CN201989946U - Small-size double-wheel foldable wing airplane - Google Patents
Small-size double-wheel foldable wing airplane Download PDFInfo
- Publication number
- CN201989946U CN201989946U CN2011200939007U CN201120093900U CN201989946U CN 201989946 U CN201989946 U CN 201989946U CN 2011200939007 U CN2011200939007 U CN 2011200939007U CN 201120093900 U CN201120093900 U CN 201120093900U CN 201989946 U CN201989946 U CN 201989946U
- Authority
- CN
- China
- Prior art keywords
- wheel
- wing
- gear
- fuselage
- bracing frame
- 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
Images
Landscapes
- Toys (AREA)
Abstract
The utility model discloses a small-size double-wheel foldable wing airplane, which belongs to aircrafts. Wings arranged at both sides of an airplane body are respectively and horizontally hinged on a wing frame arranged on the top of the airplane body, a foldable oil cylinder connected with the airplane body is arranged on each wing, a support frame is arranged under the wings arranged at both sides, a propeller is arranged on the support frame, both ends of the support frame are hinged with the wings and the airplane body, the lower end of the support frame is provided with a gear linked with the propeller, a front walking wheel and a back walking wheel are arranged under the airplane body, the front wheel is used for driving, and the back wheel is used for guiding. Gear rings are arranged at both sides of the front walking wheel, the gear arranged at the lower end of the support frame is engaged with the gear rings when the wings are in an unfolded state, and the gear arranged at the lower end of the support frame is separated from the gear rings when the wings are in a folded state. The small-size double-wheel foldable wing airplane is small, ingenious and portable, the lifting and landing condition requirements are not high, the maneuverability is good, and the purposes are wide.
Description
Technical field
The utility model belongs to aircraft, particularly a kind of blimp.
Background technology
The blimp type is more, existing proven technique.Can be land and air double-used but also do not have, landing type easily again.
Summary of the invention
The purpose of this utility model is a kind of small-sized two-wheel folding-wing aircraft of design, and it can landing on highway, also can will travel on highway behind the wing-folding.For realizing this purpose, adopted such technical scheme: small-sized two-wheel folding-wing aircraft, be made up of wing, fuselage, road wheel, screw propeller, the wing of fuselage both sides is horizontally hinged respectively on the wing frame at fuselage top, has on the wing and the folding oil cylinder of fuselage bonded assembly.Below the wing of both sides bracing frame is arranged, screw propeller is arranged on the bracing frame.Bracing frame two ends and wing and fuselage are hinged, and there is the gear with the screw propeller interlock bracing frame lower end.Former and later two road wheels are arranged, f-w-d tail wheel guiding under the fuselage.Driving engine is contained on the fuselage, is positioned at operator's saddle below, front walking wheel back, connects front walking wheel by transmission device.There is gear ring the front walking wheel both sides, when wing is in deployed condition, and the gear of wing bracing frame lower end and gear ring engagement.When wing was in folded state, the gear of bracing frame lower end separated with gear ring.
The small volume and less weight of this small-sized two-wheel folding-wing aircraft, the landing conditional request is not high.Manoevreability is good, and is of many uses.
Description of drawings
Fig. 1 is the structural representation of small-sized two-wheel folding-wing aircraft.Fig. 2 is the wing-folding view of small-sized two-wheel folding-wing aircraft.
The specific embodiment
Be further described below in conjunction with accompanying drawing.As shown in Figure 1, small-sized two-wheel folding-wing aircraft is made up of wing, fuselage, road wheel, screw propeller, the wing 2 of fuselage both sides is horizontally hinged respectively on the wing frame 11 at fuselage top, has on the wing and the folding oil cylinder 10 of fuselage bonded assembly, and oil cylinder control wing is in and launches or the folding position.Bracing frame 3 is arranged below the wing, screw propeller 1 is arranged on the bracing frame.Bracing frame two ends and wing and fuselage are hinged, and there is the gear 5 with 4 interlocks of screw propeller power wheel the bracing frame lower end, by this gear power is reached screw propeller.Former and later two road wheels are arranged under the fuselage, and front-wheel 7 is a drive wheel, and tail wheel 9 is a track adjusting wheel.Driving engine 8 is contained on the fuselage, is positioned at the front walking wheel back, and the operator's saddle below connects front walking wheel by transmission device.There is gear ring 6 the front walking wheel two sides, and when wing was in deployed condition, the gear 5 of bracing frame lower end and gear ring 6 engagements drove the screw propeller rotation.When wing during at folded state, body narrows down, and the gear of bracing frame lower end separates with gear ring, and aircraft can travel on highway.
Claims (2)
1. small-sized two-wheel folding-wing aircraft is made up of wing, fuselage, road wheel, screw propeller, it is characterized in that: the wing of fuselage both sides (2) is horizontally hinged respectively on the wing frame (11) at fuselage top, has on the wing and the folding oil cylinder (10) of fuselage bonded assembly; Bracing frame (3) is arranged below the wing of both sides, screw propeller (1) is arranged on the bracing frame; Bracing frame two ends and wing and fuselage are hinged, and there is the gear (5) with the interlock of screw propeller power wheel the bracing frame lower end, and gear (5) is connected with power; Former and later two road wheels are arranged under the fuselage, and front-wheel (7) is a drive wheel, and tail wheel (9) is a track adjusting wheel; Driving engine (8) is contained on the fuselage, is positioned at operator's saddle below, front walking wheel back, connects front walking wheel by transmission device.
2. small-sized two-wheel folding-wing aircraft as claimed in claim 1 is characterized in that: there is gear ring (6) front-wheel (7) both sides, when wing is in deployed condition, and gear of bracing frame lower end (5) and gear ring engagement; When wing was in folded state, the gear of bracing frame lower end separated with gear ring.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011200939007U CN201989946U (en) | 2011-04-02 | 2011-04-02 | Small-size double-wheel foldable wing airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011200939007U CN201989946U (en) | 2011-04-02 | 2011-04-02 | Small-size double-wheel foldable wing airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201989946U true CN201989946U (en) | 2011-09-28 |
Family
ID=44666444
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011200939007U Expired - Fee Related CN201989946U (en) | 2011-04-02 | 2011-04-02 | Small-size double-wheel foldable wing airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201989946U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104354851A (en) * | 2014-10-20 | 2015-02-18 | 中国科学院力学研究所 | High-speed aircraft with foldable upper wing |
| WO2015101346A1 (en) * | 2014-01-05 | 2015-07-09 | 曹乃承 | Aircraft and method for converting aircraft structure form during flight |
| CN107521662A (en) * | 2017-08-31 | 2017-12-29 | 佛山市龙远科技有限公司 | A kind of folding individual layer wing aircraft of wing |
| CN107554785A (en) * | 2017-08-19 | 2018-01-09 | 中国矿业大学 | The morphing aircraft control system and method that mine is detected after a kind of calamity |
-
2011
- 2011-04-02 CN CN2011200939007U patent/CN201989946U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2015101346A1 (en) * | 2014-01-05 | 2015-07-09 | 曹乃承 | Aircraft and method for converting aircraft structure form during flight |
| CN104354851A (en) * | 2014-10-20 | 2015-02-18 | 中国科学院力学研究所 | High-speed aircraft with foldable upper wing |
| CN107554785A (en) * | 2017-08-19 | 2018-01-09 | 中国矿业大学 | The morphing aircraft control system and method that mine is detected after a kind of calamity |
| CN107521662A (en) * | 2017-08-31 | 2017-12-29 | 佛山市龙远科技有限公司 | A kind of folding individual layer wing aircraft of wing |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN101885295A (en) | Land and air double-used aircraft | |
| US9505282B2 (en) | Amphibious flying car | |
| CN204915162U (en) | Navy, army and air force four -axis binary vehicle | |
| CN107757273B (en) | Flying automobile | |
| BG111231A (en) | Road aircraft | |
| NZ592991A (en) | Aircraft system that enables ground traveling | |
| CN201989946U (en) | Small-size double-wheel foldable wing airplane | |
| CN105438444A (en) | Deformable wings and vertical take-off and landing aircraft using wings | |
| CN211195749U (en) | Tilt shaftless duct rotor aerocar | |
| CN102673780A (en) | Double-configuration aircraft | |
| CN103522858A (en) | Flying passenger car | |
| CN201525255U (en) | Gyroplane landing ship capable of driving on land and water | |
| CN108177491A (en) | One kind can vertical take-off and landing flying car | |
| CN103171388B (en) | Vertical lifting land-air dual-purpose vehicle | |
| CN104260873B (en) | A kind of delta-wing aircraft | |
| CN112319160A (en) | Single-layer-propeller electric flying motorcycle capable of rapidly switching ground-air state during traveling | |
| CN201692643U (en) | Airphibian aircraft | |
| CN203698647U (en) | Low-wind-resistance and high-balance light flying wing type unmanned aerial vehicle | |
| CN203958603U (en) | A kind of aerial survey unmanned plane | |
| CN104149565A (en) | Air and ground dual-purpose multifunctional trolley | |
| CN110371286A (en) | A kind of manned vehicle | |
| CN102632993A (en) | Series-parallel tilting drive mechanism of tilt rotor aircraft | |
| CN201729037U (en) | Airphibious aircraft | |
| CN205632001U (en) | Triphibian aircraft | |
| CN202896879U (en) | Light concentric shaft helicopter |
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: 20110928 Termination date: 20120402 |