CN203623965U - Rotor wing device applied to fixed wing aircraft - Google Patents
Rotor wing device applied to fixed wing aircraft Download PDFInfo
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- CN203623965U CN203623965U CN201320677019.0U CN201320677019U CN203623965U CN 203623965 U CN203623965 U CN 203623965U CN 201320677019 U CN201320677019 U CN 201320677019U CN 203623965 U CN203623965 U CN 203623965U
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- rotor
- blade folder
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Abstract
The utility model provides a rotor wing device applied to a fixed wing aircraft. The rotor wing device concretely comprises a base, a vane clamp, a plurality of vanes arranged on the vane clamp and a rotary device which is connected with the base and the vane clamp.
Description
Technical field
The utility model relates to a kind of rotor device.
Background technology
Rotor craft appears at Europe with the form of a rotor the earliest, belongs to aviette, and load carrying ability is little.It is advantageous that simple in structure, easily manipulation, low cost of manufacture.In addition, cyclogyro also has the advantages such as the required ground run distance of landing is short, and low speed is good, is difficult for stall, and load-carrying ability is strong, and wind loading rating is strong, and therefore safety is higher.The shortcoming of rotor craft is to be difficult to improve flying speed, and the asymmetry that the aircraft rotor of single rotor is rotated also can produce certain anti-twisted moment, affects the stability of aircraft.In prior art, although also there is the aircraft of the bispin wing, two rotor wing rotation opposite directions, for balancing torque, improve the stability of aircraft, still do not solve the technical matters that improves double-rotor aerobat speed.In order to address this problem, someone has proposed to install additional the conception of rotor on the wing of fixed wing aircraft, thereby make aircraft have the advantage of fixed wing aircraft and cyclogyro concurrently, but rotor device of the prior art all can not be applied on fixed wing aircraft, make this conception delay to realize.
Utility model content
In order to solve the problems of the technologies described above, the utility model provides a kind of rotor device being applied on fixed wing aircraft, specifically comprises base, blade folder and is arranged at the some blades on blade folder, also comprises the slewing arrangement that connects base and blade folder.
Further, this slewing arrangement can also comprise the first member and second component, connects between the two by articulated form; Described second component is hinged to be arranged on described base; Described blade folder is arranged on the first member, the entirety structure that is centrosymmetric; Also possess spin motor, described spin motor is arranged on the first member; Also possess the transmission gear being arranged on blade folder, described transmission gear is driven by described spin motor; Described transmission gear is arranged on the first member top.
Owing to having adopted the technical solution of the utility model, this rotor device can be adjusted level angle and the vertical angle of rotor, can also spin, and therefore can be applied on fixed wing aircraft by actv., make it possess the various performances of cyclogyro, therefore possess high practical value.
Accompanying drawing explanation
Fig. 1 is the utility model rotor overall schematic.
Fig. 2 is the schematic diagram of second component 3 views.
Fig. 3 is the schematic diagram of the first member 4.
The specific embodiment
In order to make this novel object, technical scheme and advantage clearer, below in conjunction with drawings and Examples, to this novel being further elaborated.Should be appreciated that specific embodiment described herein is only novel in order to explain this, and this is novel to be not used in restriction.
Disclosed arbitrary feature in this specification sheets (comprising any accessory claim, summary and accompanying drawing), unless narration especially all can be replaced by other equivalences or the alternative features with similar object.,, unless narration especially, each feature is an example in a series of equivalences or similar characteristics.
Embodiment mono-
In order to adjust the flight attitude of aircraft, rotor device of the present utility model is arranged on wing, and should be able to carry out certain rotation with respect to wing, can effectively change like this size at angle windward, realize the increase and decrease speed of aircraft, conversion, climbs and the attitude control such as underriding; Or realize the object that changes lift size, to facilitate landing.Therefore, rotor device of the present utility model comprises base 5, is arranged on the slewing arrangement on base 5, and is arranged on the blade folder on slewing arrangement, and is fixed on the blade on blade folder.Why adopt blade folder, and on blade folder the separate form of stationary blade, be for keep in repair replace convenient.
Embodiment bis-
On the basis of embodiment mono-, as shown in Figure 1, rotor device of the present utility model further comprises the slewing arrangement being arranged on base 5, and is arranged on the blade folder 6 on slewing arrangement.Further, this slewing arrangement comprises the first member 4 and second component 3.Wherein, second component 4 is arranged on base 5, and is arranged on the first member 4 on second component 3, is arranged on the blade folder 6 on the first member 4, and is arranged on the some rotor blades 1 on blade folder 6.
Wherein, base 5 bottoms are for being connected and fixed the wing of wing aircraft.Top possesses the deck of a U-shaped, and deck two sides are respectively equipped with a hinge hole, and two hinge holes are located along the same line, for being connected with second component 3.
As shown in Figure 2, on second component 3, possess the first hinge hole 32, to guarantee that second component 3 can be connected on base 5, and can rotate with respect to base 5 in the vertical directions; In addition, on second component 3, also possesses a pair of the second hinge hole 32, for being connected with the 3rd hinge hole 42 on the first member 4.
As shown in Figure 3, on the first member 4, possesses the 3rd hinge hole 42, for being connected with corresponding hinge hole on second component 3, also possesses the 4th hinge hole 43, be used for connecting spin motor (not shown), on the first member 4, also possess a step surface 41 in addition, for rotary blade folder 6 is installed.The first member 4 can carry out the rotation of horizontal direction with respect to second component 3 by hinged.
Blade folder 6 can possess plural blade joint, but must guarantee the structure that blade folder entirety is centrosymmetric, to make center of gravity be positioned at the center of blade folder as far as possible.
Embodiment tri-
In a preferred embodiment, this rotor device can also possess a spin motor (not shown), and it is arranged on the first member 4, fixing by the 4th hinge hole 43.In this case, need to above the first member 4, arrange one and press from both sides 6 transmission gears that are fixedly connected with 2 with blade, transmission gear 2 drives to be with moving blade folder 6 to rotate by spin motor, thereby realizes the spin of rotor.After rotor device possesses spin function, can help fixed wing aircraft to realize ultra-short takeoff and even take off vertically.
Rotor device of the present utility model, can adjust the level angle of rotor and vertical angle, can spin, and therefore can be applied on fixed wing aircraft by actv., makes it possess the various performances of cyclogyro.
Claims (7)
1. the rotor device being applied on fixed wing aircraft, comprise base, blade presss from both sides and is arranged at the some blades on blade folder, it is characterized in that: also comprise the slewing arrangement that connects base and blade folder, described slewing arrangement comprises the first member and second component, connect by articulated form between the two, above-mentioned base bottom is for connecting the wing of above-mentioned fixed wing aircraft, base top possesses the deck of a U-shaped, deck two sides are respectively equipped with a hinge hole, two hinge holes are located along the same line, for being connected with second component, make second component to carry out the rotation on vertical direction with respect to base, on second component, possesses the first hinge hole, to guarantee that second component can be connected on above-mentioned base, on above-mentioned second component, also possess a pair of the second hinge hole for being connected with the 3rd hinge hole on the first member, the first member can carry out with respect to second component the rotation of horizontal direction by hinged.
2. rotor device as claimed in claim 1, is characterized in that: described second component is hinged to be arranged on described base.
3. rotor device as claimed in claim 1 or 2, is characterized in that: described blade folder is arranged on the first member.
4. rotor device as claimed in claim 3, is characterized in that: also possess spin motor, described spin motor is arranged on the first member.
5. rotor device as claimed in claim 4, is characterized in that: also possess the transmission gear being arranged on blade folder, described transmission gear is driven by described spin motor.
6. rotor device as claimed in claim 5, is characterized in that: described transmission gear is arranged on the first member top.
7. the rotor device as described in one of claim 4-6, is characterized in that: the described blade folder entirety structure that is centrosymmetric.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320677019.0U CN203623965U (en) | 2013-10-31 | 2013-10-31 | Rotor wing device applied to fixed wing aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320677019.0U CN203623965U (en) | 2013-10-31 | 2013-10-31 | Rotor wing device applied to fixed wing aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203623965U true CN203623965U (en) | 2014-06-04 |
Family
ID=50810464
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320677019.0U Expired - Fee Related CN203623965U (en) | 2013-10-31 | 2013-10-31 | Rotor wing device applied to fixed wing aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203623965U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104192305A (en) * | 2014-07-29 | 2014-12-10 | 杭州行之云网络有限公司 | Multi-element wing |
-
2013
- 2013-10-31 CN CN201320677019.0U patent/CN203623965U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104192305A (en) * | 2014-07-29 | 2014-12-10 | 杭州行之云网络有限公司 | Multi-element wing |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20151224 Address after: 610041 Sichuan Province, Chengdu Tianfu Street 69 No. 1 Building 1 unit 16 floor No. 1610 Patentee after: Sichuan nine ancient cooking vessel intelligence intellectual property operation far away Co., Ltd Address before: Nanchang Lu Luo town of Guanghan City, Sichuan province 618307 four Deyang City No. 46 Patentee before: Xia Guishu |
|
| CB03 | Change of inventor or designer information |
Inventor after: Shen Huan Inventor before: Xia Guishu Inventor before: Lu Jing Inventor before: Zhang Quanbin Inventor before: Zhang Yalan Inventor before: Luo Wentian Inventor before: He Mingyu Inventor before: Wang Keren |
|
| TR01 | Transfer of patent right |
Effective date of registration: 20161219 Address after: 518000 Guangdong city of Shenzhen province Nanshan District Taoyuan Street Xueyuan Road No. 1088 South University of science and Technology Science Park N11 Building 1 floor Patentee after: Shenzhen create navigation technology Co., Ltd. Address before: 610041 Sichuan Province, Chengdu Tianfu Street 69 No. 1 Building 1 unit 16 floor No. 1610 Patentee before: Sichuan nine ancient cooking vessel intelligence intellectual property operation far away Co., Ltd |
|
| 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: 20140604 Termination date: 20201031 |