公开(公告)号：US20070007384A1

公开(公告)日：2007-01-11

申请号：US11304449

申请日：2005-12-14

Applicant: John Sliwa

Inventor： John Sliwa

IPC: B64B1/02

CPC classification number: F41H13/005 ,  B64D45/0015 ,  B64D45/0036 ,  B64D45/0053 ,  B64D2201/00 ,  F41H11/00 ,  F41H13/0006

Abstract: Various novel means are provided to neutralize determined if not fanatical attackers, and in most embodiments to proactively prevent harm to most or all innocent bystanders. In one example, a flyable unmanned craft is provided, which is useful for disrupting an armed enemy from shooting friendlies. In another example, a system offering protection to victims of any one or more of terrorism, criminal behavior and disasters is provided. In yet another example, an inflatable protective device is provided, having at least one armored, puncture-resistant or projectile-resistant material or layer facing or presented to a threat which is in turn mounted upon an underlying shock-absorbing member. In a still further example, a system is provided that is capable of target-designating or tagging a potentially or actually harmful person, possibly located among innocent persons or potential victims, for neutralizing or lethal action.

Abstract translation: 提供各种新颖的手段来中和确定的不是狂热的攻击者，并且在大多数实施例中主动地防止对大多数或所有无辜旁观者的伤害。 在一个例子中，提供了一个可飞行的无人驾驶飞行器，这对于打击武装敌人来拍摄友谊赛很有用。 另一个例子中，提供了向恐怖主义，犯罪行为和灾害中的任何一种或多种受害者提供保护的制度。 在另一个示例中，提供了一种可充气的保护装置，其具有至少一个面向或呈现为威胁的装甲，抗穿刺或弹丸抵抗的材料或层，所述材料或层又依次安装在下面的减震构件上。 在另一个例子中，提供了一种系统，其能够对可能位于无辜者或潜在受害者中的潜在或实际有害的人进行目标指定或标记，以进行中和或致命的行动。

公开(公告)号：US20060249629A1

公开(公告)日：2006-11-09

申请号：US11044623

申请日：2005-01-28

Applicant: Yoo-I Lee

Inventor： Yoo-I Lee

IPC: B64D17/00

CPC classification number: B64D17/80 ,  B64D25/00 ,  B64D25/18 ,  B64D2201/00

Abstract: Emergency system of Airplane parachute with cusion means if airplane needs make a stop on the way or need temporary Landing on the way, This system work for Airplane can landing at Emergency on flying tinm. This parachute system are bringing Airplane from Flyingtime to Emergency Landing. and The Cusion system are makes Airplane Emergency Landing more safety. The Palachute string joint useing revolving, flexible and elasticy ly material. These system are Airplane can Landing on The Emergency way more Safety.

Abstract translation: 飞机降落伞的紧急系统意味着飞机需要在途中停下或需要临时着陆，飞机上的这个系统可以在紧急情况下飞行。 这个降落伞系统将飞机从飞行时间带到紧急着陆。 而Cusion系统使飞机紧急着陆更加安全。 使用旋转，弹性和弹性材料的Palachute弦接头。 这些系统是飞机可以在紧急情况下登陆更安全。

公开(公告)号：US06896224B1

公开(公告)日：2005-05-24

申请号：US10807577

申请日：2004-03-18

Applicant: John L. Goodwin

Inventor： John L. Goodwin

IPC: B60R21/16 ,  B60R21/206 ,  B64D25/10 ,  B64C1/10

CPC classification number: B64D25/10 ,  B60R2021/23176 ,  B64D2201/00

Abstract: A method for mitigating toe strike in a cockpit of an aircraft includes providing an airbag module attached to an instrument console located in the cockpit of the aircraft; releasing an airbag from the airbag module after an ejection sequence begins; using the airbag to protect a pilot's lower limbs from striking the instrument console as the pilot begins ejecting.

Abstract translation: 一种用于减轻飞机驾驶舱中的脚趾撞击的方法包括提供安装在位于飞行器驾驶舱中的仪表控制台的气囊模块; 在喷射顺序开始之后，从气囊模块释放气囊; 当飞行员开始喷射时，使用安全气囊来保护飞行员的下肢免于撞击仪表控制台。

公开(公告)号：US20020105219A1

公开(公告)日：2002-08-08

申请号：US09778498

申请日：2001-02-07

Inventor： Michael C. Riley ,  Willard F. Hagan

IPC: A47C007/02

CPC classification number: B64D11/06205 ,  B60R21/207 ,  B60R21/268 ,  B60R21/272 ,  B60R2021/0093 ,  B64D11/0649 ,  B64D25/04 ,  B64D25/06 ,  B64D2201/00 ,  Y02T50/46

Abstract: A passive restraint system in an aircraft utilizing a seat structure of the aircraft to store a source of pressurized gas or solid fuel necessary to expand the passive restraint is disclosed. The seat structure of the aircraft comprises multiple hollow tubes, and these hollow tubes can be utilized to either store pressurized gas or solid fuel directly, or to house a vessel that stores pressurized gas or solid fuel. Thus, no additional aircraft seat space is required to house a pressurized gas vessel. By using the existing seat structure to house the source of pressurized gas or solid fuel, significant space and weight savings can be realized, both of which are important factors in aircraft seat design.

Abstract translation: 公开了一种利用飞机的座椅结构来存储扩展被动约束所需的加压气体源或固体燃料源的飞行器中的被动约束系统。 飞机的座椅结构包括多个中空管，并且这些中空管可用于直接存储加压气体或固体燃料，或者容纳存储加压气体或固体燃料的容器。 因此，不需要额外的飞机座椅空间来容纳加压气体容器。 通过使用现有的座椅结构来容纳加压气体或固体燃料源，可以实现显着的空间和重量节省，这两者都是飞机座椅设计的重要因素。

公开(公告)号：US06338456B1

公开(公告)日：2002-01-15

申请号：US09671861

申请日：2000-09-28

Applicant: Renee Cairo-Iocco ,  John P. Wehrle

Inventor： Renee Cairo-Iocco ,  John P. Wehrle

IPC: B64D1900

CPC classification number: B64D25/00 ,  B64C25/30 ,  B64D2201/00

Abstract: Inflation of impact absorbing bags is effected in time delayed relation to selective jettisoning of damaged landing gear on a helicopter prior to landing for replacement of the landing gear by the bags, without puncture thereof by the landing gear being jettisoned.

Abstract translation: 冲击吸收袋的通货膨胀与时间延迟相关，在降落之前在直升机上选择性地丢弃起落架，以便由起重装置更换起落架，而不会被起落架抛出。

公开(公告)号：US06217066B1

公开(公告)日：2001-04-17

申请号：US09524370

申请日：2000-03-14

Applicant: Daniel E. Coleman ,  Rick A. Adkisson ,  Michael C. Riley

Inventor： Daniel E. Coleman ,  Rick A. Adkisson ,  Michael C. Riley

IPC: B60R2126

CPC classification number: B64D25/00 ,  B60R21/26 ,  B60R21/2644 ,  B60R2021/0093 ,  B60R2021/26058 ,  B60R2021/26094 ,  B60R2021/2612 ,  B60R2021/2633 ,  B64D2201/00 ,  Y10T137/1714

Abstract: Apparatus for use in passenger inflatable air-bag safety systems for preventing activation of an activator inflator from causing premature activation of any inflator not yet activated by system programming. The apparatus includes structure for isolating the pressure releasing construction from shock waves created when an inflator is activated and takes the form of mechanical barriers that isolate each inflator release structure from exposure to shock waves.

Abstract translation: 用于乘客充气安全气囊安全系统的装置，用于防止活化器充气机的活化，引起尚未通过系统编程激活的任何充气机的过早活化。 该装置包括用于隔离压力释放构造与在充气机被启动时产生的冲击波的结构，并且采取将每个充气机释放结构与暴露于冲击波隔离的机械障碍物的形式。

公开(公告)号：US5899414A

公开(公告)日：1999-05-04

申请号：US906116

申请日：1997-07-25

Applicant: Jose G. Duffoo

Inventor： Jose G. Duffoo

IPC: B64D17/80 ,  B64D25/12

CPC classification number: B64D25/12 ,  B64D17/80 ,  B64D2201/00

Abstract: An aircraft rescue system is provided including a plurality of parachutes coupled to a tail of the aircraft, a midsection of the aircraft, and a nose of the aircraft. The parachutes are adapted to deploy upon the actuation thereof. A control mechanism is included for allowing a pilot to manually actuate the parachutes.

Abstract translation: 提供了一种飞机救援系统，包括耦合到飞行器尾部的多个降落伞，飞机的中部和飞机的鼻子。 降落伞适于在其致动时展开。 包括用于允许飞行员手动致动降落伞的控制机构。

公开(公告)号：US5560568A

公开(公告)日：1996-10-01

申请号：US261901

申请日：1994-06-15

Applicant: Hugh Schmittle

Inventor： Hugh Schmittle

IPC: B64C3/38 ,  B64C29/00 ,  B64C29/02 ,  B64C39/02 ,  B64C39/04

CPC classification number: B64C29/02 ,  B64C29/0033 ,  B64C3/385 ,  B64C39/024 ,  B64C39/04 ,  B64C2201/044 ,  B64C2201/046 ,  B64C2201/084 ,  B64C2201/086 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/182 ,  B64C2201/187 ,  B64D2201/00 ,  Y10S446/901

Abstract: Apparatus and method for recovering and arresting an aircraft on a floating platform is disclosed. The aircraft has a fuselage, a wing, and a source of propulsion for propelling the aircraft in flight. During landing approach, an inflatable cushion attached to the fuselage is deployed below the fuselage via inflation. In the inflated condition, a fastening material disposed on a downward facing surface of the cushion is thereby adapted to adhesively contact the floating platform deck so that the forward motion of the aircraft is slowed and arrested. In the preferred embodiment, the fastening material is one of male or female VELCRO.RTM. which is adapted to mate with corresponding VELCRO.RTM. material covering the platform deck.

Abstract translation: 公开了一种用于在浮动平台上恢复和拦截飞行器的装置和方法。 这架飞机有一个机身，一个机翼和一个推进的来源，用于在飞行中推进飞机。 在着陆过程中，通过充气将附着在机身上的充气垫部署在机身的下方。 在充气状态下，设置在缓冲垫的向下的表面上的紧固材料因此适于与浮动平台甲板粘合地接触，使得飞行器的向前运动变慢并且被阻止。 在优选实施例中，紧固材料是男性或女性VELCRO TM之一，其适于与覆盖平台甲板的相应的VELCRO TM材料配合。

公开(公告)号：US5556056A

公开(公告)日：1996-09-17

申请号：US287386

申请日：1994-08-08

Applicant: Robert C. Kalberer ,  Kevin W. Kreutzer ,  Dan Goor

Inventor： Robert C. Kalberer ,  Kevin W. Kreutzer ,  Dan Goor

IPC: B60R21/00 ,  B60R21/16 ,  B60R21/203 ,  B64D25/02 ,  B64D25/00

CPC classification number: B64D25/02 ,  B60R2021/0093 ,  B60R2021/23107 ,  B64D2201/00

Abstract: An airbag assembly is positioned relative to an aircraft control yoke in a manner to minimize the application of an undesired force to the control yoke when the airbag assembly is inflated. A disc-shaped airbag assembly is horizontally rod-supported from an aircraft's instrument panel so as to surround the aircraft's horizontally extending control yoke and so as to be independent mechanically thereof. The rods that support the airbag assembly may be spring biased to a quiescent position, and may then be of the telescoping type to accommodate full inward movement of the control yoke as the aircraft's pitch attitude is controlled. In a alternate embodiment of the invention, the airbag assembly is mounted on the ceiling of the aircraft, generally above and somewhat forward of the pilot, the airbag assembly being of a size when inflated whereby the pilot is protected from impact with the instrument panel, and yet subsequent operation of the control yoke by the pilot is not prevented by obstruction of the control yoke.

Abstract translation: 安全气囊组件相对于飞行器控制轭设置，以便当气囊组件被充气时，最小化对控制轭的不期望的力的施加。 盘形安全气囊组件从飞行器的仪表板水平地杆支撑，以便围绕飞机的水平延伸的控制轭并且以机械方式独立地安装。 支撑安全气囊组件的杆可以被弹簧偏置到静止位置，然后可以是伸缩型，以适应控制轭的完全向内运动，因为控制飞机的俯仰姿态。 在本发明的替代实施例中，安全气囊组件安装在飞行器的天花板上，大体上在飞行员的上方并稍微向前，安全气囊组件具有膨胀的尺寸，从而防止飞行员受到仪表板的撞击， 并且由控制轭的阻塞不能防止由引导件控制轭的后续操作。

公开(公告)号：US5547149A

公开(公告)日：1996-08-20

申请号：US242936

申请日：1994-05-16

Applicant: Robert C. Kalberer ,  Dan Goor

Inventor： Robert C. Kalberer ,  Dan Goor

IPC: B60R21/01 ,  B60R21/16 ,  B64D25/00

CPC classification number: B64D25/00 ,  B64D2201/00

Abstract: Airbags are positioned in a general aviation aircraft cockpit relative to a control yoke, a pilot, and a front seat passenger. Airbag actuation is controlled by a adaptive programmable controller such as a microcomputer. Airbag actuation is based upon information that the controller receives from multiple acceleration sensors. The outputs of the acceleration sensors are subjected to thresholding techniques, such as output signal weighting and/or majority voting. A programmable threshold is adaptively established for the controller based upon unique aircraft parameters, such as weight, altitude, angle of attack, ground and/or air speed, etc. The controller ignores all acceleration sensor inputs that do not meet this adaptive threshold. Thus, airbag actuation takes place only when a sufficient acceleration event occurs concurrently with the presence or absence of defined aircraft parameters that establish a proper threshold for the acceleration event. Airbag inflation includes a controllable delay that is used to customize airbag inflation to particular aircraft parameters, such as ground/air speed and weight.

Abstract translation: 安全气囊位于通用航空飞机驾驶舱内，相对于控制架，飞行员和前排乘客。 气囊致动由诸如微型计算机的自适应可编程控制器控制。 安全气囊致动基于控制器从多个加速度传感器接收的信息。 对加速度传感器的输出进行阈值处理，例如输出信号加权和/或多数投票。 基于独特的飞机参数（例如重量，高度，迎角，地面和/或空气速度等），为控制器自适应地建立可编程阈值。控制器忽略不符合该自适应阈值的所有加速度传感器输入。 因此，仅当足够的加速度事件与确定加速事件的适当阈值的定义的飞行器参数的存在或不存在时才发生安全气囊致动。 安全气囊充气包括可控制的延迟，用于将气囊充气量定制为特定的飞机参数，例如地面/空气速度和重量。