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1. 发明专利

JP5498727B2 Wing of aircraft 有权
公开(公告)号：JP5498727B2
公开(公告)日：2014-05-21
申请号：JP2009137464
申请日：2009-06-08
申请人：アグスタ・ソシエタ・ペル・アツイオーニ
发明人：サンティノ・パンコッティ , ダンテ・バレリオ
IPC分类号： B64C27/04 , B64C3/18 , F41A9/35
CPC分类号： F41A9/34 , B64C27/04 , B64C2025/325 , B64D7/04 , F41A9/79

2. 发明专利

JP2557813B2 失效
公开(公告)号：JP2557813B2
公开(公告)日：1996-11-27
申请号：JP30766792
申请日：1992-10-21
申请人： JOZEFU SHETSUSEI
发明人： JOZEFU SHETSUSEI
IPC分类号： F41A3/52 , F41A3/24 , F41A3/60 , F41A9/35 , F41A9/68 , F41A19/18

3. 发明专利

JPH0719796A CARRYING-CHARGING METHOD OF MISSILE AND EQUIPMENT THEREFOR 失效
公开(公告)号：JPH0719796A
公开(公告)日：1995-01-20
申请号：JP18670493
申请日：1993-06-30
申请人： JAPAN STEEL WORKS LTD
发明人： KAMIGAKI TOSHIHIKO
IPC分类号： F41A9/00 , F41A9/35 , F41A9/38
摘要： PURPOSE:To improve the operability of mobile carriage-charging by a method wherein the lower end part of a frame and a place of storage of a missile are connected together, a canister is loaded for carriage on the frame of a carrier-charger, the carrier-charger is made to run to the vicinity of a launcher, the frame of the carrier-charger and a frame of the launcher are aligned with each other and the canister is charged on the frame of the launcher. CONSTITUTION:The lower end part of a frame 6 and a place of storage of a missile are connected by a carriage auxiliary device and a canister 23 for the missile is drawn up onto and loaded for carriage on a frame 6 of a missile carrier-charger 1 by a first towing means 18 of the missile carrier-charger 1. Then, the missile carrier-charger 1 is made to run to the vicinity of a launcher 25 and the frame 6 of the missile carrier-charger 1 and a frame 30 of the launcher 25 are aligned with each other by regulation in elevation. The canister 23 for the missile is charged on the frame 30 of the launcher 25 from the frame 6 of the missile carrier-charger 1 by the first drawing means 18.

4. 实用新型

JPH0356092U 失效
公开(公告)号：JPH0356092U
公开(公告)日：1991-05-29
申请号：JP11211189
申请日：1989-09-27
IPC分类号： F41A9/01 , F41A9/35 , F41A9/38 , F41A9/78

5. 实用新型

JP3150763U モデルガン銃身の拡張式デトネーターと薬莢失效
标题翻译：扩大模型枪管雷管和墨盒
公开(公告)号：JP3150763U
公开(公告)日：2009-06-04
申请号：JP2008009383
申请日：2008-12-26
申请人：有限会社タニオ・コバ
发明人：太三小林 , 太三小林
IPC分类号： F41A9/35
摘要：【課題】拡張可能なデトネーターによって安定したブローバック作動を可能にすると伴に、軽量薬莢により安全なブローバックモデルガンを提供する。【解決手段】銃身内に設置されているデトネーターの頭部を、発火した玩具火薬の圧力を受けた時のみ拡張する弾性材料をもたせ、発火時に拡張して薬莢内面と密着してスライドの後退力を増大させ、頭部が拡張していない時には薬莢内面との間隙を維持し、この作用により銃身内への薬莢の給弾時にはこの間隙により円滑な給弾効果をもたらすことを特徴とする。デトネーター頭部の拡張機能によって軽量なプラスチック成形薬莢の使用が可能となり、モデルガンのブローバックによって排出された薬莢が、近くのガラスや照明器具等を破損する事故も回避できる。【選択図】図1
摘要翻译：本发明公开了伴随启用反吹操作由扩张雷管稳定，提供安全反吹modelguns轻型弹壳。雷管的头部，其被安装在所述桶，点燃记忆弹性材料当受到压力时玩具炸药仅延伸，在与墨盒内表面紧密接触的滑动的缩回力延伸的点火增加，当磁头不延伸保持盒壳体内表面之间的间隙，在喂食的子弹盒插入由动作筒，其特征在于，导致平滑由该间隙子弹饲料效果的时间。由雷管头的扩展用重量轻的塑料模塑盒壳体的使得能够通过回吹模拟枪喷出弹壳，事故能够避免损坏附近玻璃和照明设备等。点域1

6. 发明专利

JP4017090B2 Bullet species automatic recognition device of Tarenso type launcher 失效
标题翻译：空值
公开(公告)号：JP4017090B2
公开(公告)日：2007-12-05
申请号：JP17623298
申请日：1998-06-23
申请人：株式会社アイ・エイチ・アイ・エアロスペース
发明人：田英夫橘 , 川智孝石
IPC分类号： F41A9/35 , F41A9/53 , F41F1/08 , F41F7/00 , G06K7/00

7. 实用新型

JPH0722630Y2 失效
公开(公告)号：JPH0722630Y2
公开(公告)日：1995-05-24
申请号：JP11211189
申请日：1989-09-27
IPC分类号： F41A9/01 , F41A9/35 , F41A9/38 , F41A9/78

8. 发明专利

JPH06137786A TANDEM BOLT ACTION MAGAZINE RIFLE 失效
公开(公告)号：JPH06137786A
公开(公告)日：1994-05-20
申请号：JP30766792
申请日：1992-10-21
申请人： JIYOZEFU SHIETSUSEI
发明人： JIYOZEFU SHIETSUSEI
IPC分类号： F41A3/52 , F41A3/24 , F41A3/60 , F41A9/35 , F41A9/68 , F41A19/18
摘要： PURPOSE: To obtain a bolt action assembly adapted to fit in the receiver of a double-barrel fire-arm, such as a rifle or a shotgun. CONSTITUTION: A bolt assembly comprises a bolt body 70 which connects to first and second breech bolts, and which also couples to a bolt collar 72. The bolt collar 72 has a bolt handle 74 for operating the bolt action assembly 10. The bolt body 70 and breech bolts have recesses for accepting first and second firing pin assemblies 90. The firing pin assemblies include first and second cocking pieces, which are both cocked by means included in the bolt collar 72. Once cocked, the cocking pieces can be released independently of each other for firing using trigger means. Pulling the bolt action assembly 10 rearwards ejects the fired cartridge through an ejection port on the receiver. During the forward travel, the bolt action assembly 10 reloads the firing chambers with cartridges from the magazine. The receiver also includes a cartridge injector port coupled to the magazine.

9. 发明专利

JP2010042799A Aircraft wing 有权
标题翻译：飞机票
公开(公告)号：JP2010042799A
公开(公告)日：2010-02-25
申请号：JP2009137464
申请日：2009-06-08
申请人： Agusta Spa , アグスタ・ソシエタ・ペル・アツイオーニ
发明人： PANCOTTI SANTINO , BALLERIO DANTE
IPC分类号： B64C27/04 , B64C3/18 , F41A9/35
CPC分类号： F41A9/34 , B64C27/04 , B64C2025/325 , B64D7/04 , F41A9/79
摘要： PROBLEM TO BE SOLVED: To provide a wing which is designed inexpensively and easily so as to increase ammunition fed in a turret without deteriorating aerodynamic characteristics of a helicopter.
SOLUTION: The wing 4 for an aircraft having at least one weapon, and a feed duct 13 for feeding the ammunition to the weapon in the form of a belt 10 is provided. The wing 4 has a compartment 20 for housing a portion 54 of the belt 10 and connectable to a loading opening of the feed duct 13.
COPYRIGHT: (C)2010,JPO&INPIT

10. 发明专利

JP3115372B2 失效
公开(公告)号：JP3115372B2
公开(公告)日：2000-12-04
申请号：JP25374391
申请日：1991-10-01
IPC分类号： F41A9/31 , F41A9/35 , F41A9/74

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