CN110816849B - Aircraft seat with head buffering anticollision function - Google Patents
Aircraft seat with head buffering anticollision function Download PDFInfo
- Publication number
- CN110816849B CN110816849B CN201911252814.3A CN201911252814A CN110816849B CN 110816849 B CN110816849 B CN 110816849B CN 201911252814 A CN201911252814 A CN 201911252814A CN 110816849 B CN110816849 B CN 110816849B
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- China
- Prior art keywords
- headrest
- spring
- fixing piece
- connecting piece
- piece
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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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- 230000003139 buffering effect Effects 0.000 title claims abstract description 10
- 210000002268 wool Anatomy 0.000 claims description 9
- 230000006835 compression Effects 0.000 claims description 6
- 238000007906 compression Methods 0.000 claims description 6
- 239000000463 material Substances 0.000 claims description 4
- 229910000851 Alloy steel Inorganic materials 0.000 claims description 3
- 239000006260 foam Substances 0.000 claims description 3
- 239000002245 particle Substances 0.000 claims description 3
- 239000000956 alloy Substances 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- JTIJZYSPRDTGGH-UHFFFAOYSA-L disodium;2-nitro-5-sulfonatosulfanylbenzoate Chemical compound [Na+].[Na+].[O-]C(=O)C1=CC(SS([O-])(=O)=O)=CC=C1[N+]([O-])=O JTIJZYSPRDTGGH-UHFFFAOYSA-L 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
- 125000006850 spacer group Chemical group 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
Images
Classifications
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- 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
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0619—Arrangements of seats, or adaptations or details specially adapted for aircraft seats with energy absorbing means specially adapted for mitigating impact loads for passenger seats, e.g. at a crash
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Seats For Vehicles (AREA)
Abstract
The invention discloses an aircraft seat with a head buffering and anti-collision function, which comprises a cushion, wherein a backrest is arranged on one side of the top of the cushion, handrails are arranged in the middle parts of two side edges of the backrest, a headrest is arranged on the top of the backrest, the headrest comprises a headrest body, two sides of the headrest body are respectively provided with a headrest flank, the headrest body is movably connected with the headrest flanks on two sides through bolts, a support frame is arranged in the headrest flanks, a buffer is arranged between the headrest flanks and the support frame, a buffer area is arranged in the middle part of one side, opposite to the headrest flanks, of two sides, a fastener and a connecting piece are arranged at the bottom of one side, opposite to the headrest flanks, a vertical groove and a transverse groove are arranged in the fastener, the transverse groove is positioned at the lower right side of the vertical groove, and a first spring gasket is arranged at the bottom of the vertical groove. Has the advantages that: the buffer zone can effectively prevent the head of the passenger from colliding with other objects due to forward tilting.
Description
Technical Field
The invention relates to the technical field of seats, in particular to an aircraft seat with a head buffering and anti-collision function.
Background
In the seventies of the last century, with the development of new technological revolution and technology, a great deal of alloy materials have come to be used for seats of airplanes. Aircraft seats are becoming lighter in weight, but the overload experienced by aircraft seats has continued for the 9G overload required in the 1952 s. Since 1980, the normal landing speed of a large jet airliner can reach 280 km/h, the brake overload acting on a human body during crash can reach 25G, and the airplane still has a seat which is installed according to the previous standard and bears the static load of 9G. In 25.1.1990, the 052 flight of columbia aviation, a boeing 707 with an old seat crashed on the mountain of the long island near the new york airport due to the exhaustion of fuel, the airplane was dropped into two parts under violent impact, 85 passengers survived and 73 passengers died. The NTSB American air crash investigator found a fact in investigation that the seat which can bear the overload of 9G according to the design standard in 1953 does not play a good role in protecting the passenger during the crash of the airplane, and the support legs of the seat of the airplane are broken during the crash of the airplane with more than 15G, so that the passenger flies on the seat fixed by the safety belt and collides with the passenger in front. The body and the floor of the airplane are still intact, the safety belt of the airplane is not broken, but the seat of the airplane is fallen off, so that the passenger who uses the safety belt to bind on the seat loses the function of protecting the passenger because the safety integrity of the seat of the airplane is damaged.
In summary, how to provide an aircraft seat with a head buffering and anti-collision function is a technical problem which needs to be solved urgently at present.
Disclosure of Invention
The invention aims at the defects and provides an aircraft seat with a head buffering and anti-collision function to solve the problems in the prior art.
The technical scheme of the invention is realized as follows:
an aircraft seat with a head buffering and anti-collision function comprises a cushion, wherein a backrest is arranged on one side of the top of the cushion, handrails are arranged in the middle of two side edges of the backrest, a headrest is arranged on the top of the backrest and comprises a headrest body, headrest side wings are arranged on two sides of the headrest body, the headrest body is movably connected with the headrest side wings on the two sides through bolts, a support frame is arranged in each headrest side wing, a buffer is arranged between each headrest side wing and the support frame, a buffer area is arranged in the middle of one side, opposite to each headrest side wing, of each headrest side wing, a fastener and a connecting piece are arranged at the bottom of one side, opposite to each headrest side wing, of each headrest side wing, a vertical groove and a horizontal groove are formed in each fastener, the horizontal groove is located at the right lower part of the vertical groove, a first spring gasket is arranged at the bottom of the vertical groove, a first spring is arranged at the top of the first spring gasket, the top of the first spring is provided with a fixing piece, one side of the fixing piece, which is far away from the transverse groove, is provided with a push plate, the push plate penetrates through the side wall of the fixing piece and extends to the outside of the fixing piece, one side of the fixing piece, which is far away from the transverse groove, is provided with a second spring gasket, the second spring gasket is welded and fixed with the push plate, the second spring gasket is close to one side of the fixing piece and is provided with a second spring, and the center of the connecting piece is provided with a round hole.
Preferably, the buffer is made of pearl wool, and the buffer area is filled with foam particles made of pearl wool.
Preferably, the headrest body is filled with pearl wool, and the support frame is made of a low alloy steel material.
Preferably, the first spring is a compression spring, and the elastic force of the first spring is greater than the sum of the dead weights of the first spring and the fixed part.
Preferably, the second spring is a compression spring, and the elasticity of the second spring is greater than the sum of the dead weights of the push plate, the second spring spacer and the second spring.
Preferably, the diameter of the circular hole at the center of the connecting member is slightly larger than the diameter of the fixing member.
Compared with the prior art, the invention has the advantages and positive effects that:
1. the buffer zone can effectively prevent the head of the passenger from colliding with other objects due to forward tilting.
2. The filler in the side wings of the headrest can protect the two sides of the head of a passenger from being impacted by other objects, so that the passenger is safer and more comfortable.
3. The headrest flank passes through bolt and this body coupling of headrest, and the passenger can be as required, angle adjustment.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed in the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings without creative efforts.
FIG. 1 is a side view of an embodiment in accordance with the invention;
FIG. 2 is a top view of a headrest according to an embodiment of the invention;
FIG. 3 is a schematic view of the internal structure of a fastener according to an embodiment of the invention;
fig. 4 is an elevation view of a connector according to an embodiment of the present invention.
In the figure:
1. a cushion; 2. a backrest; 3. a handrail; 4. a headrest body; 5. a headrest flank; 6. a support frame; 7. A buffer; 8. a bolt; 9. a buffer area; 10. a fastener; 11. a connecting member; 12. a first spring washer; 13. a first spring; 14. a fixing member; 15. a second spring washer; 16. a second spring; 17. a push plate.
Detailed Description
In order that the above objects, features and advantages of the present invention can be more clearly understood, the present invention will be further described with reference to the accompanying drawings and examples. It should be noted that the embodiments and features of the embodiments of the present application may be combined with each other without conflict.
The invention is further described with reference to the following figures and specific examples.
In the first embodiment, as shown in fig. 1, an aircraft seat with a head buffering and anti-collision function according to an embodiment of the invention comprises a seat cushion 1, a backrest 2 is arranged on one side of the top of the seat cushion 1, armrests 3 are arranged in the middle of two side edges of the backrest 2, a headrest is arranged on the top of the backrest 2, the headrest comprises a headrest body 4, headrest side wings 5 are arranged on two sides of the headrest body 4, the headrest body 4 is movably connected with the headrest side wings 5 on two sides through bolts 8, support frames 6 are arranged in the headrest side wings 5, a buffer 7 is arranged between the headrest side wings 5 and the support frames 6, a buffer zone 9 is arranged in the middle of one side of the headrest side wings 5 on two sides, a fastener 10 and a connecting piece 11 are arranged at the bottom of one side of the headrest side wings 5 on two sides, a vertical groove and a horizontal groove are arranged in the fastener 10, just horizontal recess is located the right side below of vertical recess, vertical recess bottom is equipped with spring gasket one 12, spring gasket one 12 tops is equipped with spring one 13, spring one 13 tops is equipped with mounting 14, keep away from in the horizontal recess 14 one side of mounting is equipped with push pedal 17, push pedal 17 runs through fastener 10 lateral wall extends to fastener 10 is outside, keep away from in the horizontal recess 14 one side of mounting is equipped with two 15 of spring gasket, two 15 of spring gasket with push pedal 17 welded fastening, two 15 of spring gasket are close to 14 one side of mounting is equipped with two 16 of spring, 11 center departments of connecting piece are equipped with the round hole.
In the second embodiment, as shown in fig. 2, the buffer 7 is made of pearl wool, and the buffer area 9 is filled with foam particles made of pearl wool material.
In the third embodiment, as shown in fig. 2, pearl wool is filled in the headrest body 4, the support frame 6 is made of a low alloy steel material, and the diameter of the circular hole at the center of the connecting member 11 is slightly larger than that of the fixing member 14.
In a fourth embodiment, as shown in fig. 3, the first spring 13 is a compression spring, and the elastic force of the first spring 13 is greater than the sum of the self weights of the first spring 13 and the fixing member 14.
In a fifth embodiment, as shown in fig. 3, the second spring 16 is a compression spring, and the elastic force of the second spring 16 is greater than the sum of the dead weights of the three members, i.e., the push plate 17, the second spring washer 15 and the second spring 16.
For the convenience of understanding the technical solutions of the present invention, the following detailed description will be made on the working principle or the operation mode of the present invention in the practical process.
In practical application, when a passenger sits on the seat, firstly, the headrest side wings 5 on two sides are folded inwards, then the connecting piece 11 is inserted into the fastening piece 10, the connecting piece 11 advances along the groove in the fastening piece 10 until reaching the oblique notch at the top end of the fixing piece 14, at the moment, the fixing piece 14 falls down along the advancing of the connecting piece 11, at the moment, the spring I13 is in a compressed state, and when the round hole at the center of the connecting piece 11 reaches the top end of the fixing piece 14, the elastic force of the spring I13 can enable the fixing piece 14 to be sprung until the fixing piece 14 is positioned in the round hole at the center of the connecting piece 11, at the moment. The connecting piece 11 is connected with the fastener 10, and when impact occurs, the supporting frames 6 and the buffer 7 of the headrest side wings 5 can protect the two sides of the head of a passenger from being impacted by foreign objects and play a role in buffer protection; when passengers get off the airplane, the push plate 17 is pushed, the push plate 17 is inserted into the bayonet at the middle part of the fixing piece 14, the fixing piece 14 can gradually descend along with the extension of the push plate 17, and when the top end of the fixing piece 14 is separated from the connecting piece 11, the connecting piece 11 can automatically fall off.
The present invention can be easily implemented by those skilled in the art from the above detailed description. It should be understood, however, that the intention is not to limit the invention to the particular embodiments described. On the basis of the disclosed embodiments, a person skilled in the art can combine different technical features at will, thereby implementing different technical solutions.
Claims (1)
1. The aircraft seat with the head buffering and anti-collision function is characterized by comprising a seat cushion (1), wherein a backrest (2) is arranged on one side of the top of the seat cushion (1), handrails (3) are arranged in the middle of the two side edges of the backrest (2), a headrest is arranged on the top of the backrest (2), the headrest comprises a headrest body (4), headrest side wings (5) are arranged on the two sides of the headrest body (4), the headrest side wings (5) on the two sides of the headrest body (4) are movably connected with each other through bolts (8), support frames (6) are arranged in the headrest side wings (5), a buffer (7) is arranged between the headrest side wings (5) and the support frames (6), buffer areas (9) are arranged in the middle of the opposite side of the headrest side wings (5), fasteners (10) and connecting pieces (11) are arranged at the bottom of the opposite side of the headrest side wings (5), a vertical groove and a horizontal groove are arranged in the fastener (10), the horizontal groove is positioned at the lower right part of the vertical groove, a first spring gasket (12) is arranged at the bottom of the vertical groove, a first spring (13) is arranged at the top of the first spring gasket (12), a fixing piece (14) is arranged at the top of the first spring (13), a push plate (17) is arranged on one side, far away from the fixing piece (14), in the transverse groove, the push plate (17) extends through the side wall of the fastener (10) to the outside of the fastener (10), a second spring gasket (15) is arranged on one side of the transverse groove far away from the fixing piece (14), the second spring gasket (15) is welded and fixed with the push plate (17), a second spring (16) is arranged on one side, close to the fixing piece (14), of the second spring gasket (15), and a round hole is formed in the center of the connecting piece (11); the buffer (7) is made of pearl wool, and the buffer area (9) is filled with foam particles made of pearl wool; the headrest body (4) is filled with pearl wool, and the support frame (6) is made of low-alloy steel materials; the first spring (13) is a compression spring, and the elastic force of the first spring (13) is greater than the sum of the dead weights of the first spring (13) and the fixed part (14); the second spring (16) is a compression spring, and the elasticity of the second spring (16) is greater than the sum of the dead weights of the push plate (17), the second spring gasket (15) and the second spring (16); the diameter of a round hole in the center of the connecting piece (11) is slightly larger than that of the fixing piece (14);
when a passenger sits on the seat, firstly, the headrest side wings (5) on two sides are folded inwards, then the connecting piece (11) is inserted into the fastening piece (10), the connecting piece (11) advances along the groove in the fastening piece (10) until reaching the inclined notch at the top end of the fixing piece (14), at the moment, the fixing piece (14) falls down along with the advancing of the connecting piece (11), the spring I (13) is in a compressed state, when the round hole at the center of the connecting piece (11) reaches the top of the fixing piece (14), the elastic force of the spring I (13) can enable the fixing piece (14) to be sprung up until the fixing piece (14) is positioned in the round hole at the center of the connecting piece (11), at the moment, the connecting piece (11) is connected with the fastening piece (10), and when collision occurs, the supporting frames (6) and the buffer (7) of the headrest side wings (5) can protect two sides of the head of the passenger from being collided by foreign objects, and play a role in buffering protection; when passengers get off the airplane, the passengers only need to push the push plate (17), the push plate (17) is inserted into the bayonet at the middle part of the fixing piece (14), the fixing piece (14) can gradually descend along with the extension of the push plate (17), and when the top end of the fixing piece (14) is separated from the connecting piece (11), the connecting piece (11) can automatically fall off.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911252814.3A CN110816849B (en) | 2019-12-09 | 2019-12-09 | Aircraft seat with head buffering anticollision function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911252814.3A CN110816849B (en) | 2019-12-09 | 2019-12-09 | Aircraft seat with head buffering anticollision function |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN110816849A CN110816849A (en) | 2020-02-21 |
| CN110816849B true CN110816849B (en) | 2022-06-07 |
Family
ID=69544214
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201911252814.3A Active CN110816849B (en) | 2019-12-09 | 2019-12-09 | Aircraft seat with head buffering anticollision function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110816849B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111950127B (en) * | 2020-07-15 | 2022-03-01 | 中国核动力研究设计院 | Method and system for testing safety performance of low alloy steel material for nuclear energy equipment |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8251444B2 (en) * | 2005-04-25 | 2012-08-28 | Arjuna Indraeswaran Rajasingham | Vehicle occupant support |
| DE202007017085U1 (en) * | 2007-12-05 | 2008-02-21 | Semsch, Angelika | Kopftippschutzvorrichtung and Kopftippschutzvorrichtung containing arrangement |
| US10315773B1 (en) * | 2015-12-14 | 2019-06-11 | Haeco Americas, Inc. | Seat system having an adjustable wraparound headrest |
| WO2017118868A1 (en) * | 2016-01-07 | 2017-07-13 | Mueller Thomas R A | Passenger seat comprising tiltable sections of its headrest |
| CN205770172U (en) * | 2016-06-28 | 2016-12-07 | 北京安达维尔航空设备有限公司 | It is applicable to the handrail of economy seats |
| CN106741965A (en) * | 2017-01-22 | 2017-05-31 | 湖北航宇嘉泰飞机设备有限公司 | For the energy absorption device of aero seat |
| CN109278602B (en) * | 2018-08-29 | 2024-05-24 | 布童安全科技(宁波)有限公司 | Neck flank shock-absorbing structure, safety headrest and child safety seat |
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2019
- 2019-12-09 CN CN201911252814.3A patent/CN110816849B/en active Active
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| Publication number | Publication date |
|---|---|
| CN110816849A (en) | 2020-02-21 |
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Effective date of registration: 20221228 Address after: Room 2202, 22 / F, Wantong building, No. 3002, Sungang East Road, Sungang street, Luohu District, Shenzhen City, Guangdong Province Patentee after: Shenzhen dragon totem technology achievement transformation Co.,Ltd. Address before: 256603 No. five, No. 391, the Yellow River Road, Shandong, Binzhou Patentee before: BINZHOU University |
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