CN109269363A - A kind of Flying-wing individual soldier hand-thrown type scout missile - Google Patents
A kind of Flying-wing individual soldier hand-thrown type scout missile Download PDFInfo
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- CN109269363A CN109269363A CN201811362575.2A CN201811362575A CN109269363A CN 109269363 A CN109269363 A CN 109269363A CN 201811362575 A CN201811362575 A CN 201811362575A CN 109269363 A CN109269363 A CN 109269363A
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- wing
- fuselage
- lock mechanism
- leading portion
- quick lock
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- 230000011664 signaling Effects 0.000 claims abstract description 11
- 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
- 238000010586 diagram Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 230000004888 barrier function Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000036544 posture Effects 0.000 description 1
- 239000000243 solution Substances 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 a kind of Flying-wing individual soldier hand-thrown type scout missiles, assembled by body leading portion and body back segment, body leading portion includes target seeker, warhead, first quick lock mechanism, first quick lock mechanism is located at the end of body leading portion, the first signalling contact is distributed with thereon, body back segment includes fuselage, wing, propulsion device, fixed fin, second quick lock mechanism, autopilot, number passes, battery, figure passes, wing is arranged in fuselage two sides, propulsion device is located at wing nose, the side edge of wing is equipped with a pair of of fixed fin, second quick lock mechanism is located at front fuselage, second signal contact is distributed with thereon, first quick lock mechanism, second quick lock mechanism is quickly agreed with by lock, autopilot passes through the first signalling contact, second signal contact is communicated with body leading portion.Scout missile of the invention realize both can hand-thrown cast or take off vertically by the support of fixed fin, improve individual combat efficiency and operation flexibility, promote the speed of fight reaction.
Description
Technical field
The present invention relates to a kind of scout missile, specially a kind of Flying-wing individual soldier hand-thrown type scout missile.
Background technique
Scout missile be using existing weapon launch, can target area carry out patrol aviation, can undertake monitoring, investigation,
Combat damage assessment, single or the multi-task the ammunition such as on-air radio relaying and target of attack, and the following ammunition development
One important trend.Scout missile far firing range, function are more, execute scouting, positioning, instruction, information relay, injure, assess etc. appoints
Aerial stand-by time is long when business.Using the effect and status that will greatly improve weapon system in battlefield, weapon system is improved
To the striking capabilities and precision of target, unnecessary logistic implications are reduced.In addition, energy of the combat troop under the various postures of operation
Very big extension can be obtained in power, such as: scout missile is cruised by airflight, can promote traditional ammunition strike range；Pass through essence
Really guidance realizes that high-precision is hit；By high maneuver autopilot, the strike under reverse slope, complex environment is realized.
Existing scout missile generally uses big gun to penetrate, and (such as U.S. LAM, which is patrolled, flies attack ammunition), (such as the U.S. is " aerial main for airborne dispensing
Government official person "), individual soldier launch (such as the U.S. " switchblade ") mode, it is very high to emission system attachment dependence.Wherein, individual soldier launches
Scout missile limited by weight and emission rate, substantially all using launching tube emit so that volume and weight is larger, be not easy
It carries.Launching tube is supported by higher requirement to ground simultaneously, and it is unfavorable that the flexibility and fast reaction to individual combat are brought
It influences.
Summary of the invention
The present invention is directed to above-mentioned problems of the prior art, provides easy to carry, the quick assembling of one kind, hand-thrown is cast
Individual soldier's hand-thrown type scout missile.
The technical solution adopted by the invention is as follows: a kind of Flying-wing individual soldier hand-thrown type scout missile, by body leading portion and bullet
Body back segment assembles, and the body leading portion includes target seeker, warhead, the first quick lock mechanism, and target seeker is located at body leading portion
Top, warhead and target seeker be connected directly positioned at the middle part of body leading portion, and the first quick lock mechanism is located at the end of body leading portion
It holds, the first signalling contact is distributed on the first quick lock mechanism, the body back segment includes fuselage, wing, propulsion device, vertical peace
Determine face, the second quick lock mechanism, autopilot, number biography, battery, figure biography, wing is arranged in fuselage two sides, before propulsion device is located at wing
It holds at fuselage one third, each one of left and right, rear airfoil end is one group of manipulation rudder face, and in left and right, the edge of wing is respectively provided with
A pair of of fixed fin, fixed fin are structure symmetrical above and below, generally arrow shaped, and autopilot, number biography, battery, figure pass peace
Mounted in fuselage interior, the second quick lock mechanism is located at front fuselage, and second signal contact is distributed on the second quick lock mechanism, and first is fast
Latch mechanism, the second quick lock mechanism are quickly agreed with by lock, and autopilot passes through the first signalling contact, second signal contact and body
Leading portion communication.
Further, wing is located at back, and upper surface of the airfoil highest point and fuselage are tangent.
Further, the propulsion device includes motor, propeller, and motor is mounted on the motor of leading edge by bolt
On seat, propeller is connected to the motor.
Further, the motor is brushless motor, and the motor steering on the wing of two sides is opposite.
Further, the first quick lock mechanism shape is a circular cross-shaped shape boss, and four crosswises are prominent to be uniformly distributed
In circumference, the first signalling contact is evenly distributed on side by side at boss axis, and the second quick lock mechanism shape is recessed crossed cylinder
Body, four crosswise pits are uniformly distributed in circumference, and second signal contact is evenly distributed on side by side at the axis of concave surface.
Further, fixed fin bottom is slightly below fuselage bottom.
Further, the fuselage shape is the cylinder of ellipsoidal cross section, and fuselage is front wide and rear narrow.
Further, the body shell of body leading portion and body back segment is handed over by integrated design and using nano-scale fiber
Material is knitted to be made by injection molding.
Compared with the existing technology, the present invention has following technical effect that
1, individual soldier's hand-thrown type scout missile of the invention improves lifting area, using the side of bi-motor positive and negative rotation using Flying-wing
Formula counteracts reaction torque when taking off, realize both can hand-thrown cast and also take off vertically by the support of fixed fin, greatly
Individual combat efficiency and operation flexibility are improved greatly, promote the speed of fight reaction；
2, the structure design that individual soldier's hand-thrown type scout missile of the invention is quickly assembled using integrated molding and quick lock mechanism, will fill
The leading portion and back segment for having warhead carry respectively, have higher carrying flexibility, and individual soldier can carry 4~5 pieces, greatly improve
Individual combat efficiency；
3, individual soldier's hand-thrown type scout missile body of the invention is integrally formed using nano-scale fiber interwoven material light structures, structure
Intensity is good, integrated level is high, light-weight.
Detailed description of the invention
Fig. 1 is structural schematic diagram of the invention.
Fig. 2 is three-dimensional structure diagram of the invention.
Fig. 3 is body leading portion and body back segment interconnecting piece schematic diagram of the present invention.
Specific embodiment
To facilitate the understanding of the present invention, the present invention is made below in conjunction with Figure of description and preferred embodiment more complete
Face meticulously describes, but the protection scope of the present invention is not limited to the following specific embodiments.
As shown in Figure 1-Figure 3, a kind of Flying-wing individual soldier hand-thrown type scout missile of the present embodiment, by body leading portion 1 and bullet
Body back segment 2 assembles, and the body leading portion 1 includes target seeker 101, warhead 102, the first quick lock mechanism 103, target seeker
101 are located at the top of body leading portion, and warhead 102 and target seeker 101 are connected directly positioned at the middle part of body leading portion, the first fast lock
Mechanism 103 is located at the end of body leading portion, and the first signalling contact 104 is distributed on the first quick lock mechanism 103.
The body back segment 2 includes fuselage 201, wing 205, propulsion device, fixed fin 206, the second quick lock mechanism
211, autopilot 207, number pass 208, battery 209, figure passes 210.
Wing 205 is arranged in 201 two sides of fuselage, and wing 205 is located at back, upper surface of the airfoil highest point and fuselage phase
It cuts, joining place is using streamlined natural transition；Propulsion device is located at wing nose at fuselage one third, left and right each one
A, the propulsion device includes motor 203, propeller 202, and motor 203 is mounted on the motor cabinet in 205 forward position of wing by bolt
On 204, propeller 202 is connected with motor 203, and the motor 203 is high-power brushless motor, the motor steering on the wing of two sides
Conversely, because single screw fixed-wing body is because the model plane that the conservation of angular momentum generates deflect torsion, each propeller configures one
Brushless motor, two motor speeds offset the reaction torque of propeller on the contrary, keep take-off attitude steadily controllable.205 rear end of wing is one
Group manipulation rudder face.
In left and right, the edge of wing is respectively provided with a pair of of fixed fin 206, and fixed fin is structure symmetrical above and below, whole
For arrow shaped, 206 bottom of fixed fin is slightly below fuselage bottom, and vertical rise can be achieved by the support of fixed fin 206
Function is dropped, block, the launch mission of the barriers landform such as tunnel are adapted to.
Autopilot 207, number pass 208, battery 209, figure passes 210 and is mounted on fuselage interior, and the second quick lock mechanism 211 is located at machine
Second signal contact, the first quick lock mechanism 103, the second quick lock mechanism 211 is distributed on the second quick lock mechanism 211 in 201 front end of body
Quickly agreed with by lock, it is simple and convenient, time is greatly reduced under the premise of meeting portability.Autopilot 207 is logical
Cross the first signalling contact, second signal contact is communicated with body leading portion.
Further, the first quick lock mechanism shape is a circular cross-shaped shape boss, and four crosswises are prominent to be uniformly distributed
In circumference, the first signalling contact is evenly distributed on side by side at boss axis, and the second quick lock mechanism shape is recessed crossed cylinder
Body, four crosswise pits are uniformly distributed in circumference, and second signal contact is evenly distributed on side by side at the axis of concave surface.
Further, it is elliptic cylindrical that the fuselage shape, which is section, and fuselage is front wide and rear narrow, smooth continuous.
Further, the body shell of body leading portion and body back segment is handed over by integrated design and using nano-scale fiber
Material is knitted to be made by injection molding, it is at low cost, it is with short production cycle, it can be mass-produced.Body leading portion and body back segment
It only need to be embedded in Aerial Electronic Equipment, combat gear etc. after molding, can ship, securely and reliably, quickly be assembled by fast locking device respectively
It can come into operation.
With the help of the introduction present in aforementioned specification and relevant drawings, those skilled in the art in the invention will
It will recognize that many modifications and other embodiments of the invention.It will consequently be understood that the present invention is not limited to disclosed specific realities
Scheme is applied, modification and other embodiments are to be considered as included in scope of the appended claims.Although spy is used herein
Determine term, they are only used with generic and descriptive sense, rather than limitation.
Claims (8)
1. a kind of Flying-wing individual soldier hand-thrown type scout missile, it is characterised in that: assembled by body leading portion and body back segment, institute
Stating body leading portion includes target seeker, warhead, the first quick lock mechanism, and target seeker is located at the top of body leading portion, warhead with lead
Leader is connected directly positioned at the middle part of body leading portion, and the first quick lock mechanism is located at the end of body leading portion, on the first quick lock mechanism
The first signalling contact is distributed with, the body back segment includes fuselage, wing, propulsion device, fixed fin, the second fast lock machine
Structure, autopilot, number biography, battery, figure pass, and wing is arranged in fuselage two sides, and propulsion device is located at wing nose and divides close to fuselage three
One of place, each one of left and right, rear airfoil end be one group of manipulation rudder face, in left and right, the side edge of wing is respectively provided with a pair of vertical stable
Face, fixed fin are structure symmetrical above and below, generally arrow shaped, and autopilot, number biography, battery, figure pass and be mounted on fuselage interior,
Second quick lock mechanism is located at front fuselage, second signal contact is distributed on the second quick lock mechanism, the first quick lock mechanism, second are fastly
Latch mechanism is quickly agreed with by lock, and autopilot is communicated by the first signalling contact, second signal contact with body leading portion.
2. a kind of Flying-wing individual soldier hand-thrown type scout missile as described in claim 1, it is characterised in that: wing is located on fuselage
Portion, upper surface of the airfoil highest point and fuselage are tangent.
3. a kind of Flying-wing individual soldier hand-thrown type scout missile as described in claim 1, it is characterised in that: the propulsion device packet
Motor, propeller are included, motor is mounted on the motor cabinet of leading edge by bolt, and propeller is connected to the motor.
4. a kind of Flying-wing individual soldier hand-thrown type scout missile as claimed in claim 3, it is characterised in that: the motor is brushless
Motor, the motor steering on the wing of two sides are opposite.
5. a kind of Flying-wing individual soldier hand-thrown type scout missile as described in claim 1, it is characterised in that: the first fast lock machine
Configuration shape is a circular cross-shaped shape boss, and four crosswises are prominent to be uniformly distributed in circumference, and the first signalling contact is uniformly distributed side by side
At boss axis, the second quick lock mechanism shape is recessed crossed cylinder body, and four crosswise pits are uniformly distributed in circumference,
Second signal contact is evenly distributed on side by side at the axis of concave surface.
6. a kind of Flying-wing individual soldier hand-thrown type scout missile as described in claim 1, it is characterised in that: fixed fin bottom
Slightly below fuselage bottom.
7. a kind of Flying-wing individual soldier hand-thrown type scout missile as described in claim 1, it is characterised in that: the fuselage shape is
The cylinder of ellipsoidal cross section, fuselage are front wide and rear narrow.
8. a kind of Flying-wing individual soldier hand-thrown type scout missile as described in claim 1~7 any one, it is characterised in that: bullet
The body shell of body leading portion and body back segment passes through injection molding by integrated design and using nano-scale fiber interwoven material
It is made.
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 true CN109269363A (en) | 2019-01-25 |
| CN109269363B CN109269363B (en) | 2024-05-10 |
Family
ID=65189389
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| 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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| Country | Link |
|---|---|
| CN (1) | CN109269363B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116105550A (en) * | 2021-11-10 | 2023-05-12 | 北京理工大学 | Inflatable unfolding patrol projectile with multiple modes |
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| Publication number | Publication date |
|---|---|
| CN109269363B (en) | 2024-05-10 |
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