CN211810158U - Underwater aircraft propelled by barrel fan - Google Patents
Underwater aircraft propelled by barrel fan Download PDFInfo
- Publication number
- CN211810158U CN211810158U CN201922235913.2U CN201922235913U CN211810158U CN 211810158 U CN211810158 U CN 211810158U CN 201922235913 U CN201922235913 U CN 201922235913U CN 211810158 U CN211810158 U CN 211810158U
- Authority
- CN
- China
- Prior art keywords
- wing
- fan
- roller
- rotating shaft
- barrel
- 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.)
- Active
Links
Images
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The utility model provides a cylinder fan propelled underwater vehicle, which comprises a body with a built-in power device, wherein the front end of the body is provided with a cabin cover, the two sides in front are respectively provided with cylinder fan wings, the two sides in back are respectively provided with small wings, and the back end is provided with a V-shaped empennage; the wing of the barrel fan is a wing with an arc-shaped groove formed in the wing body, a roller is installed in the groove, the wing of the barrel fan is fixedly connected with the machine body through a wing fixing block and a connection winglet, the roller is connected with a power device in the machine body through a rotating shaft, and the power device drives the roller to rotate around the axis of the rotating shaft through the rotating shaft. The utility model discloses a section of thick bamboo fan wing on the one hand can produce thrust also can produce lift simultaneously, and pneumatic and hydrodynamic performance excellence just do not need unnecessary rudder face for the aircraft structure is simpler, and it is more convenient to manipulate.
Description
Technical Field
The utility model relates to a delivery device under water relates to aircraft, a section of thick bamboo fan wing field under water, specifically is a section of thick bamboo fan propulsive aircraft under water.
Background
An underwater airplane is an airplane capable of diving, is also called a submarine capable of flying, and is a new concept weapon under development, which can hit a target like a submarine under water and can fly like an airplane after rushing out of the water surface. The principle of a traditional underwater airplane is basically similar to that of a submarine. When the underwater airplane is submerged, the valve is opened, a certain amount of water is filled into the water tank of the airplane, and when the gravity of the airplane exceeds the buoyancy, the airplane is submerged. When the airplane needs to float out of the water surface, the airplane floats out of the water surface under the action of buoyancy larger than gravity as long as water in the airplane water tank is discharged. When submerged, the jet engine nacelle of an underwater aircraft is sealed and can be started quickly once it is out of the water. When sailing in water, the ship mainly advances in water by the power of the underwater propulsion device. The pilot can control the airplane to lift and turn in water, so that the airplane can move freely in water. When the lifesaving device meets danger in water, the passengers on the airplane can also carry out water ejection lifesaving.
The principle of underwater aircraft navigating underwater and aircraft flying in the air is similar to some extent, but the challenge of the dual-purpose weapon is still huge, namely the aircraft needs to be as light as possible so as to fly with the least power, and the submarine needs a firm hull to bear water pressure; an airplane heavier than air separates airflow through wings to obtain lift force, and a submarine sucks and discharges water to change buoyancy force.
The wing of the barrel fan is a novel device for generating aerodynamic lift, the rotating fan with the front-mounted wing profile is used for generating vortex lift and thrust to fly, and the wing has the advantages of good low-speed performance, large load, no stall at a large attack angle and the like, and is concerned by relevant organizations and researchers at home and abroad. The fan wing generates lift and consists of two parts: one part is that when the fan rotates, the flow velocity of the upper and lower surfaces of the back half part of the wing is different, so as to cause the pressure difference of the upper and lower surfaces of the wing, and form the lift force of the wing; the other part is that when the fan rotates, a strong eccentric vortex is generated in the fan to generate a strong eccentric vortex low-pressure area, so that the upper surface and the lower surface of the circular arc area of the front half part of the wing generate a large pressure difference to form a larger part of wing lift force, namely the vortex lift force.
The existing underwater vehicle has the following defects: (1) the structure is complex and the weight is large; (2) the oil-consuming engine is adopted to provide power, the weight is large, the transmission mechanism is complex, and an additional liquid oxygen system is required, so that the effective load is reduced.
SUMMERY OF THE UTILITY MODEL
The utility model discloses a solve prior art's problem, provide a section of thick bamboo fan propulsive aircraft under water, section of thick bamboo fan wing can produce thrust on the one hand and also can produce lift simultaneously, and pneumatic and hydrodynamic performance excellence just do not need unnecessary control surface for the aircraft structure is simpler, and it is more convenient to manipulate.
The utility model comprises a body with a built-in power device, wherein the front end of the body is provided with a canopy, the two sides in front are respectively provided with a barrel fan wing, the two sides in rear are respectively provided with a small wing, and the rear end is provided with a V-shaped empennage; the wing of the barrel fan is a wing with an arc-shaped groove formed in the wing body, a roller is installed in the groove, the wing of the barrel fan is fixedly connected with the machine body through a wing fixing block and a connection winglet, the roller is connected with a power device in the machine body through a rotating shaft, and the power device drives the roller to rotate around the axis of the rotating shaft through the rotating shaft.
The improved structure of the cylinder fan wing comprises a plurality of connecting plates, a cylinder is arranged between every two adjacent connecting plates, the cylinder comprises rolling blade fixing plates, fixing plate connecting blocks, connecting plate connecting blocks and rolling blades, wherein the two blade fixing plates fix the plurality of rolling blades into the cylinder, the fixing plate connecting blocks are fixedly connected with the fixing plates, the connecting plate connecting blocks are fixedly connected with the connecting plates, the fixing plate connecting blocks are connected with the connecting plate connecting blocks through rotating shafts, and therefore the cylinder is installed inside a cylinder fan wing channel.
The machine body is made of polymer composite materials, the lithium battery and the power device are arranged inside the machine body, and the machine body is shaped like a shark, has good hydrodynamic performance and air performance, and is beneficial to underwater navigation and air flight. The canopy adopts No. 3 high pressure resistant glass, can guarantee that glass keeps intact under the underwater high pressure. The rolling blade is made of titanium alloy and is suitable for underwater high-pressure working environment.
The utility model has the advantages that:
1. the wing of the cylindrical fan can generate thrust and lift force on the one hand, has excellent pneumatic and hydrodynamic performances and does not need redundant control surfaces, so that the aircraft is simpler in structure and more convenient to operate.
2. The weight of the battery does not change along with the change of the flight time, the flight distance and the flight attitude angle, and the aircraft has better balance stability and maneuverability.
3. The application fields are wide, such as submarine scientific investigation, submarine sightseeing, stealth deepwater attack weapon systems and the like.
4. The novel propeller with the barrel fan wings adopts the motor to provide power, has small noise and strong stealth performance, and does not need an additional liquid oxygen system, so that the effective load is increased.
Drawings
FIG. 1 is an overall view of a sector propelled underwater vehicle.
Fig. 2 is an overall view of a turbofan wing propulsion device.
FIG. 3 is a partial view of a turbofan wing propulsion device.
The numbers in the figures are as follows: the aircraft comprises a canopy 1, a left barrel wing 2, a right barrel wing 3, a connecting winglet 4, a right small wing 5, a left small wing 6, a right small wing flap 7, a left small wing flap 8, a fuselage 9, a V-shaped empennage 10, a barrel wing trailing edge 11, a wing fixing block 12, a rotating shaft 13, rolling blades 14, a connecting plate 15, a rolling blade fixing plate 16, a fixing plate connecting block 17 and a connecting plate connecting block 18.
Detailed Description
The present invention will be further explained with reference to the accompanying drawings.
The utility model discloses the structure is as shown in fig. 1, and its leading features is leading section of thick bamboo fan wing, rearmounted little wing and V type fin overall arrangement, specifically as follows: the aircraft comprises an aircraft body 9 with a built-in power device, wherein a canopy 1 is arranged at the front end of the aircraft body 9, a left side barrel fan wing 2 and a right side barrel fan wing 3 are respectively arranged on the two sides in front, a right side small wing 5 and a left side small wing 6 are respectively arranged on the two sides in rear, and a V-shaped tail wing 10 is arranged at the rear end of the aircraft body 9. The right small wing 5 is provided with a right small wing flap 7, and the left small wing 6 is provided with a left small wing flap 8.
The overall view of the turbofan wing propulsion unit is shown in figure 2. The wing of the cylindrical fan is characterized in that an arc-shaped groove is formed in the wing on the basis of the traditional wing, a rotary roller is arranged in the groove, and each pair of wings of the cylindrical fan consists of three rollers.
The wing of the barrel fan is fixedly connected with a machine body 9 through a wing fixing block 12 and a connecting winglet 4, a roller is connected with a power device in the machine body through a rotating shaft 13, the power device drives the roller to rotate around the axis of the rotating shaft through the rotating shaft 13, and the wing of the barrel fan is provided with a wing trailing edge 11 of the barrel fan.
The fuselage make by polymer composite, lithium cell and power device settle inside the fuselage, the fuselage is imitative shark shape, has good hydrodynamic property and air behavior, is favorable to navigation under water and flight in the air. The canopy adopts No. 3 high pressure resistant glass, can guarantee that glass keeps intact under the underwater high pressure. The rolling blade is made of titanium alloy and is suitable for underwater high-pressure working environment.
The wing of the barrel fan is provided with a plurality of connecting plates 15, and a roller is arranged between every two adjacent connecting plates 15. Fig. 3 is a partial view of a wing propulsion device for a turbofan, which is mainly characterized in that each drum comprises 12 rolling blades 14, and thrust and lift are generated by high-speed rotation of the drum. The roller comprises rolling blade fixing plates 16, fixing plate connecting blocks 17, connecting plate connecting blocks 18 and rolling blades 14, wherein the rolling blades 14 are fixed into the roller by the two blade fixing plates 16, the fixing plate connecting blocks 17 are fixedly connected with the fixing plates 16, the connecting plate connecting blocks 18 are fixedly connected with the connecting plates 15, the fixing plate connecting blocks 17 are connected with the connecting plate connecting blocks 18 through the rotating shafts 13, and therefore the roller is installed inside a wing channel of the fan.
The utility model discloses the aircraft is unanimous at the manipulation mode under water and on water, and section of thick bamboo fan wing provides power and manipulation power for the aircraft, and concrete manipulation process is:
(1) the left barrel fan wing 2 and the right barrel fan wing 3 provide all thrust and partial lift for the delta wing.
(2) The right small wing 5 and the left small wing 6 can provide partial lift.
(3) The change of the motion trail of the aircraft is realized by controlling the lift force and the thrust force of the left barrel fan wing 3 and the right barrel fan wing 1, and the specific way is as follows: simultaneously, the lifting force of the left barrel fan wing 2 and the right barrel fan wing 3 is increased, and the whole machine can generate a head raising or head lowering moment as long as the force of the left barrel fan wing 2 and the force of the right barrel fan wing 3 are kept consistent, so that pitching motion is realized; increasing the lift force of the left barrel fan wing 2, reducing the lift force of the right barrel fan wing 3, generating a clockwise rolling torque, enabling the aircraft to roll clockwise, conversely, reducing the lift force of the left barrel fan wing 2, increasing the lift force of the right barrel fan wing 3, generating an anticlockwise rolling torque, and enabling the aircraft to roll anticlockwise; increasing the thrust of the left barrel fan wing 2 and decreasing the thrust of the right barrel fan wing 3 generates a rightward yawing moment, the aircraft moves in a yawing manner rightward, conversely decreasing the thrust of the left barrel fan wing 2 and increasing the thrust of the right barrel fan wing 3 generates a leftward yawing moment, and the aircraft moves in a yawing manner leftward.
(4) The small wing flap 7 on the right side and the small wing flap 8 on the left side can assist the aircraft in pitching operation. The small wing flap 7 on the right side and the small wing flap 8 on the left side deflect upwards to generate a head-up moment to enable the aircraft to fly upwards, and the small wing flap 7 on the right side and the small wing flap 8 on the left side deflect downwards to generate a head-down moment to enable the aircraft to fly downwards.
The utility model discloses the concrete application way is many, and the above-mentioned only is the preferred embodiment of the utility model, should point out, to ordinary skilled person in this technical field, under the prerequisite that does not deviate from the utility model discloses the principle, can also make a plurality of improvements, and these improvements also should be regarded as the utility model discloses a scope of protection.
Claims (2)
1. A kind of tube fan impels the underwater vehicle, including the fuselage of the built-in power plant, the front end of fuselage has canopy, the anterior both sides have tube fan wings separately, the posterior both sides have small wings separately, the rear end has V-type empennage; the method is characterized in that: the wing of the barrel fan is a wing with an arc-shaped groove formed in the wing body, a roller is installed in the groove, the wing of the barrel fan is fixedly connected with the machine body through a wing fixing block and a connection winglet, the roller is connected with a power device in the machine body through a rotating shaft, and the power device drives the roller to rotate around the axis of the rotating shaft through the rotating shaft.
2. The sector propelled underwater vehicle of claim 1, wherein: the section of thick bamboo fan wing on be provided with a plurality of connecting plates, be provided with the cylinder between the adjacent connecting plate, the cylinder including the blade fixed plate that rolls over, the fixed plate connecting block, connecting plate connecting block and the blade that rolls over, wherein two blade fixed plates are fixed into a cylinder with a plurality of blades that roll over, the fixed plate connecting block links firmly with the fixed plate, the connecting plate connecting block links firmly with the connecting plate, is connected fixed plate connecting block and connecting plate connecting block through the rotation axis to install the cylinder inside section of thick bamboo fan wing channel.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201922235913.2U CN211810158U (en) | 2019-12-13 | 2019-12-13 | Underwater aircraft propelled by barrel fan |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201922235913.2U CN211810158U (en) | 2019-12-13 | 2019-12-13 | Underwater aircraft propelled by barrel fan |
Publications (1)
Publication Number | Publication Date |
---|---|
CN211810158U true CN211810158U (en) | 2020-10-30 |
Family
ID=73139646
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201922235913.2U Active CN211810158U (en) | 2019-12-13 | 2019-12-13 | Underwater aircraft propelled by barrel fan |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN211810158U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113071639A (en) * | 2021-04-20 | 2021-07-06 | 哈尔滨工程大学 | High-speed intelligent underwater vehicle |
-
2019
- 2019-12-13 CN CN201922235913.2U patent/CN211810158U/en active Active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113071639A (en) * | 2021-04-20 | 2021-07-06 | 哈尔滨工程大学 | High-speed intelligent underwater vehicle |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US5242132A (en) | Multi-hulled aircraft/boat | |
US6439148B1 (en) | Low-drag, high-speed ship | |
CN104589938B (en) | A kind of imitative flying fish variable configuration is across medium aircraft | |
CN109229376B (en) | Cross-domain amphibious carrier | |
EP2535261B1 (en) | Paddle wheel yacht | |
CN104589939A (en) | Cross-medium aircraft with changeable shape like sailfish | |
CN110576713A (en) | Air-water submersible triphibian unmanned aerial vehicle | |
CN103640444B (en) | The oblique side amphibious unmanned boat of the binary water surface | |
CN114524091A (en) | Trans-medium aircraft with variable structure | |
CN114394233A (en) | Sea-air amphibious cross-medium bionic aircraft and working method thereof | |
EP0533915A4 (en) | Rotor flap apparatus and method | |
EP3274250B1 (en) | Three stage watercraft | |
CN115303483A (en) | Amphibious rotor unmanned aerial vehicle with blade reuse function and control method thereof | |
CN218786088U (en) | Water-air amphibious cross-medium aircraft | |
CN211810158U (en) | Underwater aircraft propelled by barrel fan | |
CN216581007U (en) | Combined type high-speed amphibious helicopter | |
CN114435044A (en) | Variable cross-medium aircraft | |
CN100592998C (en) | Air-cushion ship based on air stabilizer fin | |
CN1182005C (en) | Effectively power-boosting ground effect aircraft | |
US20080173769A1 (en) | Stabilized tilt rotor aircraft | |
CN117360814A (en) | Variable layout bionic cross-medium unmanned aircraft based on oblique folding wings and method | |
CN117360130A (en) | Cross-medium aircraft and navigation method thereof | |
AU2021104570A4 (en) | Hydrofoil | |
CN201678041U (en) | Circulating flapping-wing flying vehicle | |
CN114013649A (en) | Triphibian cross-medium transverse tilting dual-rotor aircraft |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant |