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51. 发明公开

EP0683097A2 Link apparatus 失效转让
标题翻译： Link设备
公开(公告)号：EP0683097A2
公开(公告)日：1995-11-22
申请号：EP95303198.6
申请日：1995-05-12
申请人： BRITISH AEROSPACE PUBLIC LIMITED COMPANY
发明人： Spencer-Purvis, Gary, c/o British Aerospace Def.
IPC分类号： B64D25/10
CPC分类号： B64D25/10 , Y10T137/1669 , Y10T137/86678
摘要： An extendable/retractable link apparatus 10 defines a fluid passage therethrough and may be connected between two relatively moveable components, e.g. an aircraft ejector seat and the adjacent fixed airframe, so that, when there is relative movement within pre-set limits, there is no significant displacement of fluid and no significant pressure force generated. The apparatus comprises a body 12 defining a fluid inlet/outlet port 16 and slidably receiving a piston 18 having a central bore which defines a fluid inlet/outlet port 24. The fluid passage is defined between said inlet and outlet ports 16 and 24. Relative movement of the piston 18 and body 12 does not cause significant displacement of the fluid into or out of the fluid passage.
摘要翻译：可伸出/可伸缩的连杆装置10限定了穿过其中的流体通道并且可以连接在两个相对可移动的部件之间，例如，飞机弹射座和相邻的固定机身，从而当在预设的极限内有相对运动时，流体没有明显的位移并且没有产生显着的压力。该设备包括限定流体入口/出口端口16并且可滑动地接收具有限定流体入口/出口端口24的中心孔的活塞18的主体12.流体通道限定在所述入口和出口端口16和24之间。相对活塞18和主体12的运动不会导致流体进入或流出流体通道的显着位移。

52. 发明公开

EP0590688A1 Power source for an electroballistic sequencing system 失效
标题翻译： Energieversorgungfürein elektro-ballistisches Sequenzsystem。
公开(公告)号：EP0590688A1
公开(公告)日：1994-04-06
申请号：EP93116025.3
申请日：1993-10-04
申请人： GRUMMAN AEROSPACE CORPORATION
发明人： Aronne, Armand J.
IPC分类号： B64D25/10
CPC分类号： B64D25/10 , Y10T307/50 , Y10T307/826
摘要： Start-up electrical power modules (10) are utilized in electroballistic sequencing systems for initiating the ballistic sequence necessary for seat and canopy ejection in military aircraft. The power modules (10) utilize aircraft power to initiate the ballistic sequence necessary for ejection of the pilot or pilots. The power module (10) also comprises two independent internal power supplies (18,20) as back-up power sources in the event of total aircraft power failure. The power modules (10) are activated by the manual pulling action of an actuation shaft (22) by the pilot or by the automatic pushing action of the actuation shaft (22) by a piston once the pilot initiates the ejection sequence. Once the actuation shaft (22) is pulled into an armed position, dual switches (14,16) are activated thereby supplying electrical power from the aircraft or from the back-up power sources (18,20) to a signal conditioner and controller (12). The signal conditioner and controller (12) processes the signals and outputs a single direct current signal to a ballistic sequencer (52).
摘要翻译：启动电力模块（10）用于电子竞技排序系统中，用于启动军用飞机中座椅和机盖弹出所需的弹道序列。电力模块（10）利用飞行器电力来发起飞行员或飞行员弹出所需的弹道序列。在整个飞机停电的情况下，功率模块（10）还包括作为备用电源的两个独立的内部电源（18,20）。一旦驾驶员启动喷射顺序，动力模块（10）通过驾驶员的致动轴（22）的手动拉动动作或者由致动轴（22）的自动推动动作来激活。一旦致动轴（22）被拉入到备用位置，双重开关（14,16）被激活，从而将来自飞行器或备用电源（18,20）的电力提供给信号调节器和控制器 12）。信号调节器和控制器（12）处理信号并将一个直流信号输出到弹道定序器（52）。

53. 发明公开

EP0451438A1 Ejection seats for military aircraft 失效
标题翻译：军用飞机的弹射座椅
公开(公告)号：EP0451438A1
公开(公告)日：1991-10-16
申请号：EP91100151.9
申请日：1991-01-04
申请人： BRITISH AEROSPACE PUBLIC LIMITED COMPANY
发明人： Ash, Geoffrey James, British Aerospace , Valentine, Timothy, British Aerospace
IPC分类号： B64D25/10 , B64D25/06
CPC分类号： B64D25/10 , B64D11/0616 , B64D11/06395 , B64D11/0689 , B64D25/06
摘要： A reclining ejection seat (1) for an aircraft which includes an arm support (7) composed of two parts (8,10) which are moveable fore and aft. A first part (8) carries flying controls (9) and is adjustable for reach. A second part (10) which is adjustable for comfort, locates the elbow of a pilot (11) and supports his forearm. The arm support (7) permits the pilot (11) to maintain adequate control over his arm movements even when the aircraft is carrying out very high speed manoeuvres.
摘要翻译：一种用于飞机的倾斜弹射座椅（1），其包括由可前后移动的两个部件（8,10）组成的臂支架（7）。第一部分（8）带有飞行控制装置（9），并且可以调节到达范围。第二部分（10）可调节舒适度，定位飞行员（11）的肘部并支撑其前臂。即使飞机正在进行非常高速的操纵，臂支架（7）也允许飞行员（11）保持对其手臂运动的适当控制。

54. 发明公开

EP0361369A3 Head support/spine offloading ejection seat insert 失效
标题翻译：头部支撑/脊柱卸载射出座椅插件
公开(公告)号：EP0361369A3
公开(公告)日：1990-09-19
申请号：EP89117690.1
申请日：1989-09-25
申请人： ROCKWELL INTERNATIONAL CORPORATION
发明人： Adams, William J. , Zegler, Robert E. , Monson, Conrad B.
IPC分类号： B64D25/02 , B64D25/10
CPC分类号： A42B3/0473 , B64D25/02 , B64D25/10
摘要： A seat insert insertable within the existing seat of a vehicle for maintaining a crew member of the vehicle in a forward posture during high G acceleration. An elongated head support member is provided for supporting the crew member's head during a forward leaning posture. A back plate assembly including at least one back plate is connected to the head support member for supporting the spine in its natural curvature. Means being connected to the back plate assembly are provided for pivoting the back plate assembly forward relative to the seat of the vehicle. Means are provided for transfering any G-induced weight from the spine to the back plate assembly and ultimately to the existing seat of the vehicle. The head support member is restrained in such a manner so as to maintain the crew member's head in an "eyes up" attitude during a forward lean. The seat insert reduces the risk of spinal injury by off-loading the pilot's spine and supporting the spine in its natural curvature, thereby preventing harmful bending of the spine and non-uniform load distribution across individual vertebrae interfaces.

55. 发明公开

EP0361369A2 Head support/spine offloading ejection seat insert 失效
标题翻译： Einsatzfüreinen Schleuersitz mit einerKopfstützebzw. Rückgratentlastung。
公开(公告)号：EP0361369A2
公开(公告)日：1990-04-04
申请号：EP89117690.1
申请日：1989-09-25
申请人： ROCKWELL INTERNATIONAL CORPORATION
发明人： Adams, William J. , Zegler, Robert E. , Monson, Conrad B.
IPC分类号： B64D25/02 , B64D25/10
CPC分类号： A42B3/0473 , B64D25/02 , B64D25/10
摘要： A seat insert insertable within the existing seat of a vehicle for maintaining a crew member of the vehicle in a forward posture during high G acceleration. An elongated head support member is provided for supporting the crew member's head during a forward leaning posture. A back plate assembly including at least one back plate is connected to the head support member for supporting the spine in its natural curvature. Means being connected to the back plate assembly are provided for pivoting the back plate assembly forward relative to the seat of the vehicle. Means are provided for transfering any G-induced weight from the spine to the back plate assembly and ultimately to the existing seat of the vehicle. The head support member is restrained in such a manner so as to maintain the crew member's head in an "eyes up" attitude during a forward lean. The seat insert reduces the risk of spinal injury by off-loading the pilot's spine and supporting the spine in its natural curvature, thereby preventing harmful bending of the spine and non-uniform load distribution across individual vertebrae interfaces.
摘要翻译：座椅插入件可插入车辆的现有座椅内，用于在高G加速期间将车辆的乘员组件保持在向前姿态。提供了一种细长的头部支撑构件，用于在向前倾斜姿势期间支撑船员的头部。包括至少一个背板的背板组件连接到头部支撑构件，用于将脊柱支撑在其自然曲率中。设置连接到背板组件的装置用于相对于车辆的座椅向前枢转背板组件。提供了用于将任何G引起的重量从脊柱传递到后板组件并且最终传递到车辆的现有座椅的装置。头部支撑构件以这样的方式被限制，以便在前倾时保持机组人员的头部呈“向上”姿态。座椅插件通过卸载飞行员的脊柱并将脊柱支撑在其自然曲率中，从而降低脊柱损伤的风险，从而防止脊柱的有害弯曲和跨不同椎骨界面的不均匀载荷分布。

56. 发明公开

EP0354276A1 Microprocessor controlled post ejection sequencer 失效
标题翻译： Mikroprozessor zur Ablaufsteuerung nach dem Herausschleudern。
公开(公告)号：EP0354276A1
公开(公告)日：1990-02-14
申请号：EP88307293.6
申请日：1988-08-08
申请人： UNIVERSAL PROPULSION COMPANY, Inc.
发明人： Peck, Walter R. , Duncan, James W.
IPC分类号： B64D25/10 , B64D17/58 , B64D17/56
CPC分类号： B64D25/10
摘要： A self contained, self powered microprocessor controlled aircraft ejection seat escape parachute deployment sequencer which can handle problems caused by high altitudes into the stratosphere and by high speeds above Mach 1, and which will deploy the parachute, based on seat mounted pitot tube (41) and ambient pressure readings (35, 36, 37) plus stored data (57), when speed and altitude are at human physiologically acceptable levels. Many failsafes to cope with unusual conditions, and additional features are also included.
摘要翻译：一个自包含的自动微处理器控制的飞机弹射座椅逃生降落伞部署音序器，可以处理由高空飞行到平流层和高于马赫数1的高速度引起的问题，并且将基于座椅安装的皮托管（41）部署降落伞，和环境压力读数（35,36,37）加存储数据（57），当速度和高度处于人类生理学上可接受的水平时。许多难以应付的异常情况，还包括其他功能。

57. 发明公开

EP0256425A3 Life-threat assessment and control command for aircrew escape systems 失效
标题翻译：飞机自行车系统的生命危险评估和控制指令
公开(公告)号：EP0256425A3
公开(公告)日：1989-04-05
申请号：EP87111282.7
申请日：1987-08-04
申请人： THE BOEING COMPANY
发明人： Trikha, Arun K.
IPC分类号： B64D25/10
CPC分类号： B64D25/10
摘要： A crewmember (12) is positioned within an ejection seat or other escape device (10). The escape device (10) is ejected from the aircraft or other flying vehicle when it is desired to effect an escape. At the start of ejection, the altitude, sink rate and roll angle of the escape device (10) are determined, by appropriate sensors (128, 132). A microprocessor (66) is used for dividing the altitude by the sink rate to obtain a first time value. The microprocessor (66) is used to divide the roll angle by a desired rate of roll angle correction, to obtain a second time value. The second time value is subtracted from the first time value to obtain a third time value, t c . In response to t c being larger than a predetermined value, the microprocessor (66) controls separation to subject the crewmember (12) to a relatively low injury risk level. In response to t c being smaller than said predetermined time value, the microprocessor (66) controls separation to occur faster, attended by the crewmember (12) being subjected to a higher injury risk level.

58. 发明公开

EP0292586A1 Apparatus for adjustably mounting an ejection seat in an aircraft 失效
标题翻译： Verstellbare BefestigungsanlagefürFlugzeugschleudersitze。
公开(公告)号：EP0292586A1
公开(公告)日：1988-11-30
申请号：EP87107599.0
申请日：1987-05-25
申请人： THE BOEING COMPANY
发明人： Herndon, Gerald F.
IPC分类号： B64D25/10
CPC分类号： B64D25/10
摘要： Apparatus for adjustably mounting an ejection seat (16) in an aircraft in which outer catapult cylinders (58, 60) support inner catapult cylinders (62, 64) and supply force to the inner cylinders to eject the inner cylinders and the seat from the aircraft, the inner cylinders being connected to an upper rear end of the seat (66, 68). The seat (16) is supported in the aircraft by the inner and outer catapult cylinders (62, 64, 58, 60), by adjusting actuators (40) to raise and lower and to tilt the seat forwardly and rearwardly, by lower anchor links (30) pivotally connected to the aircraft and to lower end (26, 28) of the outer catapult cylinders and to the actuators (40), and by upper links (50). The seat is connected to the catapult cylinders (58, 60) by slipper blocks 82. The slipper blocks (82) are pivotally connected to the seat by pins (84) and are slidably engaged with the outer catapult cylinders.
摘要翻译：用于将弹射座（16）可调节地安装在飞行器中的装置，其中外弹射缸（58,60）支撑内弹射缸（62,64）并且向内筒提供力以从飞机弹出内筒和座内筒与座（66,68）的上后端连接。座椅（16）由内外弹射缸（62,64,68,60）支撑在飞行器中，通过调节致动器（40）来升高和降低并使座椅向前和向后倾斜，由下锚杆（30），其枢转地连接到飞行器和外部弹射器气缸的下端（26,28）和致动器（40）以及上连杆（50）。座椅通过滑块82连接到弹射缸（58,60）。拖鞋块（82）通过销（84）枢转地连接到座椅，并且与外弹射瓶可滑动地接合。

59. 发明授权

EP0182214B1 Parachute system and aircraft ejection seat incorporating the same 有权
标题翻译： PARACHUTE系统和飞机喷射座椅同时进行
公开(公告)号：EP0182214B1
公开(公告)日：1988-08-31
申请号：EP85114195.2
申请日：1985-11-07
申请人： Engineering Patents & Equipment Limited
发明人： Martin, James William
IPC分类号： B64D25/10 , B64D17/72
CPC分类号： B64D25/10 , B64D17/72

60. 发明授权

EP0112993B1 Ejection seat stabilization apparatus 有权转让
标题翻译：喷嘴座椅稳定装置
公开(公告)号：EP0112993B1
公开(公告)日：1987-02-25
申请号：EP83110867.5
申请日：1983-10-31
申请人： Stencel Aero Engineering Corp.
发明人： Duncan, James W.
IPC分类号： B64D25/10
CPC分类号： B64D25/10

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