CN204674830U - A kind of adjustment direction aircraft - Google Patents
A kind of adjustment direction aircraft Download PDFInfo
- Publication number
- CN204674830U CN204674830U CN201520195915.2U CN201520195915U CN204674830U CN 204674830 U CN204674830 U CN 204674830U CN 201520195915 U CN201520195915 U CN 201520195915U CN 204674830 U CN204674830 U CN 204674830U
- Authority
- CN
- China
- Prior art keywords
- aircraft
- electrical motor
- turning cylinder
- axostylus axostyle
- support
- 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
Links
Abstract
-kind of adjustment direction aircraft, relates to the supporting series of products of aircraft devices---plant the production technical field regulating direction aircraft.Comprise support (1), aircraft (2), axostylus axostyle (3), first electrical motor (4), first turning cylinder (5), rpm governor (6), second electrical motor (7), second turning cylinder (8), fan leaf (9), hole (10), battery supply (11), remote controller (12), described support (1) is provided with aircraft (2), described aircraft (2) outer symmetrical arranges described axostylus axostyle (3), described axostylus axostyle (3) is connected with described first turning cylinder (5) on described first electrical motor (4) or connects through described rpm governor (6), described the first electrical motor (4) is fixed on described support (1), described aircraft (2) inside is provided with described second electrical motor (7), described the second electrical motor (7) is fixed on described aircraft (2) inwall, the upper fixing at least one group of fan leaf (9) of described second turning cylinder (8) of described the second electrical motor (7) one or both ends, reaches production technology simple, easy to operate a kind of use regulating direction aircraft.
Description
Technical field
The utility model relates to the supporting series of products of aircraft devices---plant the production technical field regulating direction aircraft.
Background technology
A kind of regulate direction aircraft to be for the supporting series of products of aircraft, at present, for only needing to and the aircraft of flight forward track, being provided with upwards and being divided into forward two straight-line trajectory power systems, complex manufacturing, complicated operation.
Summary of the invention
The utility model object is for above problem, provides simple, the easy to operate one of production technology and regulates direction aircraft corollary apparatus.
The utility model comprises support 1, aircraft 2, axostylus axostyle 3, first electrical motor 4, first turning cylinder 5, rpm governor 6, second electrical motor 7, second turning cylinder 8, fan leaf 9, hole 10, battery supply 11, remote controller 12, described support 1 is provided with aircraft 2, described aircraft 2 outer symmetrical arranges described axostylus axostyle 3, described axostylus axostyle 3 is connected with described first turning cylinder 5 on described first electrical motor 4 or connects through described rpm governor 6, the first described electrical motor 4 is fixed on described support 1, described aircraft 2 inside is provided with described second electrical motor 7, the second described electrical motor 7 is fixed on described aircraft 2 inwall, described second turning cylinder 8 of the second described electrical motor 7 one or both ends fixes at least one group of fan leaf 9.Due to only by an aircraft 2, by axostylus axostyle 3, under the first electrical motor 4 rotates, adjust aircraft 2 upwards and forward direction, reach a kind of use regulating direction aircraft that production technology is simple, easy to operate.
It is garden cylinder with described hole 10 on both ends open, wall or container that the utility model comprises described aircraft 2.Due on aircraft 2 both ends open, wall with holes 10, reach the use facilitating air to form air flow power.
The utility model comprises the first described electrical motor 4 and the second described electrical motor 7 and to be connected with described battery supply 11 and through described remote controller 12 Push And Release.
The utility model structure is simple novel, reasonable, practical.
Accompanying drawing explanation
The utility model Fig. 1 is a kind of adjustment direction Flight Vehicle Structure schematic diagram.
Detailed description of the invention
As shown in Figure 1, the utility model comprises support 1, aircraft 2, axostylus axostyle 3, first electrical motor 4, first turning cylinder 5, rpm governor 6, second electrical motor 7, second turning cylinder 8, fan leaf 9, hole 10, battery supply 11, remote controller 12, support 1 is provided with aircraft 2, aircraft 2 outer symmetrical arranges axostylus axostyle 3, axostylus axostyle 3 is connected with the first turning cylinder 5 on the first electrical motor 4 or connects through rpm governor 6, first electrical motor 4 is fixed on support 1, aircraft 2 inside is provided with the second electrical motor 7, second electrical motor 7 is fixed on aircraft 2 inwall, second turning cylinder 8 of the second electrical motor 7 one or both ends fixes at least one group of fan leaf 9, aircraft 2 is both ends open, on wall with holes 10 garden cylinder or container.
Claims (3)
1. one kind regulates direction aircraft, it is characterized in that: comprise support (1), aircraft (2), axostylus axostyle (3), first electrical motor (4), first turning cylinder (5), rpm governor (6), second electrical motor (7), second turning cylinder (8), fan leaf (9), hole (10), battery supply (11), remote controller (12), described support (1) is provided with aircraft (2), described aircraft (2) outer symmetrical arranges described axostylus axostyle (3), described axostylus axostyle (3) is connected with described first turning cylinder (5) on described first electrical motor (4) or connects through described rpm governor (6), described the first electrical motor (4) is fixed on described support (1), described aircraft (2) inside is provided with described second electrical motor (7), described the second electrical motor (7) is fixed on described aircraft (2) inwall, the upper fixing at least one group of fan leaf (9) of described second turning cylinder (8) of described the second electrical motor (7) one or both ends.
2. one according to claim 1 regulates direction aircraft, it is characterized in that described aircraft (2) is both ends open, cylinder with described hole (10) on wall or container.
3. one according to claim 1 regulates direction aircraft, it is characterized in that described the first electrical motor (4) and described the second electrical motor (7) are connected with described battery supply (11) and through described remote controller (12) Push And Release.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520195915.2U CN204674830U (en) | 2015-04-02 | 2015-04-02 | A kind of adjustment direction aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520195915.2U CN204674830U (en) | 2015-04-02 | 2015-04-02 | A kind of adjustment direction aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204674830U true CN204674830U (en) | 2015-09-30 |
Family
ID=54174542
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520195915.2U Expired - Fee Related CN204674830U (en) | 2015-04-02 | 2015-04-02 | A kind of adjustment direction aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204674830U (en) |
-
2015
- 2015-04-02 CN CN201520195915.2U patent/CN204674830U/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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150930 Termination date: 20170402 |