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1. 发明申请

US20160209189A1 ILLUMINATION MUNITION 审中-公开
标题翻译：照明系统
公开(公告)号：US20160209189A1
公开(公告)日：2016-07-21
申请号：US14913079
申请日：2014-08-18
申请人： BAE SYSTEMS PLC
发明人： DANIEL ALEXANDER ADAMS
IPC分类号： F42B12/42 , F42B4/28
CPC分类号： F42B12/42 , F42B4/28
摘要： The invention relates to an illumination munition, particularly an illumination payload ejection device housed within a common carrier payload delivery shell, with a frangible safety link.There is provided an illumination munition comprising a shearable tail unit, a main body which comprises a payload cavity for receiving an illumination payload apparatus, a fuze, an ogive element located between said main body and the fuze, and an explosive train operably connected to said fuze, wherein the illumination payload apparatus comprises an illumination composition, a drogue parachute and a main parachute, wherein the main parachute is tethered by a payload tether to the payload apparatus, such that after deployment of said main parachute said payload apparatus descends under the control of said main parachute.
摘要翻译：本发明涉及照明弹药，特别是容纳在公共载体有效载荷输送壳体内的照明有效载荷排出装置，具有易碎的安全连接。提供了一种照明弹药，其包括可剪式尾部单元，主体，其包括用于接收照明有效载荷装置的有效载荷空腔，引信，位于所述主体和引信之间的原子元件，以及可操作地连接到所述主体引信，其中所述照明有效载荷装置包括照明组合物，锥形降落伞和主降落伞，其中所述主降落伞由有效载荷系绳系在有效载荷装置上，使得在部署所述主降落伞之后，所述有效载荷装置在控制下降的主降落伞。

2. 发明授权

US4389938A Illuminating rocket possessing a cylindrical container 失效
标题翻译：具有圆柱形容器的照明火箭
公开(公告)号：US4389938A
公开(公告)日：1983-06-28
申请号：US249214
申请日：1981-03-30
申请人： Hugo Sigrist
发明人： Hugo Sigrist
IPC分类号： F41F3/042 , F41F3/077 , F42B4/28
CPC分类号： F41F3/042 , F41F3/077
摘要： Within a cylindrical container or canister, closed at both ends by a respective cover member, there is located a flare or illuminating rocket. For firing the flare rocket it is sufficient to remove the rear cover and by pulling at a tear line there is activated a tear ignition device or fuze. The ignited flare rocket then pierces the front cover member. This front cover member preferably possesses a ring-shaped or annular reference fracture location which subdivides the cover member into a disk-shaped inner portion and a ring-shaped outer portion.
摘要翻译：在圆柱形容器或罐内，两端由相应的盖构件封闭，位于火炬或照明火箭上。为了发射火炬火箭，拆卸后盖是足够的，并且在撕裂线处拉动时，会启动一个撕裂点火装置或引信。然后点燃的火炬火箭刺穿前盖构件。该前盖构件优选地具有环形或环形的参考断裂位置，其将盖构件分成盘形内部部分和环形外部部分。

3. 发明授权

US4094245A Parachute flare having a variable burn rate 失效
标题翻译：具有可变燃烧率的降落伞火炬
公开(公告)号：US4094245A
公开(公告)日：1978-06-13
申请号：US793007
申请日：1977-05-02
申请人： Joseph R. Matura
发明人： Joseph R. Matura
IPC分类号： C06B45/12 , F42B4/26 , F42B4/28
CPC分类号： F42B4/26 , C06B45/12
摘要： A variable burn rate/variable burn time parachute flare, adapted to be trported by a gun cannon or howitzer to a desired height and then ignited to burn at an intensity of 1.6 to 1.8 .times. 10.sup.6 candlepower for 25 to 35 seconds, followed by a second burn at about 0.8 .times. 10.sup.6 candlepower for 75 to 35 seconds and comprising a flare case having a hollow cylindrical wall about 4.5 inches in diameter and about 7 inches long, closed at one-end and open at the other end, and a 0.03 inch coating of polyester or epoxy resin on the closed end and on one-third to two-thirds of the inner wall thereof adjacent to the closed end.
摘要翻译：可变燃烧速率/可变燃烧时间降落伞火炬，适用于通过枪炮或榴弹炮运送至所需高度，然后点燃燃烧，强度为1.6至1.8 x 106，烛光为25至35秒，其次为第二秒以约0.8×106烛光燃烧75至35秒，并且包括具有直径约4.5英寸和约7英寸长的中空圆柱形壁的火炬箱，在一端封闭并在另一端开口，并且具有0.03英寸涂层聚酯或环氧树脂在封闭端和其内壁的三分之一至三分之二相邻于封闭端。

4. 发明授权

US3502023A Parachute-borne pyrotechnic device 失效
标题翻译： PARACHUTE-BORNE PYROTECHNIC设备
公开(公告)号：US3502023A
公开(公告)日：1970-03-24
申请号：US3502023D
申请日：1967-11-17
申请人： SCHERMULY LTD
发明人： BRITTON STANLEY
IPC分类号： F42B4/28 , F42B10/56 , F42B13/38
CPC分类号： F42B4/28 , F42B10/56

5. 发明授权

US2416957A Parachute and like flare 失效
标题翻译：降落伞和火炬
公开(公告)号：US2416957A
公开(公告)日：1947-03-04
申请号：US53850544
申请日：1944-06-02
申请人： SCHERMULY PISTOL ROCKET APP
发明人： DAVID SCHERMULY CONRAD , JAMES SCHERMULY ALFRED , CHARLES SCHERMULY
IPC分类号： F42B4/28
CPC分类号： F42B4/28

6. 发明授权

US2354025A Firearm 失效
公开(公告)号：US2354025A
公开(公告)日：1944-07-18
申请号：US45159142
申请日：1942-07-20
申请人： KILGORE MFG CO
发明人： JOHNSON EDWIN H
IPC分类号： F41C3/02 , F42B4/28
CPC分类号： F42B4/28 , F41C3/02

7. 发明授权

US1964016A Flare 失效
标题翻译：耀斑
公开(公告)号：US1964016A
公开(公告)日：1934-06-26
申请号：US66511333
申请日：1933-04-08
申请人： SAMUEL WILEY
发明人： SAMUEL WILEY
IPC分类号： F42B4/28
CPC分类号： F42B4/28

8. 发明授权

US10591266B2 Distress flare 有权
公开(公告)号：US10591266B2
公开(公告)日：2020-03-17
申请号：US16222233
申请日：2018-12-17
申请人： COMMISSARIAT A L'ENERGIE ATOMIQUE ET AUX ENERGIES ALTERNATIVES
发明人： Boris Berseneff , Daniel Chatroux
IPC分类号： F42B12/42 , F42B12/36 , G08B5/00 , F42B4/28 , F42B4/26
摘要： A distress flare including a cartridge including two ends connected by a side surface; activation device intended to expel the cartridge into the sky; an inflatable shell, covering the side surface, suitable for being deployed under the effect of deploying device and of diffusing the visible light; illuminating device powered by a battery and capable of emitting visible light, the illuminating device being arranged on the side surface.

9. 发明授权

US09829288B2 Retention clips for safety mechanisms of illumination flares and safety mechanisms 有权
公开(公告)号：US09829288B2
公开(公告)日：2017-11-28
申请号：US14857207
申请日：2015-09-17
申请人： Orbital ATK, Inc.
发明人： Mark A. Thompson , Steven M. Robbins , Michael Geslin
IPC分类号： F42B4/28
CPC分类号： F42B4/28 , F42C7/00
摘要： Retention clips for safety mechanisms of illumination flares include an abutment surface configured for abutment of an end of a rigid sleeve coupled to an igniter initiation cable and one or more protrusions configured to extend at least partially over a lateral side surface of the rigid sleeve when the rigid sleeve is retained by the clip. Safety mechanisms, illumination flares, and methods for igniting illumination flares involve such retention clips.

10. 发明申请

US20170082408A1 RETENTION CLIPS FOR SAFETY MECHANISMS OF ILLUMINATION FLARES, SAFETY MECHANISMS AND ILLUMINATION FLARES SO EQUIPPED, AND RELATED METHODS 有权
公开(公告)号：US20170082408A1
公开(公告)日：2017-03-23
申请号：US14857207
申请日：2015-09-17
申请人： Orbital ATK, Inc.
发明人： Mark A. Thompson , Steven M. Robbins , Michael Geslin
IPC分类号： F42B4/28
CPC分类号： F42B4/28 , F42C7/00
摘要： Retention clips for safety mechanisms of illumination flares include an abutment surface configured for abutment of an end of a rigid sleeve coupled to an igniter initiation cable and one or more protrusions configured to extend at least partially over a lateral side surface of the rigid sleeve when the rigid sleeve is retained by the clip. Safety mechanisms, illumination flares, and methods for igniting illumination flares involve such retention clips.

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