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1. 发明授权

US08434714B2 Aircraft landing gear 有权
标题翻译：飞机起落架
公开(公告)号：US08434714B2
公开(公告)日：2013-05-07
申请号：US12929566
申请日：2011-02-01
申请人： Andrija Ekmedzic
发明人： Andrija Ekmedzic
IPC分类号： B64C25/14
CPC分类号： B64C25/10 , B64C25/16 , Y02T50/44
摘要： An aircraft landing gear for an aircraft having an engine, an outer surface, a cavity formed in the outer surface, a cover arranged to close the cavity, the landing gear being arranged to be movable between a stowed configuration, in which it is stowed in the cavity, and a deployed configuration, the landing gear comprising an engine debris guard panel arranged to inhibit tire propelled debris striking the engine whilst the landing gear is in the deployed configuration, wherein the guard panel is arranged to form at least a part of the cover when the landing gear is in the stowed configuration.
摘要翻译：一种用于具有发动机，外表面，形成在外表面中的空腔的飞机的飞机起落架，布置成关闭空腔的盖子，起落架布置成可在其被收起在其中的收起的构型之间移动所述空腔和展开构型，所述起落架包括发动机碎片防护板，所述发动机碎片防护板布置成在所述起落架处于所述展开构型时禁止轮胎推进碎片撞击所述发动机，其中所述防护板被布置成形成所述防护板的至少一部分当起落架处于收起配置时盖住。

2. 发明申请

US20130048783A1 LANDING GEAR ATTACHMENT 有权
标题翻译：接地齿轮附件
公开(公告)号：US20130048783A1
公开(公告)日：2013-02-28
申请号：US13569528
申请日：2012-08-08
申请人： Andrija Ekmedzic , Mario Straccia , Philip Jones
发明人： Andrija Ekmedzic , Mario Straccia , Philip Jones
IPC分类号： B64C25/10
CPC分类号： B64C25/04
摘要： A landing gear attachment apparatus (100) hasa landing gear side bearing retention arrangement (104) connected to an aircraft side attachment apparatus (102), held together by a series of fuse pins. The interaction between a fuse pin carrier and a trunnion block varies the amount of load required to separate the landing gear from the fuselage depending on the direction of the load.
摘要翻译：起落架附接装置（100）具有连接到飞行器侧连接装置（102）的起落架侧轴承保持装置（104），其通过一系列熔丝销保持在一起。保险丝销托架和耳轴座之间的相互作用根据负载方向改变将起落架与机身分离所需的负载量。

3. 发明申请

US20110186680A1 Aircraft landing gear 有权
标题翻译：飞机起落架
公开(公告)号：US20110186680A1
公开(公告)日：2011-08-04
申请号：US12929566
申请日：2011-02-01
申请人： Andrija Ekmedzic
发明人： Andrija Ekmedzic
IPC分类号： B64C25/16 , B64C25/10
CPC分类号： B64C25/10 , B64C25/16 , Y02T50/44
摘要： An aircraft landing gear for an aircraft having an engine, an outer surface, a cavity formed in the outer surface, a cover arranged to close the cavity, the landing gear being arranged to be movable between a stowed configuration, in which it is stowed in the cavity, and a deployed configuration, the landing gear comprising an engine debris guard panel arranged to inhibit tyre propelled debris striking the engine whilst the landing gear is in the deployed configuration, wherein the guard panel is arranged to form at least a part of the cover when the landing gear is in the stowed configuration.
摘要翻译：一种用于具有发动机，外表面，形成在外表面中的空腔的飞机的飞机起落架，布置成关闭空腔的盖子，起落架布置成可在收起的构造之间移动，收起的构造被存放在其中所述空腔和展开构型，所述起落架包括发动机碎片防护板，所述发动机碎片防护板布置成在所述起落架处于所述展开构型时禁止轮胎推进碎片撞击所述发动机，其中所述防护板被布置成形成所述防护板的至少一部分当起落架处于收起配置时盖住。

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