CN106428505A - Flying aircraft with jet propeller - Google Patents
Flying aircraft with jet propeller Download PDFInfo
- Publication number
- CN106428505A CN106428505A CN201610998705.6A CN201610998705A CN106428505A CN 106428505 A CN106428505 A CN 106428505A CN 201610998705 A CN201610998705 A CN 201610998705A CN 106428505 A CN106428505 A CN 106428505A
- Authority
- CN
- China
- Prior art keywords
- propeller
- jet
- passenger cabin
- cabin
- flight device
- 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.)
- Pending
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/06—Rigid airships; Semi-rigid airships
- B64B1/36—Arrangement of jet reaction apparatus for propulsion or directional control
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/06—Rigid airships; Semi-rigid airships
- B64B1/24—Arrangement of propulsion plant
- B64B1/30—Arrangement of propellers
- B64B1/34—Arrangement of propellers of lifting propellers
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
The invention discloses a flying aircraft with a jet propeller, and belongs to the field of flying. The aircraft comprises a helium buoyancy lift gasbag and a cabin, wherein the cabin is hoisted below the helium buoyancy lift gasbag by virtue of a traction sling. A battery for electrical equipment, an electric control operation panel and passenger seats are arranged in the cabin, and sightseeing windows are arranged at two sides of the cabin. A propulsion propeller and a rudder for direction control are arranged on the back wall of the cabin, and a propeller motor lead is connected with the battery. The jet propeller is arranged on an outer side wall of the cabin and is arranged on a clamping collar provided with a rotary handle, and the rotary handle is arranged on the inner side wall of the cabin by virtue of a shaft sleeve. A jet motor is arranged in an inner shell duct of the propeller, and is arranged at a position close to an air inlet at the back section of the inner wall of the duct by virtue of a fixed mount. The flying aircraft disclosed by the invention achieves liftoff, forward movement, a high falling speed, a large liftoff range, and a far flying distance of a flying device.
Description
Technical field
The present invention relates to field of floating devices, more particularly to a kind of flight device with jet propeller.
Background technology
At present, with aerial observation scientific research activity or the needs of shooting, recreations, various lift-off apparatus are increasingly
Many, in addition to traditional fire balloon, various flight devices are also born therewith.Disclosed on March 2nd, 2016 State Intellectual Property Office
《A kind of gliding flight device》, publication number CN205059966U, the flight device includes helium buoyance lift air bag 1 and passenger cabin 2,
The both sides of passenger cabin 2 are provided with hang gliding 3, be provided with manpower and step on row actuating device in passenger cabin 2.Although the device saves electric transmission
Part, but hang gliding and manpower step on heavier-weight shared by row actuating device, are unfavorable for lift-off and easily fly in the air.
It is less that the manpower for flying to float steps on row drive power, consumes one's strength very big, and the flight speed that flies to float is also very slow.
Content of the invention
The present invention be directed to being short of power of existing flight device generally existing, the slow problem of gait of march, provide one
The flight device with jet propeller of the flight speed that flies to float kind can be greatly improved.
Technical scheme is as follows：Flight device with jet propeller, the flight device includes helium
Air supporting rises air bag and passenger cabin, and the passenger cabin installed in helium buoyance lift air bag bottom is lifted on helium buoyance lift air bag by drawing lifting rope
Lower section.In described passenger cabin, installation settings has battery, electronic control operating floor and a seat that charger equipment is used, and the two of passenger cabin
Side installation settings has sightseeing window.The rudder of propelling screws and control direction, propeller motor are installed on the rear wall of passenger cabin
Wire is connected with battery.Characterized in that, being provided with jet propeller on passenger cabin lateral wall, the propeller is equipped with
On the cranse of rotating handles, rotating handles is by axle sleeve on cabin interior side wall.Propeller inner shell duct is provided with spray
Pneumatic generator, jet motor is arranged on the back segment of duct inwall near the position of air inlet by fixed mount, and electric bridge is arranged on duct
The leading portion of inwall is near the position of gas outlet, it is also possible to outside propeller inner shell.The battery being connected on passenger cabin base
Wire is connected with jet engine through electric bridge.Angle of rake air outlet can be rotated by operator according to angle of rake airflow direction
To upwards, parallel and down position.After flight device lift-off, when angle of rake air outlet is in down position, propulsion flies
Waving apparatus are gone up to the air upwards；When angle of rake air outlet is in parallel position, propulsion flies to move ahead on waving apparatus horizontal level；When pushing away
Enter the air outlet of device when position upwards, propulsion flies waving apparatus falls downward.
During using the present invention, the helium buoyance lift air bag static line that first will be filled with helium unclamps, and helium buoyance lift air bag drives seat
Cabin is slowly gone up to the air, and when quick liter space-time is needed, by rotating handles, angle of rake air outlet is gone to down position, starts jet
Formula propeller, propulsion flies waving apparatus and quickly goes up to the air upwards；After lift-off to required height, jet propeller is closed, start
Propelling screws propulsion on passenger cabin rear wall flies waving apparatus and slowly moves ahead.As needed rapid flight during moving ahead,
Angle of rake air outlet is gone to parallel postposition, starts jet propeller, propulsion flies waving apparatus and quickly moves ahead.Fast arrival
Predetermined decline spatial domain, when preparing to land, angle of rake air outlet is gone to position upwards, closes propelling screws, start jet
Formula propeller, propulsion flies waving apparatus rapid decrease.When ground is close to, jet propeller is closed, apparatus of the present invention slowly decline
To the predetermined area.Described startup, jet propeller being closed, starts, propelling screws are closed all by being placed in passenger cabin
Electronic control operating floor manipulation realize.
The good effect reached by the present invention is as follows：
1. due to being mounted with jet propeller, it is achieved that winged waving apparatus go up to the air, move ahead, decrease speed fast, scope of going up to the air
Greatly, flying distance is remote.
2. range is wide, vdiverse in function.Aerial scientific experimentss and observation can be carried out using the present invention, can be navigated in the air
Shoot shadow, go sightseeing, air medium advertisement, three-dimensional transport, the large-scale air activity such as celebration, can also carry out agriculture as needed
Industry, the sowing of forestry seed or the sprinkling of chemical fertilizer.
3. energy-saving and environmental protection of the present invention, without the air-polluting fuel such as fuel oil or natural gas.
4. buoyance lift of the present invention flies principle of floaing, compared with the fire balloon using burning gas material, flight safety reliability.
5., after the aircraft lift-off, when ascending air and down current reach dynamic equilibrium, institute can be closed dynamic
System, flight device can be stopped naturally, and airborne period is long.
6. the present invention easily drives, and manipulation is convenient.
Description of the drawings
Fig. 1 is the overall structure diagram of the present invention；
Fig. 2 is jet propeller schematic appearance of the present invention；
Fig. 3 is jet propeller internal structure schematic diagram of the present invention；
Fig. 4 inwardly sees structural representation for jet propeller gas outlet direction.
As shown in the figure：1- helium buoyance lift air bag, 2- draws lifting rope, 3- passenger cabin, 4- jet propeller, 4-1 propeller shell
Body, 4-2 cranse, 4-3 fastening bolt, the anti-foreign body net of 4-4,4-5 power lead, 4-6 air outlet, 4-7 electric bridge, 4-8 impeller blade,
4-9 jet motor, 4-10 duct inwall, 4-11 fixed mount, 5- propelling screws, 6- battery, 7- sightseeing window, 8- axle sleeve, 9- revolves
Handle handss, 10- rudder.
Specific embodiment
The specific embodiment of the present invention combines accompanying drawing and is illustrated.
As Figure 1-Figure 4, the flight device with jet propeller, the flight device includes helium buoyance lift gas
Capsule 1 and passenger cabin 3, the passenger cabin 3 installed in 1 bottom of helium buoyance lift air bag is lifted under helium buoyance lift air bag by drawing lifting rope 2
Side.In described passenger cabin 2, installation settings has the battery 6, electronic control operating floor and seat that charger equipment uses, passenger cabin 3
Both sides installation settings has sightseeing window 8.The rudder 10 of propelling screws 5 and control direction, spiral are installed on the rear wall of passenger cabin
The motor wire of oar 5 is connected with battery 6.Characterized in that, jet propeller 4 is installed on 3 lateral wall of passenger cabin, jet-propelled
Propeller 4 is symmetrically installed on the both sides of passenger cabin 3.The propeller is arranged on the cranse 4-2 equipped with rotating handles 9, rotates handle
Handss 9 are by axle sleeve 8 on cabin interior side wall, and the rotating handles of both sides is coaxially connected, when operator rotates a side grip,
The coaxial servo rotary of opposite side, keeps both sides direction of rotation consistent.Propeller duct inwall 4-10 is provided with jet motor 4-
9, jet motor 4-9 are arranged on the back segment of duct inwall near the position of air inlet by fixed mount 4-11, and electric bridge 4-7 is arranged on
The leading portion of duct inwall is near the position of gas outlet 4-6, it is also possible to installed in the outside of duct housing.It is connected on passenger cabin base
Battery lead 4-5 be connected with jet motor through electric bridge.Anti- foreign body net 4-4 is used for preventing airborne foreign bodies to be sucked into jet propulsion
Device causes the infringement to equipment.Operator can according to angle of rake airflow direction by angle of rake air outlet rotate to upwards,
Parallel and down position.Flight device lift-off after, when angle of rake air outlet is in down position, propulsion fly waving apparatus to
Upper lift-off；When angle of rake air outlet is in parallel position, propulsion flies to move ahead on waving apparatus horizontal level；When angle of rake go out
When air port is in position upwards, propulsion flies waving apparatus falls downward.
Claims (5)
1. the flight device of jet propeller is carried, and the flight device includes helium buoyance lift air bag (1) and passenger cabin (3),
Passenger cabin (3) installed in helium buoyance lift air bag (1) bottom is lifted on the lower section of helium buoyance lift air bag, institute by drawing lifting rope (2)
Battery (6), electronic control operating floor and seat that the interior installation settings of the passenger cabin (2) stated has charger equipment to use, passenger cabin (3)
Both sides installation settings has sightseeing window (8), is provided with the rudder of propelling screws (5) and control direction on the rear wall of passenger cabin
(10), the motor wire of propeller (5) is connected with battery (6), it is characterised in that be provided with jet on passenger cabin (3) lateral wall
Formula propeller (4).
2. the flight device with jet propeller according to claim 1, it is characterised in that described is jet-propelled
Propeller (4) is symmetrically installed on the both sides of passenger cabin (3).
3. the flight device with jet propeller according to claim 1 and 2, it is characterised in that described spray
Gas formula propeller housing is arranged on the cranse (4-2) equipped with rotating handles (9), and rotating handles (9) is arranged on by axle sleeve (8)
On 3 medial wall of passenger cabin, propeller duct inwall (4-10) is provided with jet motor (4-9), jet motor (4-9) is by fixing
Frame (4-11) is arranged on the back segment of duct inwall near the position of air inlet, and electric bridge (4-7) is leaned on installed in the leading portion of duct inwall
The position of nearly gas outlet (4-6), the battery being connected on passenger cabin base (6) wire (4-5) is connected with jet motor through electric bridge.
4. the flight device with jet propeller according to claim 3, it is characterised in that described electric bridge
(4-7) outside of propeller housing may be mounted at.
5. the flight device with jet propeller according to claim 3, it is characterised in that described is arranged on
Rotating handles (9) on the inwall of passenger cabin both sides is coaxially connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610998705.6A CN106428505A (en) | 2016-11-14 | 2016-11-14 | Flying aircraft with jet propeller |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610998705.6A CN106428505A (en) | 2016-11-14 | 2016-11-14 | Flying aircraft with jet propeller |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106428505A true CN106428505A (en) | 2017-02-22 |
Family
ID=58208590
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610998705.6A Pending CN106428505A (en) | 2016-11-14 | 2016-11-14 | Flying aircraft with jet propeller |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106428505A (en) |
Citations (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2034745C1 (en) * | 1992-07-15 | 1995-05-10 | Авиационный научно-технический комплекс "Крыло" | Airship |
| JPH11278390A (en) * | 1998-03-27 | 1999-10-12 | Shunichi Ginya | Improved air ship |
| DE19943051A1 (en) * | 1999-06-12 | 2001-03-15 | Schultz Fademrecht Gerhard | Hot air and similar balloon has a small motor and propeller fitted to a sliding rail around the balloon basket to give a controlled flight direction to augment the effects of wind and buoyancy |
| GB2356184A (en) * | 1999-11-09 | 2001-05-16 | Thomas John Goodey | Lighter-than-air craft using steam to provide buoyancy |
| US20050279880A1 (en) * | 2004-06-18 | 2005-12-22 | Mutsuro Bundo | Multi-purpose airship |
| CN2752175Y (en) * | 2004-12-08 | 2006-01-18 | 李鱼飞 | Man power dynamic light-gas airship |
| CN201143992Y (en) * | 2007-11-02 | 2008-11-05 | 黄刚 | Novel airship |
| CN201354144Y (en) * | 2008-12-03 | 2009-12-02 | 武满吉 | Aeroboat |
| CN201484655U (en) * | 2009-07-31 | 2010-05-26 | 杨克成 | Power flying and floating aircraft |
| CN102602527A (en) * | 2012-03-18 | 2012-07-25 | 西北工业大学 | Near-space unmanned aircraft |
| CN103192977A (en) * | 2013-04-18 | 2013-07-10 | 杨礼诚 | High-speed floating aircraft |
| CN104443343A (en) * | 2014-11-13 | 2015-03-25 | 上海交通大学 | Vectored thruster suspension type flight device |
| CN105015754A (en) * | 2014-04-17 | 2015-11-04 | 杨礼诚 | Flying system moving by natural wind |
| CN205239886U (en) * | 2015-12-21 | 2016-05-18 | 深圳光启空间技术有限公司 | Aerostatics |
| CN105818955A (en) * | 2016-06-06 | 2016-08-03 | 杨礼诚 | Multi-functional flying and floating platform |
| CN205469760U (en) * | 2016-01-11 | 2016-08-17 | 南昌航空大学 | Duct impels four rotor dirigibles of I shape |
| US20160264228A1 (en) * | 2013-03-14 | 2016-09-15 | Raven Industries, Inc. | Airship pitch trim and directional control system |
| CN206155761U (en) * | 2016-11-14 | 2017-05-10 | 杨礼诚 | Aircraft that wafts flies with jetpropeller |
-
2016
- 2016-11-14 CN CN201610998705.6A patent/CN106428505A/en active Pending
Patent Citations (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2034745C1 (en) * | 1992-07-15 | 1995-05-10 | Авиационный научно-технический комплекс "Крыло" | Airship |
| JPH11278390A (en) * | 1998-03-27 | 1999-10-12 | Shunichi Ginya | Improved air ship |
| DE19943051A1 (en) * | 1999-06-12 | 2001-03-15 | Schultz Fademrecht Gerhard | Hot air and similar balloon has a small motor and propeller fitted to a sliding rail around the balloon basket to give a controlled flight direction to augment the effects of wind and buoyancy |
| GB2356184A (en) * | 1999-11-09 | 2001-05-16 | Thomas John Goodey | Lighter-than-air craft using steam to provide buoyancy |
| US20050279880A1 (en) * | 2004-06-18 | 2005-12-22 | Mutsuro Bundo | Multi-purpose airship |
| CN2752175Y (en) * | 2004-12-08 | 2006-01-18 | 李鱼飞 | Man power dynamic light-gas airship |
| CN201143992Y (en) * | 2007-11-02 | 2008-11-05 | 黄刚 | Novel airship |
| CN201354144Y (en) * | 2008-12-03 | 2009-12-02 | 武满吉 | Aeroboat |
| CN201484655U (en) * | 2009-07-31 | 2010-05-26 | 杨克成 | Power flying and floating aircraft |
| CN102602527A (en) * | 2012-03-18 | 2012-07-25 | 西北工业大学 | Near-space unmanned aircraft |
| US20160264228A1 (en) * | 2013-03-14 | 2016-09-15 | Raven Industries, Inc. | Airship pitch trim and directional control system |
| CN103192977A (en) * | 2013-04-18 | 2013-07-10 | 杨礼诚 | High-speed floating aircraft |
| CN105015754A (en) * | 2014-04-17 | 2015-11-04 | 杨礼诚 | Flying system moving by natural wind |
| CN104443343A (en) * | 2014-11-13 | 2015-03-25 | 上海交通大学 | Vectored thruster suspension type flight device |
| CN205239886U (en) * | 2015-12-21 | 2016-05-18 | 深圳光启空间技术有限公司 | Aerostatics |
| CN205469760U (en) * | 2016-01-11 | 2016-08-17 | 南昌航空大学 | Duct impels four rotor dirigibles of I shape |
| CN105818955A (en) * | 2016-06-06 | 2016-08-03 | 杨礼诚 | Multi-functional flying and floating platform |
| CN206155761U (en) * | 2016-11-14 | 2017-05-10 | 杨礼诚 | Aircraft that wafts flies with jetpropeller |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170222 |