springs (5), and the equal fixed mounting in top of base (8) in bottom of two first springs (5).
2. The anti-collision device for the seat of the navigable aircraft according to claim 1, characterized in that a vertical plate (9) is fixedly mounted at the top of the base (8), and a threaded rod (10) is rotatably mounted at the top of the outer side of the vertical plate (9).
3. A seat impact protection device for a navigable aircraft according to claim 2, characterized in that the threaded rod (10) is externally threaded with a threaded cap (11), the threaded cap (11) being slidably mounted on the outside of the riser (9).
4. The seat collision avoidance device of the navigable aircraft according to claim 1, characterized in that the outside of the backrest (2) is rotatably mounted with one end of a connecting rod (12), and the other end of the connecting rod (12) is rotatably mounted on the top of the outside of the screw cap (11).
5. The anti-collision device for the seat of the navigable aircraft according to claim 1, wherein two through holes are formed in the top of the base (8), and the outer sides of the two rotating rods (6) are movably connected with the inner sides of the corresponding through holes respectively.
6. The anti-collision device for the seat of the navigable aircraft according to claim 2, characterized in that one end of the threaded rod (10) is fixedly provided with one side of a turntable, and the other side of the turntable is fixedly provided with a handle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021193576.1U CN212685915U (en) | 2020-06-24 | 2020-06-24 | Seat anti-collision device of navigation aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021193576.1U CN212685915U (en) | 2020-06-24 | 2020-06-24 | Seat anti-collision device of navigation aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212685915U true CN212685915U (en) | 2021-03-12 |
Family
ID=74894253
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021193576.1U Active CN212685915U (en) | 2020-06-24 | 2020-06-24 | Seat anti-collision device of navigation aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212685915U (en) |
-
2020
- 2020-06-24 CN CN202021193576.1U patent/CN212685915U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A collision avoidance device for navigation aircraft seats Effective date of registration: 20230802 Granted publication date: 20210312 Pledgee: Jingzhou Tiansheng Financing Guarantee Co.,Ltd. Pledgor: JINGZHOU JIANGHAN ZHONGLI INDUSTRIAL Co.,Ltd. Registration number: Y2023980050633 |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Granted publication date: 20210312 Pledgee: Jingzhou Tiansheng Financing Guarantee Co.,Ltd. Pledgor: JINGZHOU JIANGHAN ZHONGLI INDUSTRIAL Co.,Ltd. Registration number: Y2023980050633 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A collision avoidance device for aviation aircraft seats Granted publication date: 20210312 Pledgee: Hubei Science and Technology Financing Guarantee Co.,Ltd. Pledgor: JINGZHOU JIANGHAN ZHONGLI INDUSTRIAL Co.,Ltd. Registration number: Y2024980039039 |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right |