CN205327409U - Dish form aircraft of adjustable flight gesture - Google Patents
Dish form aircraft of adjustable flight gesture Download PDFInfo
- Publication number
- CN205327409U CN205327409U CN201620129102.8U CN201620129102U CN205327409U CN 205327409 U CN205327409 U CN 205327409U CN 201620129102 U CN201620129102 U CN 201620129102U CN 205327409 U CN205327409 U CN 205327409U
- Authority
- CN
- China
- Prior art keywords
- group
- propeller assembly
- power
- propeller
- power bin
- 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
Landscapes
- Transmission Devices (AREA)
Abstract
Dish form aircraft of adjustable flight gesture, it includes base (1), power bin (2), radome fairing (3), power unit, goes up propeller component (4), down propeller component (5), a set of fixed wing (6), hydraulic power pump (7) and multiunit hydraulic drive's direction adjust pterygoid lamina (8), power bin (2) fixed mounting is on base (1), install on power bin (2) radome fairing (3), power unit includes a set of engine (9), a set ofly go up gear box (10), a set of gear box (11) down, go up screw drive ring gear (12) drives ring gear (13) with screw down, the screw that adopts two -way rotation produces huge lift, sets up the direction adjustment pterygoid lamina that is used for adjustment flight gesture in the both sides of fixed wing simultaneously, and the aerial gesture of dish form aircraft can be convenient carries out the adjustment of slightization, and whole mechanical structure is more firm.
Description
Technical field
This utility model relates to vehicle technology field, is specifically related to the Dished aircraft of adjustable flight attitude。
Background technology
At present, the attention of aircraft industry technical staff increasingly it is subject to about the research of Dished aircraft, but on the market but without a kind of feasible Dished aircraft, number of patent application be 201220126637.1 utility model patent disclose a kind of Dished aircraft, provide the technical scheme of a kind of Dished aircraft, but the overall mechanical structure of this technical scheme is firm not。
Utility model content
The purpose of this utility model is contemplated to solve above-mentioned technical problem, and provides the Dished aircraft of adjustable flight attitude。
This utility model includes base, power bin, trousers, actuating unit, upper propeller assembly, lower propeller assembly, one group of fixing wing, hydro-power pump and the hydraulically powered direction of many groups adjust wing plate, described power bin is fixedly mounted on base, described trousers is arranged on power bin, described actuating unit includes one group of electromotor, one group of upper gear box, one group of lower tooth roller box, upper propeller drives gear ring and lower propeller to drive gear ring, described one group of electromotor annular array respectively is fixedly mounted on the inside of power bin, described one group of upper gear box and one group of lower tooth roller box are separately mounted in power bin, and lay respectively at the both sides up and down of one group of electromotor, and the power intake of one group of upper gear box and one group of lower tooth roller box is connected respectively through the clutch end transmission of power transmission shaft and one group of electromotor, described upper propeller drives gear ring and lower propeller to drive gear ring to be movably arranged on the outer wall of power bin respectively through bearing, and be connected with the clutch end transmission of one group of upper gear box and one group of lower tooth roller box respectively, one end of described upper propeller assembly and lower propeller assembly drives gear ring and lower propeller to drive gear ring to be rigidly connected respectively with upper propeller, the end of described one group of fixing wing is respectively equipped with ball spout, the other end of upper propeller assembly and lower propeller assembly lays respectively at the interior slip of ball spout of one group of fixing wing end, described one group of fixing wing annular array type respectively is fixed on the outer wall of power bin, described hydro-power pump is fixedly mounted in base, described hydraulically powered direction adjustment wing plate of organizing is movably arranged on the both sides up and down of one group of fixing wing respectively, and hydro-power pump drives the action organizing hydraulically powered direction adjustment wing plate more。
The direction of rotation of described upper propeller assembly and lower propeller assembly is contrary, and produces downward airflow thrust。
Described upper propeller assembly is downward-sloping, and lower propeller assembly is inclined upwardly。
The bottom of described base is additionally provided with one group of hydraulic leg。
The helical blade of described upper propeller assembly and lower propeller assembly is additionally provided with the connection ring for connecting blade。
This utility model advantage is: adopt the propeller of bidirectional rotation to produce huge lift, the direction being simultaneously arranged to adjust flight attitude in the both sides of fixing wing adjusts wing plate, the aerial statue of Dished aircraft can carry out the adjustment of granular easily, and overall mechanical structure is more firm。
Accompanying drawing explanation
Fig. 1 is this utility model structural representation。
Fig. 2 is propeller arrangement schematic diagram。
Detailed description of the invention
Such as Fig. 1, shown in 2, this utility model includes base 1, power bin 2, trousers 3, actuating unit, upper propeller assembly 4, lower propeller assembly 5, one group of fixing wing 6, hydro-power pump 7 and the hydraulically powered direction of many groups adjust wing plate 8, described power bin 2 is fixedly mounted on base 1, described trousers 3 is arranged on power bin 2, described actuating unit includes one group of electromotor 9, one group of upper gear box 10, one group of lower tooth roller box 11, upper propeller drives gear ring 12 and lower propeller to drive gear ring 13, described one group of electromotor 9 annular array respectively is fixedly mounted on the inside of power bin 2, described one group of upper gear box 10 and one group of lower tooth roller box 11 are separately mounted in power bin 2, and lay respectively at the both sides up and down of one group of electromotor 9, and the power intake of one group of upper gear box 10 and one group of lower tooth roller box 11 is connected respectively through the clutch end transmission of power transmission shaft and one group of electromotor 9, described upper propeller drives gear ring 12 and lower propeller to drive gear ring 13 to be movably arranged on the outer wall of power bin 2 respectively through bearing, and be connected with the clutch end transmission of one group of upper gear box 10 and one group of lower tooth roller box 11 respectively, one end of described upper propeller assembly 4 and lower propeller assembly 5 drives gear ring 12 and lower propeller to drive gear ring 13 to be rigidly connected respectively with upper propeller, the end of described one group of fixing wing 6 is respectively equipped with ball spout, the other end of upper propeller assembly 4 and lower propeller assembly 5 lays respectively at the interior slip of ball spout of one group of fixing wing 6 end, described one group of fixing wing 6 annular array type respectively is fixed on the outer wall of power bin 2, described hydro-power pump 7 is fixedly mounted in base 1, described hydraulically powered direction adjustment wing plate 8 of organizing is movably arranged on the both sides up and down of one group of fixing wing 6 respectively, and hydro-power pump 7 drives the action organizing hydraulically powered direction adjustment wing plate 8 more。
The direction of rotation of described upper propeller assembly 4 and lower propeller assembly 5 is contrary, and produces downward airflow thrust。
Described upper propeller assembly 4 is downward-sloping, and lower propeller assembly 5 is inclined upwardly。
The bottom of described base 1 is additionally provided with one group of hydraulic leg 14。
The helical blade of described upper propeller assembly 4 and lower propeller assembly 5 is additionally provided with the connection ring 15 for connecting blade。
Working method principle: one group of electromotor 9 starts to upper and lower both direction output power and drives upper propeller to drive gear ring 12 and lower propeller to drive gear ring 13 high speed rotating in the opposite direction respectively through one group of upper gear box 10 and one group of lower tooth roller box 11, thus driving upper propeller assembly 4 and lower propeller assembly 5 counter-rotation, push down on air-flow simultaneously, owing to counteracting force drives aircraft to hoist, aloft during flight, hydro-power pump 7 drives the action organizing hydraulically powered direction adjustment wing plate 8 more, thus the direction of air-flow is produced impact, thus the flight attitude of aircraft is made trickle real-time adjustment。The helical blade of propeller assembly 4 and lower propeller assembly 5 is additionally provided with the connection ring 15 for connecting blade, connect ring 15 and be riveted on the blade of propeller assembly 4 and lower propeller assembly 5, blade is connected into an entirety, considerably increase the rigidity of blade, place airflow thrust excessive time, blade broken or upset。
Claims (5)
1. the Dished aircraft of adjustable flight attitude, it is characterized in that it includes base (1), power bin (2), trousers (3), actuating unit, upper propeller assembly (4), lower propeller assembly (5), one group of fixing wing (6), hydro-power pump (7) and the hydraulically powered direction of many groups adjust wing plate (8), described power bin (2) is fixedly mounted on base (1), described trousers (3) is arranged on power bin (2), described actuating unit includes one group of electromotor (9), one group of upper gear box (10), one group of lower tooth roller box (11), upper propeller drives gear ring (12) and lower propeller to drive gear ring (13), described one group of electromotor (9) annular array respectively is fixedly mounted on the inside of power bin (2), described one group of upper gear box (10) and one group of lower tooth roller box (11) are separately mounted in power bin (2), and lay respectively at the both sides up and down of one group of electromotor (9), and the power intake of one group of upper gear box (10) and one group of lower tooth roller box (11) is connected respectively through the clutch end transmission of power transmission shaft and one group of electromotor (9), described upper propeller drives gear ring (12) and lower propeller to drive gear ring (13) to be movably arranged on the outer wall of power bin (2) respectively through bearing, and be connected with the clutch end transmission of one group of upper gear box (10) and one group of lower tooth roller box (11) respectively, one end of described upper propeller assembly (4) and lower propeller assembly (5) drives gear ring (12) and lower propeller to drive gear ring (13) to be rigidly connected respectively with upper propeller, the end of described one group of fixing wing (6) is respectively equipped with ball spout, the other end of upper propeller assembly (4) and lower propeller assembly (5) lays respectively at the interior slip of ball spout of one group of fixing wing (6) end, described one group of fixing wing (6) annular array type respectively is fixed on the outer wall of power bin (2), described hydro-power pump (7) is fixedly mounted in base (1), described hydraulically powered direction adjustment wing plate (8) of organizing is movably arranged on the both sides up and down of one group of fixing wing (6) respectively, and hydro-power pump (7) drives the action organizing hydraulically powered direction adjustment wing plate (8) more。
2. the Dished aircraft of adjustable flight attitude according to claim 1, it is characterised in that the direction of rotation of described upper propeller assembly (4) and lower propeller assembly (5) is contrary, and produces downward airflow thrust。
3. the Dished aircraft of adjustable flight attitude according to claim 1, it is characterised in that described upper propeller assembly (4) is downward-sloping, and lower propeller assembly (5) is inclined upwardly。
4. the Dished aircraft of adjustable flight attitude according to claim 1, it is characterised in that the bottom of described base (1) is additionally provided with one group of hydraulic leg (14)。
5. the Dished aircraft of adjustable flight attitude according to claim 1, it is characterised in that be additionally provided with the connection ring (15) for connecting blade on the helical blade of described upper propeller assembly (4) and lower propeller assembly (5)。
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620129102.8U CN205327409U (en) | 2016-02-19 | 2016-02-19 | Dish form aircraft of adjustable flight gesture |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620129102.8U CN205327409U (en) | 2016-02-19 | 2016-02-19 | Dish form aircraft of adjustable flight gesture |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205327409U true CN205327409U (en) | 2016-06-22 |
Family
ID=56314185
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620129102.8U Expired - Fee Related CN205327409U (en) | 2016-02-19 | 2016-02-19 | Dish form aircraft of adjustable flight gesture |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205327409U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105752330A (en) * | 2016-02-19 | 2016-07-13 | 张红艳 | Disk-like aircraft capable of adjusting flying attitude |
-
2016
- 2016-02-19 CN CN201620129102.8U patent/CN205327409U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105752330A (en) * | 2016-02-19 | 2016-07-13 | 张红艳 | Disk-like aircraft capable of adjusting flying attitude |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205707301U (en) | A kind of pulp distance varying mechanism | |
| CN204223182U (en) | Civilian depopulated helicopter rotor controls tilting frame actuating device | |
| CN203780797U (en) | Double-motor variable-pitch multi-rotor aircraft | |
| CN203497177U (en) | Five-rotor aircraft capable of changing amplitude | |
| CN104787327B (en) | A kind of multi-rotor aerocraft of changeable wheelbase | |
| CN203767067U (en) | Centre-of-gravity shift yawing device for helicopters | |
| CN103908785B (en) | Multi-rotor aerocraft | |
| CN201793018U (en) | Four-rotor-winged aircraft with retractable fuselage | |
| CN205327409U (en) | Dish form aircraft of adjustable flight gesture | |
| CN105015768A (en) | Multi-rotor aircraft | |
| CN205396540U (en) | Unmanned aerial vehicle screw mechanism of verting | |
| CN103693195A (en) | Miniature aircraft | |
| CN205076038U (en) | Multi -rotor -wing aircraft | |
| CN205076037U (en) | Multi -rotor -wing aircraft | |
| US20240133389A1 (en) | Device and method for converting reciprocating motion into continuous rotation, and application | |
| CN105752330A (en) | Disk-like aircraft capable of adjusting flying attitude | |
| CN206171833U (en) | Solar cell panel receive and releases and posture adjustment device | |
| CN105015769A (en) | Multi-rotor craft | |
| CN106741932A (en) | A kind of axle unmanned plane of mixed type nine based on VTOL | |
| CN102743880A (en) | Disc-shaped aircraft toy | |
| CN208344536U (en) | A kind of DCB Specimen unmanned plane | |
| CN102556342A (en) | Wing combination | |
| CN202557795U (en) | Flying saucer aircraft | |
| CN202609090U (en) | Airplane with multi-purpose engine | |
| CN205060012U (en) | Four -rotor aircraft |
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 |
Granted publication date: 20160622 Termination date: 20210219 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |