CN2605494Y - Infrared single-hole range wind-plate - Google Patents
Infrared single-hole range wind-plate Download PDFInfo
- Publication number
- CN2605494Y CN2605494Y CN 03212263 CN03212263U CN2605494Y CN 2605494 Y CN2605494 Y CN 2605494Y CN 03212263 CN03212263 CN 03212263 CN 03212263 U CN03212263 U CN 03212263U CN 2605494 Y CN2605494 Y CN 2605494Y
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- CN
- China
- Prior art keywords
- aerofoil
- bottom line
- plate
- hypotenuse
- narrow end
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Abstract
Disclosed is an air plate for infrared single eye range, which relates to an improvement of the air plate structure for an infrared single eye gas range and comprises a single eye range (1) and an air plate (2), wherein the air plate (2) is a trapezoid; the wide end (5) of the air plate (2) is fixed to front side of the upper surface plate (8) of the single eye range (1); bottom line (4) of the narrow end (9) of the air plate (2) is a folded edge; the air plate (2) at the lower end of the folded edge has a fixedly connected air hole plate (3); the air hole plate (3) is provided with an air hole (6), which communicates with air inlet of the single eye range (1); the inclined edges (7) of the air plate (2) at two ends of the bottom line of the narrow end (9) of the air plate (2) are symmetrically arranged; an angle apha of 92 to 160 degrees is formed between each incline edge (7) and bottom line (4) of the narrow end (9) of the trapezoid air plate (2). The utility model has the advantages of simple and smooth structure, small size, eye-pleasing appearance, light weight as well as low cost.
Description
Technical field: the utility model relates to the improvement of the simple eye kitchen range aerofoil of gas-fired infrared structure.
Background technology: the broad that the aerofoil of existing infrared ray single-hole range is all made, both wasted material, increased the weight and the cost of kitchen range again, nor attractive in appearance.
The utility model content: the purpose of this utility model is the aerofoil of a kind of infrared ray single-hole range of development, and it should have smoothness simple in structure, volume is small and exquisite, specious, in light weight, cost is low advantage.The utility model is made up of single-hole range 1, aerofoil 2, aerofoil 2 is trapezoidal, the wide end 5 of aerofoil 2 is fixed on the front side of single-hole range 1 top panel 8, bottom line 4 places of aerofoil 2 narrow ends 9 are flangings, connect intrinsic wind orifice plate 3 on the aerofoil 2 of flanging lower end, have wind hole 6 on the wind orifice plate 3, wind hole 6 is connected with the air inlet of single-hole range 1, the hypotenuse 7 of the bottom line 4 two ends aerofoils 2 of trapezoidal aerofoil 2 narrow ends 9 is symmetrical arranged, and the bottom line 4 of trapezoidal aerofoil 2 narrow ends 9 is 92 °～160 ° with the angle [alpha] of hypotenuse 7.The utlity model has smoothness simple in structure, volume is small and exquisite, specious, in light weight, cost is low advantage.
Description of drawings: Fig. 1 is an overall structure schematic diagram of the present utility model, and Fig. 2 is the structural representation of the specific embodiment two.
The specific embodiment one: present embodiment is made up of single-hole range 1, aerofoil 2, aerofoil 2 is trapezoidal, the wide end 5 of aerofoil 2 is fixed on the front side of square panel 8 on the single-hole range 1, bottom line 4 places of aerofoil 2 narrow ends 9 are flangings, connect intrinsic wind orifice plate 3 on the aerofoil 2 of flanging lower end, have wind hole 6 on the wind orifice plate 3, wind hole 6 is connected with the air inlet of single-hole range 1, the hypotenuse 7 of the bottom line 4 two ends aerofoils 2 of trapezoidal aerofoil 2 narrow ends 9 is symmetrical arranged, and the bottom line 4 of trapezoidal aerofoil 2 narrow ends 9 is 92 °～160 ° with the angle [alpha] of hypotenuse 7.
The specific embodiment two: the difference of the present embodiment and the specific embodiment one is that the panel 8 on the single-hole range 1 is circular, and the wide end 5 of trapezoidal aerofoil 2 is a circular arc.Other composition is identical with the specific embodiment one with annexation.
The specific embodiment three: in the present embodiment, the bottom line 4 of trapezoidal aerofoil 2 narrow ends 9 is 92 °～99 ° with the angle [alpha] of hypotenuse 7.
The specific embodiment four: in the present embodiment, the bottom line 4 of trapezoidal aerofoil 2 narrow ends 9 is 100 °～107 ° with the angle [alpha] of hypotenuse 7.
The specific embodiment five: in the present embodiment, the bottom line 4 of trapezoidal aerofoil 2 narrow ends 9 is 108 °～115 ° with the angle [alpha] of hypotenuse 7.
The specific embodiment six: in the present embodiment, the bottom line 4 of trapezoidal aerofoil 2 narrow ends 9 is 116 °～123 ° with the angle [alpha] of hypotenuse 7.
The specific embodiment seven: in the present embodiment, the bottom line 4 of trapezoidal aerofoil 2 narrow ends 9 is 124 °～131 ° with the angle [alpha] of hypotenuse 7.
The specific embodiment eight: in the present embodiment, the bottom line 4 of trapezoidal aerofoil 2 narrow ends 9 is 132 °～139 ° with the angle [alpha] of hypotenuse 7.
The specific embodiment nine: in the present embodiment, the bottom line 4 of trapezoidal aerofoil 2 narrow ends 9 is 140 °～147 ° with the angle [alpha] of hypotenuse 7.
The specific embodiment ten: in the present embodiment, the bottom line 4 of trapezoidal aerofoil 2 narrow ends 9 is 148 °～155 ° with the angle [alpha] of hypotenuse 7.
The specific embodiment 11: in the present embodiment, the bottom line 4 of trapezoidal aerofoil 2 narrow ends 9 is 156 °～160 ° with the angle [alpha] of hypotenuse 7.
Claims (10)
1, the aerofoil of infrared ray single-hole range, it is by single-hole range (1), aerofoil (2) is formed, aerofoil (2) is trapezoidal, the wide end (5) of aerofoil (2) is fixed on the front side of single-hole range (1) top panel (8), it is flanging that the bottom line (4) of the narrow end of aerofoil (2) (9) is located, connect intrinsic wind orifice plate (3) on the aerofoil of flanging lower end (2), have wind hole (6) on the wind orifice plate (3), wind hole (6) is connected with the air inlet of single-hole range (1), the hypotenuse (7) of the bottom line two ends aerofoils (2) of the narrow end of trapezoidal aerofoil (2) (9) is symmetrical arranged, and it is characterized in that the bottom line (4) of the narrow end of trapezoidal aerofoil (2) (9) and the angle [alpha] of hypotenuse (7) are 92 °～160 °.
2, the aerofoil of infrared ray single-hole range according to claim 1 is characterized in that the bottom line (4) of the narrow end of described trapezoidal aerofoil (2) (9) and the angle [alpha] of hypotenuse (7) are 92 °～99 °.
3, the aerofoil of infrared ray single-hole range according to claim 1 is characterized in that the bottom line (4) of the narrow end of described trapezoidal aerofoil (2) (9) and the angle [alpha] of hypotenuse (7) are 100 °～107 °.
4, the aerofoil of infrared ray single-hole range according to claim 1 is characterized in that the bottom line (4) of the narrow end of described trapezoidal aerofoil (2) (9) and the angle [alpha] of hypotenuse (7) are 108 °～115 °.
5, the aerofoil of infrared ray single-hole range according to claim 1 is characterized in that the bottom line (4) of the narrow end of described trapezoidal aerofoil (2) (9) and the angle [alpha] of hypotenuse (7) are 116 °～123 °.
6, the aerofoil of infrared ray single-hole range according to claim 1 is characterized in that the bottom line (4) of the narrow end of described trapezoidal aerofoil (2) (9) and the angle [alpha] of hypotenuse (7) are 124 °～131 °.
7, the aerofoil of infrared ray single-hole range according to claim 1 is characterized in that the bottom line (4) of the narrow end of described trapezoidal aerofoil (2) (9) and the angle [alpha] of hypotenuse (7) are 132 °～139 °.
8, the aerofoil of infrared ray single-hole range according to claim 1 is characterized in that the bottom line (4) of the narrow end of described trapezoidal aerofoil (2) (9) and the angle [alpha] of hypotenuse (7) are 140 °～147 °.
9, the aerofoil of infrared ray single-hole range according to claim 1 is characterized in that the bottom line (4) of the narrow end of described trapezoidal aerofoil (2) (9) and the angle [alpha] of hypotenuse (7) are 148 °～155 °.
10, the aerofoil of infrared ray single-hole range according to claim 1 is characterized in that the bottom line (4) of the narrow end of described trapezoidal aerofoil (2) (9) and the angle [alpha] of hypotenuse (7) are 156 °～160 °.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 03212263 CN2605494Y (en) | 2003-03-28 | 2003-03-28 | Infrared single-hole range wind-plate |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 03212263 CN2605494Y (en) | 2003-03-28 | 2003-03-28 | Infrared single-hole range wind-plate |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2605494Y true CN2605494Y (en) | 2004-03-03 |
Family
ID=34159433
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 03212263 Expired - Fee Related CN2605494Y (en) | 2003-03-28 | 2003-03-28 | Infrared single-hole range wind-plate |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2605494Y (en) |
-
2003
- 2003-03-28 CN CN 03212263 patent/CN2605494Y/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 | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |