CN109269363B - Single-soldier hand-throwing type fly-round missile with flying wing layout - Google Patents
Single-soldier hand-throwing type fly-round missile with flying wing layout Download PDFInfo
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- CN109269363B CN109269363B CN201811362575.2A CN201811362575A CN109269363B CN 109269363 B CN109269363 B CN 109269363B CN 201811362575 A CN201811362575 A CN 201811362575A CN 109269363 B CN109269363 B CN 109269363B
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- 230000007246 mechanism Effects 0.000 claims abstract description 31
- 239000003381 stabilizer Substances 0.000 claims abstract description 15
- 230000005540 biological transmission Effects 0.000 claims abstract description 12
- 229920001971 elastomer Polymers 0.000 claims description 9
- 239000000806 elastomer Substances 0.000 claims description 9
- 238000013461 design Methods 0.000 claims description 4
- 239000000463 material Substances 0.000 claims description 4
- 239000002121 nanofiber Substances 0.000 claims description 4
- 238000001746 injection moulding Methods 0.000 claims description 3
- 240000002836 Ipomoea tricolor Species 0.000 claims 1
- 230000036632 reaction speed Effects 0.000 abstract description 2
- 230000008901 benefit Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000011156 evaluation Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 238000012876 topography Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The invention discloses an individual soldier hand-thrown type fly-round missile with an all-wing layout, which is formed by assembling a front missile body section and a rear missile body section, wherein the front missile body section comprises a guide head, a fighter part and a first quick lock mechanism, the first quick lock mechanism is positioned at the tail end of the front missile body section and is distributed with a first signal contact, the rear missile body section comprises a fuselage, wings, a propelling device, vertical stabilizers, a second quick lock mechanism, a self-driving instrument, a data transmission, a battery and a picture transmission, the wings are arranged on two sides of the fuselage, the propelling device is positioned at the front wing, a pair of vertical stabilizers are arranged on the side edges of the wings, the second quick lock mechanism is positioned at the front fuselage section and is distributed with a second signal contact, the first quick lock mechanism and the second quick lock mechanism are quickly engaged through a lock catch, and the self-driving instrument is communicated with the front missile body section through the first signal contact and the second signal contact. The fly-patrol projectile can realize the vertical take-off by hand throwing and by means of the support of the vertical stabilizer, improves the individual combat efficiency and combat flexibility, and improves the combat reaction speed.
Description
Technical Field
The invention relates to a fly-round missile, in particular to a fly-round missile which is arranged on an all-wing aircraft and is thrown by a single hand.
Background
The patrol projectile is ammunition which can carry out patrol flight in a target area by utilizing the existing weapon throwing, can bear single or multiple tasks such as monitoring, investigation, fight damage evaluation, aerial wireless relay, target attack and the like, and is also an important trend of future ammunition development. The fly-round projectile has long range and multiple functions, and has long air standby time when performing tasks such as reconnaissance, positioning, indication, information relay, damage, evaluation and the like. The use in battlefield will greatly improve the action and position of weapon system, improve the striking ability and accuracy of weapon system to target, reduce unnecessary logistic burden. In addition, the ability of combat forces to work in a variety of combat situations can be greatly expanded, such as: the fly-round projectile cruises through flying in the air, so that the traditional ammunition striking range can be improved; high-precision striking is realized through accurate guidance; the striking under the reverse inclined plane and complex environment is realized through high maneuvering control.
The existing fly-patrol projectile generally adopts modes of shooting (such as American LAM fly-patrol attack ammunition), airborne throwing (such as American "air master"), individual throwing (such as American "spring knife"), and the like, and has high dependence on accessories of a launching system. The fly-patrol projectile thrown by the individual soldier is limited by weight and launching speed, and is launched by adopting a launching tube basically, so that the fly-patrol projectile is large in volume and weight and not easy to carry. Meanwhile, the transmitting cylinder has higher requirements on ground support, and adverse effects are brought to the flexibility and quick response of individual combat.
Disclosure of Invention
Aiming at the problems in the prior art, the invention provides the single-soldier hand-thrown type fly-round projectile which is convenient to carry, fast to assemble and throw by hand.
The technical scheme adopted by the invention is as follows: the utility model provides an individual soldier's hand throwing formula of flying wing overall arrangement patrols flying projectile, is assembled by projectile front segment and projectile back segment and forms, the projectile front segment includes guide head, fight portion, first quick lock mechanism, and the guide head is located the top of projectile front segment, and fight portion and guide head direct link to each other are located the middle part of projectile front segment, and first quick lock mechanism is located the end of projectile front segment, and it has first signal contact to distribute on the first quick lock mechanism, the projectile back segment includes fuselage, wing, advancing device, vertical stabilizer, second quick lock mechanism, self-driving appearance, data transmission, battery, picture transmission, and the wing sets up in fuselage both sides, and advancing device is located wing front end and is close to fuselage third department, and control the rudder face for a set of, respectively is equipped with a pair of vertical stabilizer at the edge of left and right wings, and vertical stabilizer is the upper and lower symmetrical structure, wholly is the arrow-shaped, self-driving appearance, data transmission, battery, picture transmission are installed in inside, and second quick lock mechanism is located the fuselage front end, and second signal contact has on the second quick lock mechanism, and first quick lock mechanism passes through the fuselage signal contact, and first self-driving appearance, first quick lock mechanism and second signal contact.
Further, the wing is positioned at the upper part of the fuselage, and the highest position of the upper surface of the wing is tangential to the fuselage.
Further, the propulsion device comprises a motor and a propeller, wherein the motor is arranged on a motor seat at the front edge of the wing through bolts, and the propeller is connected with the motor.
Further, the motors are brushless motors, and the directions of the motors on the wings at two sides are opposite.
Further, the first quick locking mechanism is in the shape of a circular cross boss, four cross protrusions are uniformly distributed on the circumference, the first signal contacts are uniformly distributed on the boss axis side by side, the second quick locking mechanism is in the shape of a concave cross cylinder, four cross pits are uniformly distributed on the circumference, and the second signal contacts are uniformly distributed on the concave axis side by side.
Further, the bottom of the vertical stabilizer is slightly lower than the bottom of the machine body.
Further, the shape of the machine body is a cylinder with an oval section, and the machine body is wide in front and narrow in back.
Further, the elastomer shells of the front elastomer segment and the rear elastomer segment are manufactured through integrated design and injection molding by adopting nanoscale fiber interweaving materials.
Compared with the prior art, the invention has the following technical effects:
1. The single-soldier hand-thrown type fly-round projectile adopts the flying wing layout to improve the lifting area, adopts a double-motor forward and reverse rotation mode to counteract the reactive torque during take-off, realizes the purpose of hand-thrown throwing and vertical take-off by means of the support of the vertical stabilizer, greatly improves the single-soldier combat efficiency and combat flexibility, and improves the combat reaction speed;
2. The single soldier hand throwing type fly-round projectile adopts the structural design of integrated forming and quick assembly of the quick locking mechanism, the front section and the rear section provided with the warhead are respectively carried, the carrying flexibility is high, the single soldier can carry 4 to 5 single soldiers, and the single soldier combat efficiency is greatly improved;
3. The individual hand-thrown type patrol projectile body is integrally formed by adopting a lightweight structure of nanoscale fiber interweaving materials, and has the advantages of good structural strength, high integration level and light weight.
Drawings
Fig. 1 is a schematic structural view of the present invention.
Fig. 2 is a perspective view of the present invention.
FIG. 3 is a schematic view of the joint between the front and rear elastomeric segments of the present invention.
Detailed Description
The present invention will be described more fully hereinafter with reference to the accompanying drawings, in which preferred embodiments are shown, for the purpose of illustrating the invention, but the scope of the invention is not limited to the specific embodiments shown.
As shown in fig. 1-3, an individual soldier hand-thrown type fly-round missile in the flying wing layout of the present embodiment is assembled by a front projectile segment 1 and a rear projectile segment 2, the front projectile segment 1 includes a seeker 101, a fighter part 102 and a first quick lock mechanism 103, the seeker 101 is located at the top of the front projectile segment, the fighter part 102 is directly connected with the seeker 101 and located in the middle of the front projectile segment, the first quick lock mechanism 103 is located at the tail end of the front projectile segment, and first signal contacts 104 are distributed on the first quick lock mechanism 103.
The rear segment 2 of the projectile body comprises a fuselage 201, wings 205, a propulsion device, a vertical stabilizer 206, a second quick locking mechanism 211, a self-driving instrument 207, a data transmission 208, a battery 209 and a picture transmission 210.
The wings 205 are arranged on two sides of the fuselage 201, the wings 205 are positioned on the upper part of the fuselage, the highest position of the upper surface of the wings is tangent to the fuselage, and the joint part adopts streamline natural transition; the propulsion unit is located wing front end and is close to fuselage third department, controls one respectively, propulsion unit includes motor 203, screw 202, and motor 203 passes through the bolt to be installed on the motor cabinet 204 of wing 205 front edge, and screw 202 links to each other with motor 203, motor 203 is high-power brushless motor, and the motor turns to on the both sides wing is opposite, because the model aeroplane and model ship deflection torsion that the single screw fixed wing body produced because of the conservation of angular momentum, every screw disposes a brushless motor, and the counter-torque of two motor rotational speeds counter-force screws makes take off the gesture steady controllably. The rear end of the wing 205 is a set of control surfaces.
The edges of the left wing and the right wing are respectively provided with a pair of vertical stabilizers 206, the vertical stabilizers are in an up-down symmetrical structure, the whole is in an arrow shape, the bottom of each vertical stabilizer 206 is slightly lower than the bottom of the machine body, the vertical lifting function can be realized by virtue of the support of each vertical stabilizer 206, and the emission tasks of the topography of obstacles such as a block, a roadway and the like can be adapted.
The self-driving instrument 207, the data transmission 208, the battery 209 and the image transmission 210 are arranged inside the machine body, the second quick lock mechanism 211 is positioned at the front end of the machine body 201, second signal contacts are distributed on the second quick lock mechanism 211, the first quick lock mechanism 103 and the second quick lock mechanism 211 are quickly engaged through lock catches, and the self-driving instrument is simple and convenient, and greatly reduces the preparation time on the premise of meeting portability. The autopilot 207 communicates with the projectile front through the first signal contact and the second signal contact.
Further, the first quick locking mechanism is in the shape of a circular cross boss, four cross protrusions are uniformly distributed on the circumference, the first signal contacts are uniformly distributed on the boss axis side by side, the second quick locking mechanism is in the shape of a concave cross cylinder, four cross pits are uniformly distributed on the circumference, and the second signal contacts are uniformly distributed on the concave axis side by side.
Further, the shape of the machine body is an elliptical cylinder with a wide front part and a narrow rear part, and the machine body is smooth and continuous.
Furthermore, the elastomer shells of the front elastomer segment and the rear elastomer segment are manufactured by adopting an integrated design and adopting a nanoscale fiber interweaving material through injection molding, so that the cost is low, the production period is short, and mass production can be realized. After the front segment and the rear segment of the projectile body are formed, the projectile body can be respectively shipped by embedding avionics equipment, a fighter device and the like, and the projectile body is safe and reliable and can be put into use by quick assembly through a quick locking device.
Many modifications and other embodiments of the invention will come to mind to one skilled in the art to which this invention pertains having the benefit of the teachings presented in the foregoing descriptions and the associated drawings. Therefore, it is to be understood that the inventions are not to be limited to the specific embodiments disclosed and that modifications and other embodiments are intended to be included within the scope of the appended claims. Although specific terms are employed herein, they are used in a generic and descriptive sense only and not for purposes of limitation.
Claims (6)
1. An individual soldier hand throwing type fly-round missile with an all-wing layout, which is characterized in that: the self-locking device comprises a body, wings, a propelling device, a vertical stabilizer, a second quick locking mechanism, a self-driving instrument, a data transmission, a battery and a picture transmission, wherein the body front section comprises a guide head, a fighter part and a first quick locking mechanism; the first quick locking mechanism is in the shape of a circular cross boss, four cross-shaped protrusions are uniformly distributed on the circumference, the first signal contacts are uniformly distributed on the boss axis side by side, the second quick locking mechanism is in the shape of a concave cross cylinder, four cross-shaped pits are uniformly distributed on the circumference, and the second signal contacts are uniformly distributed on the concave axis side by side.
2. The flying wing layout individual hand-thrown type fly-round as defined in claim 1, wherein: the propulsion device comprises a motor and a propeller, wherein the motor is arranged on a motor seat at the front edge of the wing through bolts, and the propeller is connected with the motor.
3. An individual hand-thrown type fly-round for flying wing layout as defined in claim 2, wherein: the motors are brushless motors, and the directions of the motors on the wings at two sides are opposite.
4. The flying wing layout individual hand-thrown type fly-round as defined in claim 1, wherein: the bottom of the vertical stabilizer is slightly lower than the bottom of the machine body.
5. The flying wing layout individual hand-thrown type fly-round as defined in claim 1, wherein: the shape of the machine body is a cylinder with an elliptic section, and the machine body is wide in front and narrow in back.
6. An individual soldier hand thrown type flying saucer according to any one of claims 1 to 5, wherein: the elastomer shells of the elastomer front section and the elastomer rear section are manufactured by adopting an integrated design and adopting a nano-scale fiber interweaving material through injection molding.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811362575.2A CN109269363B (en) | 2018-11-16 | 2018-11-16 | Single-soldier hand-throwing type fly-round missile with flying wing layout |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811362575.2A CN109269363B (en) | 2018-11-16 | 2018-11-16 | Single-soldier hand-throwing type fly-round missile with flying wing layout |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109269363A CN109269363A (en) | 2019-01-25 |
| CN109269363B true CN109269363B (en) | 2024-05-10 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201811362575.2A Active CN109269363B (en) | 2018-11-16 | 2018-11-16 | Single-soldier hand-throwing type fly-round missile with flying wing layout |
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Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN116105550A (en) * | 2021-11-10 | 2023-05-12 | 北京理工大学 | Inflatable unfolding patrol projectile with multiple modes |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4962706A (en) * | 1988-05-04 | 1990-10-16 | Ivermee Stanley W O | Fuze for artillery shell |
| CN205131625U (en) * | 2015-11-10 | 2016-04-06 | 湖南云顶智能科技有限公司 | Small -size portable all -wing aircraft overall arrangement unmanned aerial vehicle |
| CN206537488U (en) * | 2016-10-21 | 2017-10-03 | 中国民航大学 | A kind of flexible rotor aircraft |
| CN108639328A (en) * | 2018-05-15 | 2018-10-12 | 西北工业大学 | A kind of New Tail A seating axial symmetry multiple propeller vertical take-off and landing drone |
| CN207976062U (en) * | 2018-03-26 | 2018-10-16 | 西安冰果智能航空科技有限公司 | A kind of high-performance scout missile adapting to varying environment |
| CN209147839U (en) * | 2018-11-16 | 2019-07-23 | 湖南省军合科技有限公司 | A kind of Flying-wing individual soldier hand-thrown type scout missile |
-
2018
- 2018-11-16 CN CN201811362575.2A patent/CN109269363B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4962706A (en) * | 1988-05-04 | 1990-10-16 | Ivermee Stanley W O | Fuze for artillery shell |
| CN205131625U (en) * | 2015-11-10 | 2016-04-06 | 湖南云顶智能科技有限公司 | Small -size portable all -wing aircraft overall arrangement unmanned aerial vehicle |
| CN206537488U (en) * | 2016-10-21 | 2017-10-03 | 中国民航大学 | A kind of flexible rotor aircraft |
| CN207976062U (en) * | 2018-03-26 | 2018-10-16 | 西安冰果智能航空科技有限公司 | A kind of high-performance scout missile adapting to varying environment |
| CN108639328A (en) * | 2018-05-15 | 2018-10-12 | 西北工业大学 | A kind of New Tail A seating axial symmetry multiple propeller vertical take-off and landing drone |
| CN209147839U (en) * | 2018-11-16 | 2019-07-23 | 湖南省军合科技有限公司 | A kind of Flying-wing individual soldier hand-thrown type scout missile |
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| CN109269363A (en) | 2019-01-25 |
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