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1. 发明授权

US4270183A Data dejittering apparatus 失效
标题翻译：数据消除装置
公开(公告)号：US4270183A
公开(公告)日：1981-05-26
申请号：US767807
申请日：1977-02-11
申请人： Robert L. Robinson , David C. Hoff , Robert L. Midling
发明人： Robert L. Robinson , David C. Hoff , Robert L. Midling
IPC分类号： G06F5/06 , H03L7/085 , H04J3/06 , G06F11/00
CPC分类号： H03L7/085 , G06F5/06 , H04J3/0626 , G06F2205/061
摘要： A circuit for dejittering transmitted digital data. A buffer stores the incoming data and has its half-full condition monitored by content decoding circuitry including a counter whose count is converted to control the frequency of a voltage controlled oscillator. The oscillator clocks the data out of the buffer effectively free of harmful jitter.
摘要翻译：用于消除发射数字数据的电路。缓冲器存储输入数据并且具有由内容解码电路监视其半满状态，该内容解码电路包括其计数被转换以控制压控振荡器的频率的计数器。振荡器将数据从缓冲器中计时，从而有效地避免了有害抖动。

2. 发明授权

US3912202A Side force control for airplanes 失效
标题翻译：机场侧力控制
公开(公告)号：US3912202A
公开(公告)日：1975-10-14
申请号：US47987874
申请日：1974-06-17
申请人： LOCKHEED AIRCRAFT CORP
发明人： JENKINS MICHAEL W M
IPC分类号： B64C15/02 , F02K1/00 , B64C15/06
CPC分类号： F02K1/002 , B64C15/02
摘要： This invention proposes to minimize the roll control requirements of airplanes at low speeds and to trim the airplane in crosswind landings by means of applying side forces on the airplane which are generated by lateral vectoring of the cruise engines. This is accomplished through the use of deflectors at the aft end of the engines which are angularly adjustable in unison through control linkage integrated with the operation of the existing, conventional control surfaces of the airplane.

3. 发明授权

US3897695A Linkage system, particularly for aircraft control 失效
标题翻译：联动系统，特别适用于飞机控制
公开(公告)号：US3897695A
公开(公告)日：1975-08-05
申请号：US43999574
申请日：1974-02-06
申请人： LOCKHEED AIRCRAFT CORP
发明人： ROSTAD NELS C
IPC分类号： B64C13/32 , G05G7/04
CPC分类号： G05G7/04 , B64C13/32 , Y10T74/20558 , Y10T74/2057 , Y10T74/2101
摘要： A linkage, particularly for an aircraft control surface utilizing an arrowhead cam and a follower member. The shape of the arrowhead in cooperation with the location of the pivot points of this cam and of the follower predetermines the output motion of the follower in response to input motion on the arrowhead cam. The linkage produces a variable gain; i.e., a different output response at the follower for the same increment of input motion at different places in the total range of input motion.
摘要翻译：一种联动装置，特别是用于利用箭头凸轮和从动件的飞机控制表面。与该凸轮和跟随器的枢转点的位置协调的箭头形状预先确定随动件对箭头凸轮上的输入运动的输出运动。连接产生可变增益; 即在输入运动的总范围内在不同位置输入运动相同增量的跟随器处的不同输出响应。

4. 发明授权

US3852854A Girt bar latching system 失效
标题翻译： GIRT酒吧锁定系统
公开(公告)号：US3852854A
公开(公告)日：1974-12-10
申请号：US34823473
申请日：1973-04-05
申请人： LOCKHEED AIRCRAFT CORP
发明人： RICKEL E , CLINE J , SIGRUD D , FIELDS C
IPC分类号： B64D25/14 , A44B11/25 , A44B13/00
CPC分类号： B64D25/14 , Y10T24/45644 , Y10T292/23
摘要： A girt bar latching system for operating the deployment of an evauation slide or combination slideraft in event of an emergency, and in normal mode of operation to latch and release its girt bar from floor fittings when the exit door is closed and opened, respectively. An inflatable but collapsed and packed slide is stored in a container mounted upon the interior side of the exit door, and is utilized in emergency situations only. In normal operation, as the door closes, the end portions of a girt bar connected to the slide engage the floor fittings. Upon opening the door, latches included in the floor fittings are depressed thereby providing for release of the girt bar so that it travels with the slide, container, and door. In an emergency mode of operation, as the door is opened, the latches remain raised to prevent the girt bar from releasing from the floor fittings. The girt bar is retained in the floor fittings as the escape slide or raft deploys. An arming mechanism is employed for selection of normal and emergency operational modes.
摘要翻译：一种用于在发生紧急情况时操作释放滑块或组合滑块的部署，并且在正常操作模式下，分别在出口门关闭和打开时将其衬管杆从地板配件上释放并释放。可膨胀但折叠和包装的载玻片储存在安装在出口门内侧的容器中，仅在紧急情况下使用。在正常操作中，当门关闭时，连接到滑块的连接杆的端部接合地板配件。在打开门时，包括在地板配件中的闩锁被压下，从而提供释放杆状物，使得其与滑动件，容器和门一起行进。在紧急操作模式下，当门打开时，闩锁保持升高以防止棉条从地板配件上释放。当逃生滑梯或筏子部署时，棉条被保留在地板配件中。采用布防机制来选择正常和应急操作模式。

5. 发明授权

US3848662A Method and apparatus for supplying a temperature conditioned airflow to an open compartment in an explosion sustaining ambient surrounding 失效
标题翻译：在爆炸持续环境中向开放舱提供温度调节气流的方法和装置
公开(公告)号：US3848662A
公开(公告)日：1974-11-19
申请号：US22328272
申请日：1972-02-03
申请人： LOCKHEED AIRCRAFT CORP
发明人： KILGORE R
IPC分类号： B64D13/00 , F24D9/00 , F24H3/06
CPC分类号： F24D9/00 , B64D13/00
摘要： This invention discloses the combination of (1) a liquid temperature conditioning apparatus located exteriorly of a potential explosion sustaining zone, (2) an explosion proof airliquid heat exchange device located within a potential explosion sustaining zone, and (3) air ducts interconnecting the air-liquid heat exchange device with the interior of a compartment open to the ambient and containing explosion sustaining vapors, such as the interior of an integral fuel tank compartment in an aircraft containing vapors arising from highly volatile hydrocarbon fuels normally carried therein. This combination further includes a closed-loop liquid circuit interconnecting the liquid temperature conditioning apparatus exterior of the explosion sustaining zone and the air-liquid heat exchange device located within the explosion sustaining zone, along with a blower means associated with the air-liquid heat exchange device whereby air ambient to the air-liquid heat exchange device within the explosion sustaining zone is temperature conditioned by being blown through an air-liquid heat exchange coil and supplied to the compartment interior. By appropriate control of the liquid temperature conditioning apparatus, the compartment interior can be continuously supplied by temperature conditioned air that is either cooled or heated.
摘要翻译：本发明公开了（1）位于潜在的防爆区域外部的液体温度调节装置，（2）位于潜在的防爆区域内的防爆气液热交换装置和（3）相互连接的空气管道空气 - 液体热交换装置，其室内部开放于环境，并且包含防爆蒸气，例如飞机中的整体燃料箱舱室的内部，其中包含由其中通常携带的高挥发性烃类燃料产生的蒸气。该组合还包括将防爆区域的液体温度调节装置和位于防爆区域内的空气 - 液体热交换装置连接在一起的空气 - 液体热交换器其中通过吹入空气 - 液体热交换盘管并将其提供给隔室内部，使得在爆炸维持区内的空气 - 液体热交换装置的空气温度受到温度调节。

6. 发明授权

US3834654A Boxplane wing and aircraft 失效
标题翻译： BOXPLANE WING AND AIRCRAFT
公开(公告)号：US3834654A
公开(公告)日：1974-09-10
申请号：US34282373
申请日：1973-03-19
申请人： LOCKHEED AIRCRAFT CORP
发明人： MIRANDA L
IPC分类号： B64C39/06 , B64C3/06
CPC分类号： B64C39/068
摘要： An aircraft wing system wherein a first pair of rearwardly swept wings is interconnected at the wing tips to a second pair of forwardly swept wings, the interconnection being accomplished by a pair of vertically swept fins, the two pair of wings being horizontally and vertically staggered relative to one another. Each pair of wings is also structurally attached to another aircraft component.
摘要翻译：一种飞机机翼系统，其中第一对向后扫掠的翼在翼尖处互连到第二对向前扫掠的翼，所述互连由一对垂直扫掠的翅片完成，所述两对翼相对于水平和垂直交错彼此。每对翼也在结构上连接到另一飞行器部件。

7. 发明授权

US3827278A Joggling tool 失效
标题翻译： JOGGLING工具
公开(公告)号：US3827278A
公开(公告)日：1974-08-06
申请号：US36671373
申请日：1973-06-04
申请人： LOCKHEED AIRCRAFT CORP
发明人： MERSHON B , WILHELM K
IPC分类号： B21D11/18 , B21J7/26 , B21J7/24
CPC分类号： B21J7/26 , B21D11/18
摘要： A joggling tool explosively actuated to release energy at a high rate to a punch member which physically imparts a force to a workpiece held in a forming die member to accomplish a joggle or indentation therein. A cartridge mounted upon an inner barrel member is fired to develop explosive gas in its bore chamber to drive the punch member. An outer barrel member is mounted about the inner barrel member to guide the movement of the punch member. A breech housing circumscribes both barrel members and has mounted thereon a firing device for the cartridge. The outer barrel member is supported by a frame member or yoke which is securely mounted, such as by locating pins, to the forming die member.
摘要翻译：爆破式致动以将高能量释放到冲压件的冲击工具，所述冲头构件物理地向保持在成型模具构件中的工件施加力，以在其中实现弯曲或凹陷。燃烧安装在内筒构件上的筒体，以在其孔室中产生爆炸性气体以驱动冲压构件。外筒构件围绕内筒构件安装以引导冲压构件的运动。臀部外壳围绕两个筒构件，并且在其上安装有用于墨盒的点火装置。外筒构件由框架构件或轭架支撑，框架构件或轭架通过定位销牢固地安装到成型模具构件上。

8. 发明授权

US3824842A Apparatus and method for the measurement of acoustic absorption and impedance 失效
标题翻译：用于测量吸声和阻抗的装置和方法
公开(公告)号：US3824842A
公开(公告)日：1974-07-23
申请号：US24577672
申请日：1972-04-20
申请人： LOCKHEED AIRCRAFT CORP
发明人： WIRT L , MORROW D
IPC分类号： G01N29/09 , G01N29/00
CPC分类号： G01N29/09 , G01N2291/02491
摘要： Apparatus and method for measuring the acoustical impedance and/or the absorption coefficient of materials of the class which exhibit nonlinear behavior at high sound intensities. A highintensity biasing noise having a broadband spectrum and a low intensity pure sinusoidal tracer tone are introduced in combination into a standard impedance tube or standing-wave apparatus. The standing-wave pattern in the tube is measured by a pressure microphone probe movable along the axis of the tube. The tracer tone is retrieved by highly selective filtering and used to provide a measurement signal which corresponds to the response of the material. By sampling the standing wave pattern in the tube, the entire spectrum of the broadband noise response may be obtained.
摘要翻译：用于测量在高声强度下表现出非线性行为的类的材料的声阻抗和/或吸收系数的装置和方法。将具有宽带频谱和低强度纯正弦曲线色调的高强度偏置噪声组合引入到标准阻抗管或驻波装置中。通过可沿着管的轴线移动的压力麦克风探头来测量管中的驻波图案。通过高度选择性滤波检索示踪音，并用于提供对应于材料响应的测量信号。通过对管中的驻波模式进行采样，可以获得宽带噪声响应的整个频谱。

9. 发明授权

US3820627A Apparatus for noise and air pollution abatement 失效
标题翻译：噪音和空气污染评估装置
公开(公告)号：US3820627A
公开(公告)日：1974-06-28
申请号：US28442372
申请日：1972-08-28
申请人： LOCKHEED AIRCRAFT CORP
发明人： WIRT L
IPC分类号： B23Q11/00 , E04B1/82 , G10K11/16 , E04B1/84
CPC分类号： G10K11/161 , B23Q11/0046 , B23Q11/0078 , B23Q11/0096 , Y10S454/906
摘要： A system for simultaneously controlling airborne noise and air pollutants. Comprises an acoustic panel or enclosure constructed of a permeable sheet separated by an air space from an impermeable sheet, and includes means for inducing a ventilating flow of air through the permeable sheet. The air flow and permeability of the sheet are selected to lie within a specified range such that Delta p/u about Z where Delta p is the differential pressure across the sheet, u is the velocity of air approaching the sheet, and Z is the characteristic impedance of air. Especially suitable for ventilating hoods, enclosures, or semi-enclosures for machine tools, spray booths, welding apparatus, and the like.

10. 发明授权

US3798199A Carboxylic acid dihydrazide polymers 失效
标题翻译：羧酸二异氰酸酯聚合物
公开(公告)号：US3798199A
公开(公告)日：1974-03-19
申请号：US3798199D
申请日：1972-10-05
申请人： LOCKHEED AIRCRAFT CORP
发明人： HAN Y
IPC分类号： C08G4/00 , C08G73/06 , C08G9/06 , C08G5/02
CPC分类号： C08G4/00 , C08G73/0694
摘要： A NEW CALSS OF POLYMER, NAMELY A CARBOXYLIC ACID DIHYDRAZIDE-DIOL-ALDEHYDE POLYMER, IS PREPARED BY POLYMERIZING A CARBOXYLIC ACID DIHYDRAZIDE WITH A DIOL AND AN ALDEHYDE UNDER TEMPERATURE CONDITIONS TO FORM AN NUNCYCLIZED POLYAMIC ACID. THE POLYAMIC ACID IS THEN INTERNALLY N-N CYCLIZED AT A HIGHER TEMPERATURE.

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