CN2803136Y - Wing device set on winging bed - Google Patents
Wing device set on winging bed Download PDFInfo
- Publication number
- CN2803136Y CN2803136Y CN 200420103213 CN200420103213U CN2803136Y CN 2803136 Y CN2803136 Y CN 2803136Y CN 200420103213 CN200420103213 CN 200420103213 CN 200420103213 U CN200420103213 U CN 200420103213U CN 2803136 Y CN2803136 Y CN 2803136Y
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- CN
- China
- Prior art keywords
- wing aircraft
- wing
- blade
- flying
- flying wing
- 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.)
- Expired - Fee Related
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Abstract
The utility model relates to a flying wing device arranged on a flying wing bed. The utility model is composed of flying wing blades, a rotating ball, a TPE elastic body and a fixing seat, wherein the center of each flying wing blade is provided with a central hole, the center of the fixing seat is provided with a protruding casing pipe of which the top end is provided with a clamping edge, the rotating ball is composed of a ball body and a connecting head on which a groove is arranged, the top end of the groove is provided with a clamping edge, the ball body of the rotating ball is clamped by the clamping edge of the casing pipe arranged on the fixing seat, the connecting head of the rotating ball passes through the central hole of each flying wing blade, the clamping edge arranged on the connecting head is clamped at the end of the central hole and the cylindrical hollow TPE elastic body which is arranged between the fixing seat and each flying wing blade is sheathed at the periphery of the casing pipe of the fixing seat. The utility model has the advantages that the flying wing blades have elasticity under strong gravity so as to decrease pressure applied on a human body and to alleviate local harm to a human body, the rotating ball alleviates the bearing force of part of a body and the TPE elastic body alleviates pressure applied on a human body at the sleeping time.
Description
Technical field
The utility model relates to the all-wing aircraft bed, more particularly relates to be arranged on the flying-wing device on the all-wing aircraft bed.
Background technology
Present existing beddo all is to contact with human body by face, and its weak point is that permeability is poor, and does not alleviate the function of body part bearing capacity.
Summary of the invention
The purpose of this utility model is the weak point that solves in the above-mentioned technology, and a kind of flying-wing device that is arranged on the all-wing aircraft bed is provided.
The purpose of this utility model is achieved by following technical proposals:
The utility model is by the all-wing aircraft blade, roating sphere, the TPE elastomer, holder is formed, the central authorities of described all-wing aircraft blade are provided with centre bore, holder central authorities are provided with an outstanding sleeve pipe, cannula tip is provided with edge, described roating sphere is by spheroid, connector is formed, connector is provided with groove, the top is provided with edge, the be fixed edge of the sleeve pipe on the seat of the spheroid of roating sphere blocks, centre bore and the edge on the connector that the connector of roating sphere passes the all-wing aircraft blade are stuck in the center nose end, described TPE elastomer is located between holder and the all-wing aircraft blade, and the TPE elastomer becomes cylindrical shape and hollow, by the sleeve pipe periphery of hollow sleeve at holder.
All-wing aircraft blade centre is provided with a lid, and lid is provided with card, and the all-wing aircraft blade is provided with bayonet socket, and card is stuck in the bayonet socket; The blade of all-wing aircraft blade becomes butterfly-like shape; Groove on the connector of roating sphere evenly distributes; Groove on the connector is 3; Groove on the connector also can be 4; The elastomeric outer surface waviness of TPE shape.
The utility model has following beneficial effect compared to existing technology:
The all-wing aircraft blade is designed to butterfly-like shape, and is attractive in appearance; Change traditional face contact for the some contact, have the high ventilation performance, flexible under strong gravity, can slow down pressure to human body, alleviate localized injury to human body;
Roating sphere changes all-wing aircraft direction blade and angle according to the difference of people's sleeping posture, alleviates the bearing capacity of body part;
The TPU elastomer has elasticity preferably, alleviates the pressure to human body during sleep;
Holder is fixed on whole all-wing aircraft on the batten of bed;
Lid plays decoration function.
Description of drawings
Fig. 1 is a vertical view of the present utility model;
Fig. 2 is along the cutaway view of A-A among Fig. 1;
Fig. 3 is along the cutaway view of B-B among Fig. 1.
The specific embodiment
To closing accompanying drawing the utility model is further described below:
With reference to Fig. 1-3, the utility model is by all-wing aircraft blade 1, roating sphere 2, TPE elastomer 3, holder 4, lid 11 is formed, the blade of described all-wing aircraft blade 1 is designed to butterfly-like shape, the central authorities of all-wing aircraft blade 1 are provided with centre bore, holder 4 central authorities are provided with an outstanding sleeve pipe 5, sleeve pipe 5 tops are provided with edge 6, described roating sphere 2 is by spheroid 7, connector 8 is formed, connector 8 has retractility, connector 8 is provided with equally distributed 3 grooves 9, the top is provided with edge 10, and the be fixed edge 6 of the sleeve pipe 5 of seat on 4 of the spheroid 7 of roating sphere 2 blocks, and the connector 8 of roating sphere 2 passes the centre bore of all-wing aircraft blade 1 and the edge 10 on the connector 8 is stuck in the center nose end, described TPE elastomer 3 is located between holder 4 and the all-wing aircraft blade 1,3 one-tenth cylindrical shapes of TPE elastomer and hollow are by sleeve pipe 5 peripheries of hollow sleeve at holder 4, the external surface waviness shape of TPE elastomer 3, all-wing aircraft blade 1 centre is provided with lid 11, lid 11 is provided with card 12, and all-wing aircraft blade 1 is provided with bayonet socket, and card 12 is stuck in the bayonet socket.
Claims (7)
1. be arranged on the flying-wing device on the all-wing aircraft bed, it is characterized in that by all-wing aircraft blade (1), roating sphere (2), TPE elastomer (3), holder (4) is formed, the central authorities of described all-wing aircraft blade (1) are provided with centre bore, holder (4) central authorities are provided with an outstanding sleeve pipe (5), sleeve pipe (5) top is provided with edge (6), described roating sphere (2) is by spheroid (7), connector (8) is formed, connector (8) is provided with groove (9), the top is provided with edge (10), the be fixed edge (6) of the sleeve pipe (5) of seat on (4) of the spheroid (7) of roating sphere (2) blocks, the connector (8) of roating sphere (2) passes the centre bore of all-wing aircraft blade (1) and the edge (10) on the connector (8) is stuck in the center nose end, described TPE elastomer (3) is located between holder (4) and the all-wing aircraft blade (1), TPE elastomer (3) becomes cylindrical shape and hollow, by sleeve pipe (5) periphery of hollow sleeve in holder (4).
2. the flying-wing device that is arranged on the all-wing aircraft bed according to claim 1 is characterized in that all-wing aircraft blade (1) centre is provided with a lid (11), and lid (11) is provided with card (12), and all-wing aircraft blade (1) is provided with bayonet socket, and card (12) is stuck in the bayonet socket.
3. the flying-wing device that is arranged on the all-wing aircraft bed according to claim 1 is characterized in that the blade of all-wing aircraft blade (1) becomes butterfly-like shape.
4. the flying-wing device that is arranged on the all-wing aircraft bed according to claim 1 is characterized in that the groove (9) on the connector (8) of roating sphere (2) evenly distributes.
5. the flying-wing device that is arranged on the all-wing aircraft bed according to claim 4 is characterized in that groove (9) is 3.
6. the flying-wing device that is arranged on the all-wing aircraft bed according to claim 4 is characterized in that groove (9) is 4.
7. the flying-wing device that is arranged on the all-wing aircraft bed according to claim 1 is characterized in that the outer surface waviness shape of TPE elastomer (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200420103213 CN2803136Y (en) | 2004-12-30 | 2004-12-30 | Wing device set on winging bed |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200420103213 CN2803136Y (en) | 2004-12-30 | 2004-12-30 | Wing device set on winging bed |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2803136Y true CN2803136Y (en) | 2006-08-09 |
Family
ID=36908440
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200420103213 Expired - Fee Related CN2803136Y (en) | 2004-12-30 | 2004-12-30 | Wing device set on winging bed |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2803136Y (en) |
-
2004
- 2004-12-30 CN CN 200420103213 patent/CN2803136Y/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20060809 Termination date: 20101230 |