CN209147840U - A kind of normal arrangement individual soldier hand-thrown type scout missile - Google Patents
A kind of normal arrangement individual soldier hand-thrown type scout missile Download PDFInfo
- Publication number
- CN209147840U CN209147840U CN201821883828.6U CN201821883828U CN209147840U CN 209147840 U CN209147840 U CN 209147840U CN 201821883828 U CN201821883828 U CN 201821883828U CN 209147840 U CN209147840 U CN 209147840U
- Authority
- CN
- China
- Prior art keywords
- lock mechanism
- fuselage
- quick lock
- leading portion
- individual soldier
- 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
Landscapes
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The utility model discloses a kind of normal arrangement 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, the body back segment includes fuselage, wing, empennage, propulsion device, second quick lock mechanism, autopilot, number passes, battery, figure passes, fuselage shape is cylindrical body, end section is front wide and rear narrow rotary table, wing is arranged in fuselage two sides, a pair of of empennage is installed on the two sides of rotary table, propulsion device is located at rotary table end, empennage rear direction rudder adjoins propulsion device, 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 is touched by the first signal Point, second signal contact are communicated with body leading portion.The utility model realizes hand-thrown projectile and takes off, and improves individual combat efficiency and operation flexibility.
Description
Technical field
The utility model relates to a kind of scout missile, specially a kind of normal arrangement 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 utility model is directed to above-mentioned problems of the prior art, provides easy to carry, the quick assembling of one kind, hand-thrown
Individual soldier's hand-thrown type scout missile of projectile.
The technical solution adopted in the utility model is as follows: a kind of normal arrangement individual soldier hand-thrown type scout missile, by body leading portion
Assemble with body back segment, the body leading portion includes target seeker, warhead, the first quick lock mechanism, and target seeker is located at body
The top of leading portion, warhead and target seeker are connected directly positioned at the middle part of body leading portion, and the first quick lock mechanism is located at body leading portion
End, the first signalling contact is distributed on the first quick lock mechanism, the body back segment includes fuselage, wing, empennage, promotes dress
It sets, the second quick lock mechanism, autopilot, number biography, battery, figure biography, fuselage shape is cylindrical body, and tail cone part is front wide and rear narrow
Rotary table, wing is arranged in fuselage two sides, and a pair of of empennage is installed on the two sides of tail cone rotary table, and empennage level inclination is 45
Degree occupies entire rotary table, and propulsion device is located at rotary table end, and empennage rear portion is equipped with rudder, and rudder adjoins propulsion device, from
It drives instrument, number biography, battery, figure to pass and be mounted on fuselage interior, the second quick lock mechanism is located at front fuselage, is distributed on the second quick lock mechanism
There is second signal contact, the first quick lock mechanism, the second quick lock mechanism are quickly agreed with by lock, and autopilot is touched by the first signal
Point, second signal contact are communicated with body leading portion.
Further, wing is located at back, and upper surface of the airfoil highest point and fuselage are tangent, wing and fuselage joining place
Using streamlined natural Transition Design.
Further, tail cone rotary table accounts for about fuselage length one third.
Further, the propulsion device includes a propeller and a motor, and motor uses high-power brushless motor.
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, fuselage roof is provided with the hatchcover for agreeing with contact with fuselage, for installing scout missile Aerial Electronic Equipment.
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 utility model is designed using normal arrangement high aspect ratio, improves lifting surface
Product, the stagnant empty cruise time for improving scout missile, enhance rudder face effect by the way of single motor propulsion device and empennage cooperation,
It improves the flexibility of scout missile control, use big thrust loading dynamical system, realize hand-thrown projectile and take off, substantially increase
Individual combat efficiency and operation flexibility promote the speed of fight reaction；
2, the structure that individual soldier's hand-thrown type scout missile of the utility model uses integrated molding and quick lock mechanism quickly to assemble
The leading portion that warhead is housed and back segment are carried respectively, have higher carrying flexibility by design, 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 utility model is using nano-scale fiber interwoven material light structures one
Molding, structural strength is good, integrated level is high, light-weight.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model.
Fig. 2 is the three-dimensional structure diagram of the utility model.
Fig. 3 is the utility model body leading portion and body back segment interconnecting piece schematic diagram.
Specific embodiment
For the ease of understanding the utility model, below in conjunction with Figure of description and preferred embodiment to the utility model
Work more comprehensively, meticulously describes, but the protection scope of the utility model is not limited to embodiment in detail below.
As shown in Figure 1-Figure 3, a kind of normal arrangement 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 includes fuselage 201, wing 202, empennage 207, propulsion device, the second quick lock mechanism 210, self-driving
Instrument 203, number pass 205, battery 206, figure passes 204.201 shape of fuselage is cylindrical body, and fuselage roof is provided with to agree with fuselage and contact
Hatchcover, for installing scout missile Aerial Electronic Equipment, tail cone part is front wide and rear narrow rotary table, and rotary table accounts for about fuselage length three
/ mono-.Wing 202 is arranged in fuselage two sides, and wing 202 is located at 201 top of fuselage, 202 upper surface highest point of wing and fuselage
201 is tangent, and wing 202 and 201 joining place of fuselage are using streamlined natural Transition Design.A pair of of empennage 207 is installed on fuselage end
The two sides of rotary table are held, 207 level inclination of empennage is 45 degree, occupies entire rotary table, propulsion device is located at rotary table end, including one
Propeller 209 and a motor 208, motor 208 use high-power brushless motor, meet the lift that scout missile quickly takes off and want
It asks.207 rear portion of empennage is equipped with rudder, and body attitude is adjusted, and rudder adjoins propulsion device, passes through propulsion device propeller
The air-flow of generation can enhance the rudder face effect of rudder, quickly adjust body attitude, enhance the controllability of scout missile.Autopilot
203, number passes 205, battery 206, figure passes 204 and is mounted on fuselage interior, and the second quick lock mechanism 210 is located at front fuselage, and second is fast
Second signal contact is distributed on latch mechanism 210, the first quick lock mechanism 103, the second quick lock mechanism 210 are by latching quick contract
It closes, it is simple and convenient, time is greatly reduced under the premise of meeting portability.Autopilot 203 by 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, 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.
With the help of the introduction present in aforementioned specification and relevant drawings, the technology people of the utility model fields
Member will be appreciated that many modifications and other embodiments of the utility model.It will consequently be understood that the utility model is not limited to
Disclosed specific embodiment, modification and other embodiments are to be considered as included in scope of the appended claims.Although this
Specific term is used in text, they are only used with generic and descriptive sense, rather than limitation.
Claims (7)
1. a kind of normal arrangement 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, empennage, propulsion device, the second quick lock mechanism, self-driving
Instrument, number biography, battery, figure pass, and fuselage shape is cylindrical body, and tail cone part is front wide and rear narrow rotary table, and wing is arranged in machine
Body two sides, a pair of of empennage are installed on the two sides of tail cone rotary table, and empennage level inclination is 45 degree, occupy entire rotary table, promote
Device is located at rotary table end, and empennage rear portion is equipped with rudder, and rudder adjoins propulsion device, and autopilot, number biography, battery, figure pass
It is mounted on fuselage interior, the second quick lock mechanism is located at front fuselage, it is distributed with second signal contact on the second quick lock mechanism, first
Quick lock mechanism, the second quick lock mechanism are quickly agreed with by lock, and autopilot passes through the first signalling contact, second signal contact and bullet
The communication of body leading portion.
2. a kind of normal arrangement 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, and wing and fuselage joining place are using streamlined natural Transition Design.
3. a kind of normal arrangement individual soldier hand-thrown type scout missile as described in claim 1, it is characterised in that: tail cone rotary table is about
Account for fuselage length one third.
4. a kind of normal arrangement individual soldier hand-thrown type scout missile as described in claim 1, it is characterised in that: the propulsion device packet
A propeller and a motor are included, motor uses high-power brushless motor.
5. a kind of normal arrangement 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 normal arrangement individual soldier hand-thrown type scout missile as described in claim 1, it is characterised in that: fuselage roof be provided with
Fuselage agrees with the hatchcover of contact, for installing scout missile Aerial Electronic Equipment.
7. a kind of normal arrangement individual soldier hand-thrown type scout missile as described in claim 1~6 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 |
|---|---|---|---|
| CN201821883828.6U CN209147840U (en) | 2018-11-16 | 2018-11-16 | A kind of normal arrangement individual soldier hand-thrown type scout missile |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821883828.6U CN209147840U (en) | 2018-11-16 | 2018-11-16 | A kind of normal arrangement individual soldier hand-thrown type scout missile |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209147840U true CN209147840U (en) | 2019-07-23 |
Family
ID=67285971
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821883828.6U Active CN209147840U (en) | 2018-11-16 | 2018-11-16 | A kind of normal arrangement individual soldier hand-thrown type scout missile |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209147840U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110763090A (en) * | 2019-10-11 | 2020-02-07 | 南京理工大学 | Combinable and deformable primary-secondary type patrol and play integrated flying bomb and working method thereof |
| CN110940236A (en) * | 2019-11-21 | 2020-03-31 | 陈秀梅 | Non-aiming intelligent flying patrol bomb |
| CN111981902A (en) * | 2020-09-10 | 2020-11-24 | 中国工程物理研究院总体工程研究所 | Multi-connected barrel-mounted shooting patrol missile, system and working method |
-
2018
- 2018-11-16 CN CN201821883828.6U patent/CN209147840U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110763090A (en) * | 2019-10-11 | 2020-02-07 | 南京理工大学 | Combinable and deformable primary-secondary type patrol and play integrated flying bomb and working method thereof |
| CN110763090B (en) * | 2019-10-11 | 2022-04-08 | 南京理工大学 | Combinable and deformable primary-secondary type patrol and play integrated flying bomb and working method thereof |
| CN110940236A (en) * | 2019-11-21 | 2020-03-31 | 陈秀梅 | Non-aiming intelligent flying patrol bomb |
| CN111981902A (en) * | 2020-09-10 | 2020-11-24 | 中国工程物理研究院总体工程研究所 | Multi-connected barrel-mounted shooting patrol missile, system and working method |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN209147840U (en) | A kind of normal arrangement individual soldier hand-thrown type scout missile | |
| CN109436296A (en) | The folding wings unmanned plane and its launching technique of cartridge type transmitting | |
| CN209274879U (en) | The folding wings unmanned plane of cartridge type transmitting | |
| CN209147839U (en) | A kind of Flying-wing individual soldier hand-thrown type scout missile | |
| CN211626280U (en) | Four-duct propelling type small missile | |
| CN103968714A (en) | Defending bomb device hung in air | |
| CN108100217A (en) | A kind of unmanned vehicle based on X wings layout | |
| CN108327897A (en) | Equip with arms unmanned helicopter | |
| CN109323633A (en) | A kind of normal arrangement individual soldier hand-thrown type scout missile | |
| CN202508282U (en) | Helicopter with guided missiles | |
| CN208216982U (en) | Equip with arms unmanned helicopter | |
| CN109764766A (en) | A kind of electricity duct tail portion push type miniature missile | |
| CN109269363A (en) | A kind of Flying-wing individual soldier hand-thrown type scout missile | |
| CN110567326B (en) | Fixed wing-rotor wing composite unmanned aerial vehicle | |
| CN201362361Y (en) | Forward and rearward attacking type fighter | |
| CN110940236A (en) | Non-aiming intelligent flying patrol bomb | |
| CN113335499B (en) | High-mobility unmanned aerial vehicle based on solid rocket auxiliary power | |
| CN210952527U (en) | Wireless instruction guidance rocket projectile and controlled infrared beacon for 40mm rocket launcher | |
| CN110595293B (en) | Working method of fixed wing-rotor wing composite unmanned aerial vehicle | |
| CN200945932Y (en) | Solar energy folding type bird-shaped flying screen | |
| CN209689503U (en) | A kind of electricity duct tail portion push type miniature missile | |
| CN209889117U (en) | Airborne anti-riot bullet emitter and unmanned aerial vehicle | |
| CN112611268A (en) | Small high-speed flying patrol bomb based on visual image accurate guidance | |
| CN207007016U (en) | A kind of durable type individual soldier target drone | |
| CN218515076U (en) | Air bubble agricultural plant protection system based on unmanned vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |