-
公开(公告)号：US5308715A
公开(公告)日：1994-05-03
申请号：US109216
申请日：1993-08-19
Applicant: Armand J. Aronne
Inventor： Armand J. Aronne
Abstract: An aircraft system battery pack is housed in a housing having a removable cover with a window formed therein. A pair of batteries is positioned in the housing. A lamp is mounted in the window of the cover. A pushbutton switch is mounted in the cover and manually depressible from outside the cover. Electrical conductors electrically connect the batteries in series and provide a DC output voltage and electrical conductors electrically connect the batteries in circuit with the lamp and the switch in a manner whereby manual depression of the switch closes the circuit with the batteries and the lamp. The lamp then indicates the power output condition of the batteries.
Abstract translation: 飞机系统电池组被容纳在具有其中形成有窗口的可移除盖的壳体中。 一对电池位于外壳中。 一个灯安装在盖的窗口中。 按钮开关安装在盖子上，并可从盖子的外部手动按压。 电导体串联电连接电池并提供直流输出电压，电导体将电路中的电池与灯和开关电连接，从而手动按压开关用电池和灯关闭电路。 灯然后指示电池的电源输出状态。
-
公开(公告)号：US5261630A
公开(公告)日：1993-11-16
申请号：US802376
申请日：1991-12-04
Applicant: Armand J. Aronne
Inventor： Armand J. Aronne
IPC: B64D25/10 , B64D25/11 , B64D25/112
CPC classification number: B64D25/10
Abstract: A pilot's ejection seat is propelled in an upward direction after ejection by employing a high gain signal from a radio altimeter on board an aircraft. The vertically downward high gain vector is inverted by adding 180.degree. to its phase component and providing the resultant signal to an inexpensive gyro or assembly of gyros installed in the seat. The gyros are constantly updated with information concerning the upward vertical direction and upon ejection, the gyros maintain this information for a sufficient period of time to control the ejection seat propulsion system in a manner achieving a vertically upward trajectory that will enable the pilot to clear a disabled aircraft and achieve the orientation necessary to deploy a parachute.
Abstract translation: 通过采用飞机上的无线电高度计的高增益信号，飞行员的弹射座椅在弹出后沿向上的方向被推进。 垂直向下的高增益矢量通过向其相位分量加180度而反转，并将得到的信号提供给安装在座椅中的便宜的陀螺仪或陀螺仪组件。 关于陀螺仪的上升方向的信息不断更新，并且在弹出时，陀螺仪保持该信息足够的时间以便以实现垂直向上的轨迹的方式控制喷射座椅推进系统，这将使飞行员能够清除 残疾飞机，并实现部署降落伞所必需的方向。
-
公开(公告)号：US5072727A
公开(公告)日：1991-12-17
申请号：US522500
申请日：1990-05-10
Applicant: Armand J. Aronne
Inventor： Armand J. Aronne
CPC classification number: B64D10/00 , A62B17/008 , A62B9/00 , B64G6/00 , B64D2010/002
Abstract: A multi-purpose protective garment is provided for aviators and astronauts. The garment includes inflatable pads which selectively exert pressure on the chest and abdominal areas of the wearer to counteract the effects of high altitude and high G forces which have detrimental effects upon an aviator. The garment includes an integral harness for easily attaching a hollowed backpack frame which not only contains a stored parachute but serves as an oxygen bottle for inflation of the pads as well as providing an emergency oxygen supply for the wearer.
Abstract translation: 为飞行员和宇航员提供多用途防护服。 衣服包括充气垫，其可选择性地对穿着者的胸部和腹部区域施加压力，以抵消对飞行员具有不利影响的高空和高G力的影响。 该衣服包括用于容易地连接中空的背包框架的整体式线束，该框架不仅包含存储的降落伞，而且用作氧气瓶，以用于垫的充气以及为穿着者提供紧急供氧。
-
公开(公告)号：US5036660A
公开(公告)日：1991-08-06
申请号：US482755
申请日：1990-02-21
Applicant: Armand J. Aronne
Inventor： Armand J. Aronne
CPC classification number: B64D17/32 , F42C5/00 , F42C7/12 , Y10T137/2036
Abstract: Aviator harness fittings are pneutically actuated by a central device including a pressurized gas cartridge. A firing pin may mechanically pierce the cartridge or automatic ballistic actuation of the firing pin may be accomplished by SEA WARS gas-generating devices when the latter contacts sea water. The ballistic actuation of the present invention requires two separate SEA WAR gas-generating devices to fire simultaneously thereby minimizing the chance of false actuation.
Abstract translation: 飞行员线束配件由包括加压气体盒的中央装置气密地致动。 撞击销可以机械地刺穿卡盘，或者当打击销接触海水时，SEA WARS气体发生装置可以实现撞针的自动弹道致动。 本发明的弹道致动要求两个独立的SEA WAR气体发生装置同时起动，从而使假动作的机会最小化。
-
公开(公告)号：US5318252A
公开(公告)日：1994-06-07
申请号：US35295
申请日：1993-03-22
Applicant: Armand J. Aronne
Inventor： Armand J. Aronne
IPC: B64D25/02 , B64D25/115
CPC classification number: B64D25/02
Abstract: An aviator suit is provided with a sewn-on channel of hook and eye material which encloses an elongated line that extends to a floor bracket by a shear fastener. The enclosed line prevents snagging on objects within a cockpit and becomes easily removed when the VELCRO gives way during ejection when forces are exerted upon the enclosed channel line. A simplified snubber plug is releasably clamped to the aviator's seat and becomes released after the aviator has cleared a cockpit.
Abstract translation: 飞行员套装配有钩和眼睛材料的缝合通道，其包围通过剪切紧固件延伸到地板支架的细长线。 封闭的线路防止在驾驶舱内的物体上发生阻塞，并且当力量施加在封闭的通道线上时，VELCRO在排出期间放弃时容易移除。 一个简化的缓冲塞可释放地夹在飞行员的座位上，并在飞行员清空驾驶舱之后释放。
-
Patent Agency Ranking
公开(公告)号：US5303881A
公开(公告)日：1994-04-19
申请号：US933089
申请日：1992-08-21
Applicant: Armand J. Aronne
Inventor： Armand J. Aronne
CPC classification number: B64D25/10 , B64D11/0689
Abstract: Threaded shafts engage threaded fittings at the top and bottom of a pilot's ejection seat. A motorized gear train selectively rotates the threaded shafts so as to adjust the fore-aft position of a seat while maintaining it behind a pre-designed emergency ejection path from a cockpit.
Abstract translation: 螺纹轴接合飞行员弹出座椅顶部和底部的螺纹接头。 电动齿轮系选择性地旋转螺纹轴，以便调节座椅的前后位置，同时将其保持在来自驾驶舱的预先设计的紧急排出路径的后面。
-
公开(公告)号：US5301903A
公开(公告)日：1994-04-12
申请号：US43545
申请日：1993-04-06
Applicant: Armand J. Aronne
Inventor： Armand J. Aronne
IPC: B64D25/02 , B64D25/115
CPC classification number: B64D25/02
Abstract: An assembly for restraining the upper limbs of an occupant of a seat, particularly an aircraft ejector seat, includes a storage unit which is adapted to be fixedly secured to an upper back portion of the seat. The storage houses a pair of movable cover members and first and second bladder units. The cover members and bladder units are connected by means of straps to a quick release mechanism which mates with a corresponding fitting carried by the occupant and then to a fixed structure adjacent the seat. When it is desired to deploy the restraint assembly, a tension is applied to the straps which causes the cover members to extend around opposite sides and laterally inward of the occupant's body, about respective arms of the occupant, and the bladder units to extend about the occupant's neck. The bladder units are then inflated so as to permit undesirable movement of the occupant's head.
Abstract translation: 用于限制座椅的乘员，特别是飞机顶出座椅的上肢的组件包括适于固定地固定到座椅的上后部的存储单元。 储存器容纳一对可移动盖构件和第一和第二囊单元。 盖构件和气囊单元通过带子连接到快速释放机构，其与乘员承载的相应配件相配合，然后与靠近座椅的固定结构配合。 当希望部署约束组件时，张力被施加到带子上，这使得盖构件围绕乘员的身体的相对侧和横向内侧延伸，围绕乘员的各个臂延伸，并且膀胱单元围绕 乘客的脖子 然后将膀胱单元充气以便允许乘客头部的不期望的运动。
-
公开(公告)号：US5072457A
公开(公告)日：1991-12-17
申请号：US534949
申请日：1990-06-08
Applicant: Armand J. Aronne
Inventor： Armand J. Aronne
IPC: A41D13/00
CPC classification number: A41D13/0007 , Y10S2/913
Abstract: The harness of a pilot may be custom fitted in the field by temporarily fitting front and back vest panels. The vest includes strips pre-sewn thereon which serve as passageways for harness straps. The straps are tightened and temporarily secured to the vest so as to closely conform to the torso of the pilot. The vest is then removed so that the front and back panels may be sewn together as well as the temporarily secured straps. The result is a harness/vest combination which will conform securely to the torso of a pilot.
Abstract translation: 飞行员的安全带可以通过临时安装前后背板来定制。 背心包括预先缝合在其上的条带，其用作线束带的通道。 皮带被紧固并临时固定在背心上，以便紧密地符合飞行员的躯干。 然后拆下背心，使得前面板和后面板可以缝合在一起以及临时固定的带子。 结果是一个安全地与飞行员的躯干一致的线束/背心组合。
-
公开(公告)号：US5050278A
公开(公告)日：1991-09-24
申请号：US482886
申请日：1990-02-22
Applicant: Armand J. Aronne
Inventor： Armand J. Aronne
IPC: B64D25/04
CPC classification number: B64D25/04 , Y10T24/45728
Abstract: A lock pin mechanism for a negative "G" pilot's harness includes a contoured strap lug received within a metal keeper. A lock pin passes through the keeper and engages the lug. A bearing surface exists between the lug and the keeper so that high upward forces exerted on a negative "G" strap are transmitted to the strap lug but become shared between a lug-pin interface as well as a lug-keeper interface. Thus, binding frictional engagement between pin and lug is avoided so that safe and secure withdrawal of the pin is achieved when required.
Abstract translation: 用于负“G”导向器的线束的锁定销机构包括接收在金属保持器内的轮廓带耳环。 锁销穿过保持器并与凸耳接合。 在凸耳和保持器之间存在支承表面，使得施加在负的“G”带上的高向上的力传递到带凸耳，但是在凸耳 - 针接口和凸耳接口之间共享。 因此，避免了销和凸耳之间的结合摩擦接合，从而当需要时可实现销的安全和可靠的取出。
-
10.发明授权
公开(公告)号：US4775119A
公开(公告)日：1988-10-04
申请号：US31549
申请日：1987-03-30
Applicant: Armand J. Aronne
Inventor： Armand J. Aronne
IPC: B64D17/42
CPC classification number: B64D17/42
Abstract: A backpack for a wearer in an aircraft has a rigid housing releasably storing equipment for bailing out of the wearer from the aircraft over land, water and all types of surfaces under all types of surface conditions and for survival of the wearer during, upon and after descent.
Abstract translation: 用于飞行器中的穿戴者的背包具有刚性壳体，其可释放地存储用于在所有类型的表面条件下从陆地，水和所有类型的表面上的飞机上的飞行员穿过佩戴者的设备，并且用于在，在， 血统
-
-
-
-
-
-
-
-
-
Search Results
18
records
(took 0.012 seconds)
