JP2000199699A - Flying body catcher employing several sheets of net - Google Patents

Flying body catcher employing several sheets of net

Info

Publication number
JP2000199699A
JP2000199699A JP11045224A JP4522499A JP2000199699A JP 2000199699 A JP2000199699 A JP 2000199699A JP 11045224 A JP11045224 A JP 11045224A JP 4522499 A JP4522499 A JP 4522499A JP 2000199699 A JP2000199699 A JP 2000199699A
Authority
JP
Japan
Prior art keywords
nets
outer frame
net
flying body
country
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
Application number
JP11045224A
Other languages
Japanese (ja)
Inventor
Yoshio Abe
芳男 阿部
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to JP11045224A priority Critical patent/JP2000199699A/en
Publication of JP2000199699A publication Critical patent/JP2000199699A/en
Pending legal-status Critical Current

Links

Abstract

PROBLEM TO BE SOLVED: To catch the flying body of a hostile country and carry the same to an arbitrary place. SOLUTION: Jet engines and rocket engines are provided on both ends of wings and supporting beams 51 at fore-and-rear, left-and-right and up-and-down positions through crank arms and oscillating devices, then, the blades and supporting beams 51 are connected to outer frame skeletons 45 or housings through connecting beams, while a plurality of sets of bodies, in which nets are provided in an outer frame skeleton 45 and the peripheries of the nets are connected to the outer frame skeletons 45, are connected through connecting beams. Further, a plurality of nets 47, 59 are provided in the housing, having a cavity from the tip end of one part to the tip end of the other part, while the periphery of the nets are connected to the housing. The flying body of a hostile country can be caught by hitting the flying body of hostile country by the nets of the flying body catcher since initial few sheets of the nets will be broken, however, several sheets of nets will remain. The arbitrary parts of the nets are made of expandable material whereby shock, generated upon hitting the flying body of the hostile country, can be lightened.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【産業上の利用分野】相手国の飛行物を捕獲し、任意の
所に落とす。
[Industrial applications] Capture flying objects from other countries and drop them anywhere.

【0002】[0002]

【従来の技術】相手国の飛行物をミサイルで打ち落とし
ていた。
2. Description of the Related Art Missile shots of a flight from a partner country have been shot down.

【0003】[0003]

【発明が解決しようとする課題】飛行物は、高速で飛行
するので、それを待っていて捕獲する事は大きな衝撃が
生じ飛行物捕獲機が壊されるおそれがあるので飛行物を
やんわり受け止めて捕獲し、人家の無い所に落としても
良いし相手国に落としても良い。
Since a flying object flies at a high speed, catching it while waiting for it will cause a great impact and may damage the flying object catcher. Then, it can be dropped to a place without a house or to the partner country.

【0004】[0004]

【発明が解決するための手段】相手国の飛行物が、近ず
きつつあったら前後の翼及び前後の支持梁にクランク
腕、首振りを介して制御によりジェットエンジン及びロ
ケットエンジンを装置した飛行物捕獲機を離陸させ、相
手国の飛行物の軌道上で待つか又は相手国の飛行物の軌
道上を相手に向かって行くか又は相手国の飛行物の軌道
上を相手国の飛行物の速度より遅い速度で遅げ、そして
相手国の飛行物と飛行物捕獲が当たり相手国の飛行物が
飛行物捕獲機の網を1枚目から何枚目かまで破らせ後何
枚目かの網で相手国の飛行物を止めて捕獲し任意の所に
落とす。
SUMMARY OF THE INVENTION A flight in which a jet engine and a rocket engine are installed on front and rear wings and front and rear support beams by a crank arm and a swing through control when a flying object of a partner country is approaching. Take off the catcher and wait in the orbit of the other country's flight, or go in orbit of the other country's flight or in the orbit of the other country's flight. Slower than the speed, and the other country's aircraft and fly catches hit, and the other country's fly breaks the net of the fly catcher from the first to the next several times, Use a net to stop and capture the other country's flight and drop it anywhere.

【0005】上記飛行物捕獲機を空中で静止させるには
ジェットエンジン及びロケットエンジンの噴射口を下に
向け、離陸した後は、ジャイロスコープ又は液体の中に
入れた下げ振り又は水平器等を設けて下がった方のエン
ジンに燃料及び空気又は酸素を多く送る事により略水平
になる。翼及び支持梁の先にクランク腕及び首振りを介
してジェットエンジン及びロケットエンジンを設ける。
[0005] In order to stop the above-mentioned aircraft in the air, the injection ports of the jet engine and the rocket engine are directed downward, and after takeoff, a gyroscope or a plumb bob or a leveler placed in a liquid is provided. By sending more fuel and air or oxygen to the lowered engine, it becomes almost horizontal. A jet engine and a rocket engine are provided at the tip of the wing and the support beam via a crank arm and a swing.

【0006】複数の外枠骨を連結梁及び連結棒で連結
し、前の2本の外枠骨間に斜材を設けてラチス梁状に
し、前記外枠骨の中に網を張りめぐらした物を相手国の
飛行物が飛んで来る方に向けて何枚か設ける。翼及び支
持梁と1部の連結梁を介して外枠骨と結合させる。
[0006] A plurality of outer frame bones are connected by connecting beams and connecting rods, and a diagonal member is provided between the previous two outer frame bones to form a lattice beam, and a net is stretched in the outer frame bones. Several objects should be set up for the person flying from the other country. It is connected to the outer frame bone via the wing and the supporting beam and a part of the connecting beam.

【0007】外枠骨の外形は、多角形、楕円形、円形又
は前記各各を任意に組み合わせる事もある。
The outer shape of the outer frame bone may be polygonal, elliptical, circular or any combination of the above.

【0008】網の糸は、縦と横方向又は縦と横と斜め方
向又は縦又は横と斜め方向又は放射状と中心から外側に
向けた円状のものがある。
[0008] The yarn of the mesh may be in a vertical and horizontal direction, or in a vertical and horizontal and diagonal direction, or in a vertical or horizontal and diagonal direction, or in a radial shape and a circular shape extending outward from the center.

【0009】請求項2で断面某形は、多角形、円形又は
楕円形又は前記各各の形を任意に組み合わせたハウジン
グの1方の端から他方の端まで空洞にした中にハウジン
グの空洞方向と約直角にした網を複数枚設けてハウジン
グと網を固着させる。
According to a second aspect of the present invention, the shape of the cross section is a polygon, a circle, or an ellipse or any combination of the above shapes. The housing is hollow from one end to the other end. The housing and the net are fixed by providing a plurality of nets approximately at right angles to each other.

【0010】請求項3で網を外枠骨又はハウジングの近
く又は網の全体を伸縮性にする。前記伸縮性は、バネ状
又はゴム又は伸縮ビニール等とする。
In the third aspect, the net is made elastic near the outer frame bone or the housing or the whole net. The elasticity is spring-like or rubber or elastic vinyl.

【0011】[0011]

【作用】請求項1のように翼及び支持梁にクランク腕及
び首振りを介してジェットエンジン及びロケットエンジ
ンを前後左右及び上下に設けて制御により前後左右に回
転させる事により滑走路無しで離陸出来、そして空中で
静止出来る。そして縦、横、斜、そして前後又は斜前後
に飛行出来る。外枠骨の中に網を設けたもの複数個連結
梁及び連結棒で連結する事により相手国の飛行物が飛行
物捕獲機に当っても外枠骨は壊れないで初めから何枚か
の網は破れるが後の何枚かの網が破られないようにする
事により相手国の飛行物を捕獲出来る。外枠骨の外形
は、色色あるが円形が1番く正多角形でも角数が多くな
る程良い。
The jet engine and the rocket engine are provided on the wing and the supporting beam via the crank arm and the swing as described in claim 1, and can be taken off without a runway by being rotated back and forth and left and right by control. , And can stand still in the air. It can fly vertically, horizontally, diagonally, and back and forth or back and forth. Outer frame bone provided with a mesh By connecting with a plurality of connecting beams and connecting rods, the outer frame bone is not broken even if the flight of the partner country hits the aircraft The net breaks, but you can capture the other country's flight by keeping some of the nets unbroken. Although the outer shape of the outer frame bone is colored, it is better that the number of corners is larger even in a regular polygon having the largest circular shape.

【0012】請求項2のように断面某形は円形又は多角
形で角の数が多い方が良い、そして1方の先端から他方
の先端まで空洞としたハウジングの中に網を複数枚設け
る事により初めの何枚かの網を相手国の飛行物で破らせ
後の何枚かの網を残す事により相手国の飛行物を捕獲出
来る。
It is preferable that the shape of the cross section is circular or polygonal and the number of corners is large, and that a plurality of nets are provided in a housing having a cavity from one end to the other end. By breaking the first few nets with the flight of the partner country and leaving some nets after, the flight of the partner country can be captured.

【0013】請求項3のように外枠骨又はハウジングの
近くの網を伸縮性のバネ又はゴム等にするか又は網全体
を伸縮性にする事により相手国の飛行物と飛行物捕獲機
が当ってもバネ又はゴム等が伸びる事により飛行物捕獲
機に与える衝撃が少なくなる。
According to a third aspect of the present invention, the net near the outer frame bone or the housing is made of an elastic spring or rubber or the like, or the entire net is made elastic so that the flying object and the flying object catcher of the partner country can be constructed. Even if it hits, the impact given to the flying object catcher is reduced by the extension of the spring or rubber.

【0014】[0014]

【実施例】請求項順に説明すると翼19、21、44、
74、2Eの両端にクランク腕3、18、42、54、
71、83を設け、前記クランク腕の先に首振り2、1
7、41、53、88、86、を設け、前記首振の先に
ジェットエンジン及びロケットエンジン1、16、4
0、52、70、82、1Eを装置し、前記クランク腕
は、前後に回転させる為ウォームギヤ図6の7D、8D
及びラックとピニオンで動かし、前記首振りを左右に動
かす場ウォームギヤ図6の11D、12D及びラックと
ピニオンで動かす。
DESCRIPTION OF THE PREFERRED EMBODIMENTS In the order of the claims, the wings 19, 21, 44,
74, 2E at both ends of the crank arms 3, 18, 42, 54,
71 and 83 are provided, and a swing 2, 1 is provided at the tip of the crank arm.
7, 41, 53, 88 and 86, and the jet engine and the rocket engine 1, 16, 4
0, 52, 70, 82, and 1E, and the worm gear is used to rotate the crank arm back and forth.
The worm gear is moved by the rack and the pinion, and the swing is moved by the worm and the pinion.

【0015】支持梁10、51、81の両端にクランク
腕7、14、48、55、78、85を設け、前記クラ
ンク腕の先に首振8、13、49、56、84、89を
設けて、前記首振りの先にジェットエンジン及びロケッ
トエンジン9、12、50、57、80、87、9E、
を装置し、前記クランク腕を前後に回転させる場合は、
ウォームギヤ図6の7D、8D及びラックとピニオンで
動かし、前記首振りを左右に動かす場合はウォームギヤ
図6の11D、12D及びラックとピニオンで動かす。
上記翼の両端にクランク腕及び首振りを介し及び支持梁
の両端にクランク腕及び首振り介してジェットエンジン
及びロケットエンジン装置して制御によりジェットエン
ジン及びロケットエンジンの噴射口を任意の方に向け
る。
Crank arms 7, 14, 48, 55, 78, 85 are provided at both ends of the support beams 10, 51, 81, and swings 8, 13, 49, 56, 84, 89 are provided at the ends of the crank arms. And the jet and rocket engines 9, 12, 50, 57, 80, 87, 9E,
If you want to rotate the crank arm back and forth,
The worm gear is moved by 7D, 8D, a rack and a pinion in FIG. 6, and when the swing is moved right and left, the worm gear is moved by 11D and 12D in FIG. 6 and a rack and a pinion.
The jet engine and the rocket engine are controlled through the crank arm and the swing at both ends of the wing and the crank arm and the swing at both ends of the support beam, and the jet ports of the jet engine and the rocket engine are directed to arbitrary directions by control.

【0016】翼及び支持梁に1部の連結梁28、26、
32、11E、12E、を結合させ、前記連結梁に外枠
骨4、45、75、6E、7E、を結合し、前の外枠骨
2本を斜材29、5Eを用いてラチス梁状とし、前記外
枠骨の中に網を設けた物を相手国の飛行物が向かって来
る方に複数個を連結梁及び連結棒で連結する。外枠骨の
外形は多角形、円形、楕円形、又は前記各各の形を任意
に組み合わせたものとするが円形が1番良い。上の翼よ
り支持梁を短くする。
A part of connecting beams 28, 26,
32, 11E, and 12E, and outer frame bones 4, 45, 75, 6E, and 7E are connected to the connection beam, and the two outer frame bones are formed into lattice beams using diagonal members 29 and 5E. Then, a plurality of nets provided in the outer frame bones are connected by connecting beams and connecting rods in a direction to which the flying object of the partner country comes. The outer shape of the outer frame bone is a polygon, a circle, an ellipse, or any combination of the above shapes, but the circle is the best. Make the support beam shorter than the upper wing.

【0017】請求項2のように翼及び支持梁に断面多角
形又は円形又は楕円形又は前記各各を任意に組み合わせ
た1方の先端から他方の先端まで空洞としたハウジング
の中に網をハウジングと略直角に設けて結合する。網
は、複数枚とする。
[0017] According to a second aspect of the present invention, a net is formed in a housing having a hollow from one end to the other end in which the wing and the support beam have a polygonal or circular or elliptical cross section or any combination of the above. Are provided at substantially right angles to each other. There are a plurality of nets.

【0018】請求項3のように外枠骨及びハウジングの
内に網を設けて接合させ、前記網の周囲にバネ5、4
6、76を設けるか又は網全体を伸縮性のひも状とす
る。
According to a third aspect of the present invention, a net is provided and joined in the outer frame bone and the housing, and springs 5, 4 are provided around the net.
6, 76 are provided or the whole net is made into an elastic string.

【0019】レーダにより相手国の飛行物を確認し無線
操縦又は自動操縦により相手国の飛行物の軌道上に待つ
か又は向かって行くか又は相手国の飛行物より遅い速度
で逃げてそして相手国の飛行物と飛行物捕獲機と衝突さ
せて初めの何枚かの網を破らせ後の何枚かの網を残す。
翼及び支持梁と外枠骨を支柱で結合する。
The radar confirms the flight of the partner country and waits or heads for the flight of the partner country by radio control or autopilot or escapes at a slower speed than the flight of the partner country and Collision with a flying object and a flight catcher to break some of the first nets and leave some nets after.
The wings and the supporting beams are connected to the outer frame bones by columns.

【0020】[0020]

【発明の効果】請求項1のように飛行物捕獲機の前後左
右及び上下にジェットエンジン及びロケットエンジンを
装置する事によりジェットエンジン及びロケットエンジ
ンの噴射口を下に向ける事により滑走路無しで離陸出
来、そして空中で静止させたり相手国の飛行物の飛行線
と並行に飛行物捕獲機の向を合わせて並行に移動出来
る。1番前の外枠骨と2番目の外枠骨の間に斜材を結合
させてラチス梁状とし、前記ラチス梁状に何本かの連結
梁及び何本かの連結棒を結合し、前記連結梁及び連結棒
を複数の外枠骨と結合させて各各の外枠骨の中に網を設
けて端を外枠骨に結合する事により相手国の飛行物と衝
突しても初めの何枚か網は破らせるが後の何枚かの網は
残るので相手国の飛行物を捕獲出来る。外枠骨の外形は
色色あるが円形が1番良い。
According to the first aspect of the present invention, a jet engine and a rocket engine are installed in front, back, left, right and up and down of a flying object catcher. It can be stationary in the air or move in parallel with the flight catcher in parallel with the flight line of the other country's flight. A diagonal member is connected between the foremost outer frame bone and the second outer frame bone to form a lattice beam, and a number of connecting beams and some connecting rods are connected to the lattice beam, Even if the connecting beam and the connecting rod are connected to a plurality of outer frame bones, a net is provided in each outer frame bone, and the ends are connected to the outer frame bones, even if the vehicle collides with a flying object of the other country, the first time. Some nets can be broken, but some nets remain so that you can capture the flight of the other country. The outer shape of the outer frame bone is colored, but a circle is best.

【0021】請求項2のように1方の先端から他方の先
端まで空洞としたハウジングの中に網を複数設けて網の
端とハウジングを結合する事により初めの何枚かの網を
相手国の飛行物で破せるが残りの何枚かの網で相手国の
飛行物を止めるので相手国の飛行物を捕獲出来る。
According to a second aspect of the present invention, a plurality of nets are provided in a hollow housing from one end to the other end, and the first several nets are connected to the other country by connecting the ends of the nets to the housing. Can be broken with any other airplane, but you can capture the airplane of the other country by stopping the airplane of the other country with the remaining nets.

【0022】請求項3のように外枠骨又はハウジングの
近くの網を伸縮性のバネ又はゴム等又は網全体を伸縮性
にする事により相手国の飛行物と飛行物捕獲機が衝突し
た時はバネ又は伸縮性のゴム又はプラスチック等が伸び
る事により飛行物捕獲機に与える衝撃は少なくなる。
According to a third aspect of the present invention, when the net near the outer frame bone or the housing is made of an elastic spring or rubber or the entire net is made elastic, the flying object of the other country collides with the flying object catcher. The impact applied to the aircraft catcher by the expansion of a spring or elastic rubber or plastic is reduced.

【図面の簡単な説明】[Brief description of the drawings]

【図1】外枠骨が四角な飛行物捕獲機の正面図である。FIG. 1 is a front view of a flying object catcher having a square outer frame bone.

【図2】図1のA−A断面図である。FIG. 2 is a sectional view taken along line AA of FIG.

【図3】図1のB−B断面図である。FIG. 3 is a sectional view taken along the line BB of FIG. 1;

【図4】外枠骨が、円形な飛行物捕獲機の正面図であ
る。
FIG. 4 is a front view of the aircraft catcher having a circular outer frame bone.

【図5】図4のC−C断面図である。FIG. 5 is a sectional view taken along line CC of FIG. 4;

【図6】各各のクランク腕及び首振りの詳細図である。FIG. 6 is a detailed view of each crank arm and swing.

【図7】外枠骨が、円形な飛行物捕獲機の正面図であ
る。
FIG. 7 is a front view of the aircraft catcher having a circular outer frame bone.

【図8】図7のE方向から見た側面図である。FIG. 8 is a side view as seen from a direction E in FIG. 7;

【符号の説明】[Explanation of symbols]

ジェットエンジン及びロケットエンジン 1、1
6、9、12、40、50、52、57、1D、70、
80、82、87、1E、9E、 首振り 2、8、17、13、41、4
9、53、56、16D、88、86、 クランク腕 3、18、8、13、42、4
8、54、55、17D、71、78、83、85、 外枠骨 4、10、15、31、45、
75、6E、7E、 バネ 5、46、7C、76 翼 19、20、21、44、1
C、3C、74、10E、2E、 連結梁 33、26、32、30、2
C、8C11E、72、79、12E 網 6、11、22、23、24、
25、27、47、59、4C、5C、9C、10C、
77、 支持梁 51、81 ラチス 29、90 ウォームギヤ 7D、8D、11D、12D、 プレート 6C 電線 2D、6D 油送管 3D ギヤ 4D、5D、 クラッチ 9D、 クラッチ棒 10D、13D、 抜け止め 14D、15D 支柱 73
Jet engine and rocket engine 1, 1
6, 9, 12, 40, 50, 52, 57, 1D, 70,
80, 82, 87, 1E, 9E, Swing 2, 8, 17, 13, 41, 4
9, 53, 56, 16D, 88, 86, Crank arm 3, 18, 8, 13, 42, 4
8, 54, 55, 17D, 71, 78, 83, 85, outer frame bones 4, 10, 15, 31, 45,
75, 6E, 7E, spring 5, 46, 7C, 76 wings 19, 20, 21, 44, 1
C, 3C, 74, 10E, 2E, connecting beams 33, 26, 32, 30, 2
C, 8C11E, 72, 79, 12E Network 6, 11, 22, 23, 24,
25, 27, 47, 59, 4C, 5C, 9C, 10C,
77, support beams 51, 81 lattice 29, 90 worm gear 7D, 8D, 11D, 12D, plate 6C electric wire 2D, 6D oil feed pipe 3D gear 4D, 5D, clutch 9D, clutch rod 10D, 13D, retaining stopper 14D, 15D post 73

Claims (3)

【特許請求の範囲】[Claims] 【請求項1】 翼(19)、(21)、(44)、(3
C)、(74)、(2E)及び支持梁(10)、(5
1)、(81)の両端にクランク腕(3)、(18)、
(42)、(54)、(71)、(83)及び(7)、
(14)、(48)、(55)、(78)、(85)を
設け、前記クランク腕の先に首振り(2)、(17)、
(41)、(41)、(53)、(88)、(86)及
び(8)、(13)、(49)、(56)、(84)、
(89)を設けて、前記首振りの先にジェットエンジン
及びロケットエンジン(1)、(16)、(40)、
(52)、(70)、(82)、(1E)及び(9)、
(12)、(50)、(57)、(80)、(87)、
(9E)を装置した飛行物捕獲機で、前記ジェットエン
ジン及びロケットエンジンは、制御により上下左右に回
転可とし、前記翼と1部の連結梁を介して外枠骨
(4)、(45)、(75)を結合させ、前記外枠骨と
1部の連結梁を介して前記支持梁と結合させ、前記外枠
骨を何個か連結梁(28)、(26)、(32)(2
C)、(8C)、(11E)、(72)(79)、(1
2E)で連結し、前記外枠骨の外形を某形とした中に網
を設けて網の端と骨枠骨を結合したものを飛行物が飛ん
で来る方に向けて複数枚門を設けて重ねる事を特徴とし
た飛行物捕獲機。
1. Wings (19), (21), (44), (3)
C), (74), (2E) and supporting beams (10), (5)
1), crank arms (3), (18),
(42), (54), (71), (83) and (7),
(14), (48), (55), (78), and (85) are provided, and a swing (2), (17),
(41), (41), (53), (88), (86) and (8), (13), (49), (56), (84),
(89), a jet engine and a rocket engine (1), (16), (40),
(52), (70), (82), (1E) and (9),
(12), (50), (57), (80), (87),
In the aircraft catcher equipped with (9E), the jet engine and the rocket engine are rotatable up, down, left, and right under control, and outer frame bones (4), (45) are connected to the wings and a partial connecting beam. , (75) are connected to the support beam via the outer frame bone and a part of the connecting beam, and some of the outer frame bones are connected to the connecting beams (28), (26), (32) ( 2
C), (8C), (11E), (72) (79), (1
2E), a net is provided in the shape of the outer frame bone having a predetermined shape, and a plurality of gates are provided by connecting the end of the net and the bone frame bone to a direction in which a flying object is flying. A flying object capture machine characterized by stacking.
【請求項2】断面某形で1方の端から他方の端まで空洞
としたハウジングの中に飛行物が飛んで来る方に向けて
網を複数枚間を設けて前記ハウジングと網の端を結合し
たものを複数設ける事を特徴とした請求項1記載の飛行
物捕獲機。
2. A plurality of nets are provided between a plurality of nets toward a direction in which a flying object comes into a housing having a hollow section from one end to the other end with a certain cross section. 2. The flying object catcher according to claim 1, wherein a plurality of joined objects are provided.
【請求項3】網の任意の所を伸縮性とした事を特徴とし
た請求項1又は2記載の飛行物捕獲機。
3. The flying object catcher according to claim 1, wherein an arbitrary portion of the net is made elastic.
JP11045224A 1999-01-04 1999-01-04 Flying body catcher employing several sheets of net Pending JP2000199699A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11045224A JP2000199699A (en) 1999-01-04 1999-01-04 Flying body catcher employing several sheets of net

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11045224A JP2000199699A (en) 1999-01-04 1999-01-04 Flying body catcher employing several sheets of net

Publications (1)

Publication Number Publication Date
JP2000199699A true JP2000199699A (en) 2000-07-18

Family

ID=12713309

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11045224A Pending JP2000199699A (en) 1999-01-04 1999-01-04 Flying body catcher employing several sheets of net

Country Status (1)

Country Link
JP (1) JP2000199699A (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102374828A (en) * 2010-08-27 2012-03-14 北京理工大学 Curtain type aircraft intercepting equipment without collateral damages
CN102384702A (en) * 2010-08-30 2012-03-21 北京理工大学 Method for intercepting aircrafts without collateral damage in unmanned way
US9085362B1 (en) * 2012-11-21 2015-07-21 Lockheed Martin Corporation Counter-unmanned aerial vehicle system and method
CN106741889A (en) * 2016-11-28 2017-05-31 上海交通大学 A kind of band catches the pouch-type aircraft of playing function

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102374828A (en) * 2010-08-27 2012-03-14 北京理工大学 Curtain type aircraft intercepting equipment without collateral damages
CN102384702A (en) * 2010-08-30 2012-03-21 北京理工大学 Method for intercepting aircrafts without collateral damage in unmanned way
US9085362B1 (en) * 2012-11-21 2015-07-21 Lockheed Martin Corporation Counter-unmanned aerial vehicle system and method
US9896221B1 (en) 2012-11-21 2018-02-20 Lockheed Martin Corporation Unmanned aerial vehicle (UAV) having a deployable net for capture of threat UAVs
US10800546B2 (en) 2012-11-21 2020-10-13 Lockheed Martin Corporation Unmanned aerial vehicle (UAV) and system and method for capture of threat UAVs
CN106741889A (en) * 2016-11-28 2017-05-31 上海交通大学 A kind of band catches the pouch-type aircraft of playing function
CN106741889B (en) * 2016-11-28 2020-07-14 上海交通大学 Pocket type aircraft with catching and releasing functions

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