CN106923563A - A kind of Electric mattress inner frame structure - Google Patents

A kind of Electric mattress inner frame structure Download PDF

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Publication number
CN106923563A
CN106923563A CN201710281441.7A CN201710281441A CN106923563A CN 106923563 A CN106923563 A CN 106923563A CN 201710281441 A CN201710281441 A CN 201710281441A CN 106923563 A CN106923563 A CN 106923563A
Authority
CN
China
Prior art keywords
area
framework
wing aircraft
end set
clip
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.)
Pending
Application number
CN201710281441.7A
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Chinese (zh)
Inventor
蔡方正
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.)
Shanghai Jing Jian Trading Co Ltd
Original Assignee
Shanghai Jing Jian Trading Co 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 Shanghai Jing Jian Trading Co Ltd filed Critical Shanghai Jing Jian Trading Co Ltd
Priority to CN201710281441.7A priority Critical patent/CN106923563A/en
Publication of CN106923563A publication Critical patent/CN106923563A/en
Pending legal-status Critical Current

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Classifications

    • AHUMAN NECESSITIES
    • A47FURNITURE; DOMESTIC ARTICLES OR APPLIANCES; COFFEE MILLS; SPICE MILLS; SUCTION CLEANERS IN GENERAL
    • A47CCHAIRS; SOFAS; BEDS
    • A47C27/00Spring, stuffed or fluid mattresses or cushions specially adapted for chairs, beds or sofas

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  • Mattresses And Other Support Structures For Chairs And Beds (AREA)

Abstract

The invention discloses a kind of Electric mattress inner frame structure, including mattress inside casing, all-wing aircraft sparerib shelf and Xia Jian areas sparerib shelf, the mattress inside casing includes that first area's framework, second area's framework, the 3rd area's framework and the 4th area's framework, first area's framework, second area's framework, the 3rd area's framework and the 4th area's framework are metal framework structure, and first area's framework, second area's framework, the 3rd area's framework and the 4th area's base of frame are fixedly connected on the banded plate of bottom;First area's frame roof is provided with cephalic protection sizing cotton, and cephalic protection sizing cotton lower section is provided with an all-wing aircraft sparerib shelf, and all-wing aircraft sparerib shelf lower section is provided with Xia Jian areas sparerib shelf;Simple structure of the present invention, stability is strong, the impulse stroke of the compression of the adjustable end set of strength can be changed by the insertion number for changing soft or hard adjusting plug, so as to change the soft or hard degree of mattress, user can be met under all ages and classes period and physical qualification, to the demand of mattress supports soft durometer change.

Description

A kind of Electric mattress inner frame structure
Technical field
The present invention relates to field of fixture equipment, specifically a kind of Electric mattress inner frame structure.
Background technology
With the improvement of people ' s living standards, requirement more and more higher of the people to quality of life, convenient, health, high-quality Target of the life as higher pursues of life, high-quality life be unable to do without high-quality sleep, people's length of one's sleep one in life As exceed whole life 1/3, research find, improve sleep quality have much relations with four elementses, the apparatus exactly slept, The posture of sleep, the time of sleep and the environment of sleep.
Currently, the bedding product such as sleep sping mattress of commercial type, be when dispatching from the factory one-shot forming and closing not Disassembled bedding product, we are referred to as " conventional mattresses ", and the type mattress is seen everywhere on the market in China.
Conventional mattresses during user's use, obvious defect and deficiency below long-term existence, so as to influence user's Experience and ease of use, are never hacked and are lifted improvement;The soft durometer of " conventional mattresses " will determine throughout one's life once being molded Property, it is impossible to adapt to the preference that user's body changes in different times to mattress supports soft durometer.
The content of the invention
It is an object of the invention to provide a kind of Electric mattress inner frame structure, with asking for solving to propose in above-mentioned background technology Topic.
To achieve the above object, the present invention provides following technical scheme:
A kind of Electric mattress inner frame structure, including mattress inside casing, all-wing aircraft sparerib shelf and Xia Jian areas sparerib shelf, the mattress inside casing bag Include first area's framework, second area's framework, the 3rd area's framework and the 4th area's framework, first area's framework, second area's framework, the 3rd area's frame Frame and the 4th area's framework are metal framework structure, first area's framework, second area's framework, the 3rd area's framework and the 4th area's framework bottom Portion is fixedly connected on the banded plate of bottom;First area's frame roof is provided with cephalic protection sizing cotton, under cephalic protection sizing cotton Side is provided with an all-wing aircraft sparerib shelf, and all-wing aircraft sparerib shelf lower section is provided with Xia Jian areas sparerib shelf;Secondth area framework is provided with three All-wing aircraft sparerib shelf, the 3rd area's framework is provided with two all-wing aircraft sparerib shelfs, and the 4th area's framework is provided with three all-wing aircraft rows Skeleton, the 4th area's base of frame is provided with tail defense sizing cotton.
Further, the all-wing aircraft sparerib shelf includes end set clip, the adjustable end set of strength, space glass fiber rod, soft or hard Adjusting plug and all-wing aircraft blade, end set clip are symmetrical arranged the both sides being fixed on the inside of mattress inside casing, the adjustable end inserting of strength It is connected on the set clip of end, space glass fiber rod is plugged on the set clip of end, and some all-wing aircraft blades are provided with space glass fiber rod.
Further, Xia Jian areas sparerib shelf includes that chop frame end set, end cover clip, space glass fiber rod and all-wing aircraft leaf Piece, skeleton end set is connected on the set clip of end, and space glass fiber rod is plugged between the set of skeleton end, and all-wing aircraft blade is movably arranged on On space glass fiber rod;The chop frame end set left and right sides is arranged with the second grafting set being adapted to inserting column, chop frame end Set top is provided with three the second glass drill steels and inserts.
Further, the end set clip top is provided with the platform for being overlapped on arch in mattress, end set clip Side offers three counter sinks, and the screwed hole being adapted to counter sink is offered on the inwall of mattress inside casing, and end set clip leads to Cross counter sink screwed hole and being equipped with for bolt be fixed on mattress inside casing, end set clip bottom is provided with two inserting columns, End set clip is injection moulding integrated molding structure.
Further, the adjustable end set of the strength is elastoplast injection moulding integrated molding structure, the adjustable end set of strength Bottom is provided with the first grafting set being adapted to inserting column, the adjustable end set of strength be provided with from bottom to top three regulation slotting rings, one First glass drill steel slotting ring and a dome, the first glass drill steel slotting ring inwall are arranged with two fixed strips, three regulation slotting rings and It is fixedly connected between first glass drill steel slotting ring, wherein the regulation slotting ring, the first glass drill steel slotting ring and dome positioned at top pass through The bottom of the adjustable end set of connection strap connection strength of arc, soft or hard adjusting plug is plugged with regulation slotting ring;Wherein adjust slotting ring It is the structure of both ends open, the first glass drill steel slotting ring is the structure of one end closing.
Further, the space glass fiber rod bottom offers groove, and groove alleviates the overall weight of space glass fiber rod, Space glass fiber rod both sides offer fixing groove, and fixing groove is equipped with the fixed strip in the first glass drill steel slotting ring.
Further, the all-wing aircraft blade bottom is arranged with clip, and clip is equipped with fixing groove, all-wing aircraft leaf Piece is movably arranged on space glass fiber rod.
Compared with prior art, simple structure of the present invention, stability is strong, by all-wing aircraft sparerib shelf and Xia Jian areas sparerib shelf It is independently arranged, each all-wing aircraft sparerib shelf and Xia Jian areas sparerib shelf non-interference, by the insertion number for changing soft or hard adjusting plug The impulse stroke of the compression of the adjustable end set of strength can be changed, so as to change the soft or hard degree of mattress, conventional mattresses are solved soft The shortcoming that hardness can not be adjusted arbitrarily, can meet user under all ages and classes period and physical qualification, soft or hard to mattress supports Spend the demand of change, it is to avoid change cost and the wasting of resources that mattress is caused.
Brief description of the drawings
Fig. 1 is the top view of Electric mattress inner frame structure.
Fig. 2 is the side view of Electric mattress inner frame structure.
Fig. 3 is the front view of Electric mattress inner frame structure.
Fig. 4 is the structural representation of all-wing aircraft sparerib shelf in Electric mattress inner frame structure.
Fig. 5 is the front view that Electric mattress inner frame structure middle-end covers clip.
Fig. 6 is the side view that Electric mattress inner frame structure middle-end covers clip.
Fig. 7 holds the front view of set strongly to be can adjust in Electric mattress inner frame structure.
Fig. 8 holds the side view of set strongly to be can adjust in Electric mattress inner frame structure.
Fig. 9 holds the top view of set strongly to be can adjust in Electric mattress inner frame structure.
Figure 10 is the sectional view of space glass fiber rod in Electric mattress inner frame structure.
Figure 11 is the top view of all-wing aircraft blade in Electric mattress inner frame structure.
Figure 12 is the side view of all-wing aircraft blade in Electric mattress inner frame structure.
Figure 13 is the three-view diagram of soft or hard adjusting plug in Electric mattress inner frame structure.
Figure 14 is the front view of chop frame end set in Electric mattress inner frame structure.
Figure 15 is the rearview of chop frame end set in Electric mattress inner frame structure.
Specific embodiment
The technical scheme of this patent is described in more detail with reference to specific embodiment.
Refer to Fig. 1-15, a kind of Electric mattress inner frame structure, including mattress inside casing, all-wing aircraft sparerib shelf 6 and Xia Jian areas row Skeleton 7, the mattress inside casing includes first area's framework 1, second area's framework 2, the 3rd area's framework 3 and the 4th area's framework 4, the firstth area Framework 1, second area's framework 2, the 3rd area's framework 3 and the 4th area's framework 4 are metal framework structure, first area's framework 1, the secondth area Framework 2, the 3rd area's framework 3 and the bottom of the 4th area's framework 4 are fixedly connected on bottom banded plate 5;Install at the top of first area's framework 1 There is cephalic protection sizing cotton 11, the lower section of cephalic protection sizing cotton 11 is provided with an all-wing aircraft sparerib shelf 6, and the lower section of all-wing aircraft sparerib shelf 6 sets You Xiajian areas sparerib shelf 7;Secondth area framework 2 is provided with three all-wing aircraft sparerib shelfs 6, and the 3rd area's framework 3 is provided with two Root all-wing aircraft sparerib shelf 6, the 4th area's framework 4 is provided with three all-wing aircraft sparerib shelfs 6, and the bottom of the 4th area's framework 4 is provided with afterbody and prevents Shield sizing cotton 41;
The all-wing aircraft sparerib shelf 6 includes that end covers the adjustable end set 62, space glass fiber rod 63 of clip 61, strength, soft or hard adjusting plug 64 and all-wing aircraft blade 65, end set clip 61 is symmetrical arranged the both sides being fixed on the inside of mattress inside casing, the adjustable end set 62 of strength It is plugged on the set clip 61 of end, space glass fiber rod 63 is plugged on the set clip 61 of end, if being provided with space glass fiber rod 63 Dry all-wing aircraft blade 65;
The top of end set clip 61 is provided with the platform 611 for being overlapped on arch in mattress, and the side of end set clip 61 is opened Three counter sinks 612 are provided with, the screwed hole being adapted to counter sink 612, end set clip 61 are offered on the inwall of mattress inside casing It is fixed on mattress inside casing by the screwed hole of counter sink 612 and being equipped with for bolt, end set clip 61 bottom is provided with two Inserting column 613, end set clip 61 is injection moulding integrated molding structure;
The adjustable end set 62 of the strength is elastoplast injection moulding integrated molding structure, adjustable 62 bottoms of end set of strength be provided with The first grafting set 621 of the adaptation of inserting column 613, the adjustable end set 62 of strength is provided with three regulation slotting rings 622, from bottom to top First glass drill steel slotting ring 623 and a dome 624, the inwall of the first glass drill steel slotting ring 623 are arranged with two fixed strips 625, three It is fixedly connected between the individual regulation glass drill steel slotting ring 623 of slotting ring 622 and first, wherein regulation slotting ring 622, the first glass positioned at top Drill steel slotting ring 623 and dome 624 connect the bottom of the adjustable end set 62 of strength by the connection strap 645 of arc, adjust slotting ring Soft or hard adjusting plug 64 is plugged with 622, the adjustable end set 62 of strength can be changed by the insertion number for changing soft or hard adjusting plug 64 Compression impulse stroke, so as to change the soft or hard degree of mattress;Wherein regulation slotting ring 622 is the structure of both ends open, first Glass drill steel slotting ring 623 is the structure of one end closing;
The bottom of space glass fiber rod 63 offers groove, and groove alleviates the overall weight of space glass fiber rod 63, space glass The both sides of bar 63 offer fixing groove 631, and fixing groove 631 is equipped with the fixed strip 625 in the first glass drill steel slotting ring 623;
The bottom symmetrical of all-wing aircraft blade 65 is provided with clip 651, and clip 651 is equipped with fixing groove 631, all-wing aircraft blade 65 are movably arranged on space glass fiber rod 63;
Xia Jian areas sparerib shelf 7 includes that chop frame end set 71, end covers clip 61, space glass fiber rod 63 and all-wing aircraft blade 65, Skeleton end set 71 is connected on the set clip 61 of end, and space glass fiber rod 63 is plugged between skeleton end set 71, and all-wing aircraft blade 65 is lived It is dynamic to be arranged on space glass fiber rod 63;The chop frame end covers 71 left and right sides and is arranged with second be adapted to inserting column 613 Grafting set 711, the top of chop frame end set 71 is provided with three the second glass drill steels and inserts 712.
The better embodiment to this patent is explained in detail above, but this patent is not limited to above-mentioned embodiment party Formula, in the ken that one skilled in the relevant art possesses, can also be on the premise of this patent objective not be departed from Make a variety of changes.

Claims (7)

1. a kind of Electric mattress inner frame structure, including mattress inside casing, all-wing aircraft sparerib shelf and Xia Jian areas sparerib shelf, it is characterised in that The mattress inside casing includes first area's framework, second area's framework, the 3rd area's framework and the 4th area's framework, first area's framework, second Area's framework, the 3rd area's framework and the 4th area's framework are metal framework structure, first area's framework, second area's framework, the 3rd area's frame Frame and the 4th area's base of frame are fixedly connected on the banded plate of bottom;First area's frame roof is provided with cephalic protection sizing cotton, Cephalic protection sizing cotton lower section is provided with an all-wing aircraft sparerib shelf, and all-wing aircraft sparerib shelf lower section is provided with Xia Jian areas sparerib shelf;Described second Area's framework is provided with three all-wing aircraft sparerib shelfs, and the 3rd area's framework is provided with two all-wing aircraft sparerib shelfs, the 4th area's framework Three all-wing aircraft sparerib shelfs are installed, the 4th area's base of frame is provided with tail defense sizing cotton.
2. Electric mattress inner frame structure according to claim 1, it is characterised in that the all-wing aircraft sparerib shelf includes that end set is solid The adjustable end set of fixed button, strength, space glass fiber rod, soft or hard adjusting plug and all-wing aircraft blade, end set clip are symmetrical arranged and are fixed on Both sides on the inside of mattress inside casing, the adjustable end set of strength is plugged on the set clip of end, and space glass fiber rod is plugged on end set and fixes Buckle, some all-wing aircraft blades are provided with space glass fiber rod.
3. Electric mattress inner frame structure according to claim 1, it is characterised in that Xia Jian areas sparerib shelf includes chop Frame end set, end cover clip, space glass fiber rod and all-wing aircraft blade, and skeleton end set is connected on the set clip of end, space glass fiber rod It is plugged between the set of skeleton end, all-wing aircraft blade is movably arranged on space glass fiber rod;The chop frame end set left and right sides is symmetrical The second grafting set being adapted to inserting column is provided with, chop frame end set top is provided with three the second glass drill steels and inserts.
4. Electric mattress inner frame structure according to claim 2, it is characterised in that the end set clip top is provided with takes The platform of arch in mattress is connected on, the side of end set clip offers three counter sinks, opened up on the inwall of mattress inside casing There is the screwed hole being adapted to counter sink, end set clip is fixed in mattress by counter sink screwed hole and being equipped with for bolt On frame, end set clip bottom is provided with two inserting columns, and end set clip is injection moulding integrated molding structure.
5. Electric mattress inner frame structure according to claim 2, it is characterised in that the adjustable end set of the strength is elasticity Plastic injection integrated formed structure, the adjustable end set bottom of strength is provided with the first grafting set being adapted to inserting column, and strength is adjustable Section end set is provided with three regulation slotting rings, a first glass drill steel slotting ring and a domes from bottom to top, in the first glass drill steel slotting ring Wall is arranged with two fixed strips, is fixedly connected between three regulation slotting rings and the first glass drill steel slotting ring, wherein positioned at top Regulation slotting ring, the first glass drill steel slotting ring and dome connect the bottom of the adjustable end set of strength, regulation by the connection strap of arc Soft or hard adjusting plug is plugged with slotting ring;Wherein regulation slotting ring is the structure of both ends open, and the first glass drill steel slotting ring is closed for one end Structure.
6. Electric mattress inner frame structure according to claim 2, it is characterised in that the space glass fiber rod bottom offers Groove, groove alleviates the overall weight of space glass fiber rod, and space glass fiber rod both sides offer fixing groove, fixing groove and the first glass Fixed strip in drill steel slotting ring is equipped with.
7. Electric mattress inner frame structure according to claim 2, it is characterised in that the all-wing aircraft blade bottom is arranged with Clip, clip is equipped with fixing groove, and all-wing aircraft blade is movably arranged on space glass fiber rod.
CN201710281441.7A 2017-04-26 2017-04-26 A kind of Electric mattress inner frame structure Pending CN106923563A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710281441.7A CN106923563A (en) 2017-04-26 2017-04-26 A kind of Electric mattress inner frame structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710281441.7A CN106923563A (en) 2017-04-26 2017-04-26 A kind of Electric mattress inner frame structure

Publications (1)

Publication Number Publication Date
CN106923563A true CN106923563A (en) 2017-07-07

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ID=59438080

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710281441.7A Pending CN106923563A (en) 2017-04-26 2017-04-26 A kind of Electric mattress inner frame structure

Country Status (1)

Country Link
CN (1) CN106923563A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110584378A (en) * 2019-10-30 2019-12-20 安徽农业大学 Sofa with bamboo shell fragment elastomer
CN110840148A (en) * 2019-12-02 2020-02-28 上海菁筑贸易有限公司 Elastic supporting device for bed frame

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3426570A1 (en) * 1983-11-12 1985-05-30 Huelsta Werke Huels Kg Mattress for a slatted frame
DE20004542U1 (en) * 2000-03-10 2000-09-21 Ahlat, Edith, 42799 Leichlingen Water mattress chamber system with adjustable water mattress frame
CN1447665A (en) * 2000-08-23 2003-10-08 马里奥·皮拉伊诺 Improved mattress
RU2004115075A (en) * 2003-05-19 2005-11-10 Седак-Мекобель С.А. (Be) FOLDING FRAME FOR CHAIR BED
DE102009055782A1 (en) * 2009-03-02 2010-09-23 Thomas Beteiligungs- und Vermögens-GmbH & Co. KG Resting furniture, in particular sleeping or lying furniture
CN202222833U (en) * 2011-09-09 2012-05-23 王剑东 Composite mattress with partitioned spring layer
DE202012008282U1 (en) * 2012-08-30 2012-09-27 Matraflex Gmbh bed
CN104080371A (en) * 2011-11-14 2014-10-01 托马斯投资和财产有限及两合公司 Supporting spring system for a mattress in particular
CN105662008A (en) * 2016-04-13 2016-06-15 天津琴海新材料科技有限公司 Double mattress with separated soft and hard areas
CN205457481U (en) * 2016-02-04 2016-08-17 贺智挺 Spareribs frame with doublestage buffer structure
US9624688B1 (en) * 2015-06-10 2017-04-18 Michael Tyson Inflatable sleeper apparatus

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3426570A1 (en) * 1983-11-12 1985-05-30 Huelsta Werke Huels Kg Mattress for a slatted frame
DE20004542U1 (en) * 2000-03-10 2000-09-21 Ahlat, Edith, 42799 Leichlingen Water mattress chamber system with adjustable water mattress frame
CN1447665A (en) * 2000-08-23 2003-10-08 马里奥·皮拉伊诺 Improved mattress
RU2004115075A (en) * 2003-05-19 2005-11-10 Седак-Мекобель С.А. (Be) FOLDING FRAME FOR CHAIR BED
DE102009055782A1 (en) * 2009-03-02 2010-09-23 Thomas Beteiligungs- und Vermögens-GmbH & Co. KG Resting furniture, in particular sleeping or lying furniture
CN202222833U (en) * 2011-09-09 2012-05-23 王剑东 Composite mattress with partitioned spring layer
CN104080371A (en) * 2011-11-14 2014-10-01 托马斯投资和财产有限及两合公司 Supporting spring system for a mattress in particular
DE202012008282U1 (en) * 2012-08-30 2012-09-27 Matraflex Gmbh bed
US9624688B1 (en) * 2015-06-10 2017-04-18 Michael Tyson Inflatable sleeper apparatus
CN205457481U (en) * 2016-02-04 2016-08-17 贺智挺 Spareribs frame with doublestage buffer structure
CN105662008A (en) * 2016-04-13 2016-06-15 天津琴海新材料科技有限公司 Double mattress with separated soft and hard areas

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腾讯视频: "《德国乐德飞翼》", 《腾讯视频》 *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110584378A (en) * 2019-10-30 2019-12-20 安徽农业大学 Sofa with bamboo shell fragment elastomer
CN110840148A (en) * 2019-12-02 2020-02-28 上海菁筑贸易有限公司 Elastic supporting device for bed frame

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Application publication date: 20170707