公开(公告)号：WO1987006017A1

公开(公告)日：1987-10-08

申请号：PCT/US1987000358

申请日：1987-02-24

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  FERRER, John, J.

IPC: G02B27/00

CPC classification number: G02B27/0103 ,  B60K2350/2052 ,  G02B27/0081 ,  G02B2027/0109 ,  G02B2027/0145 ,  G02B2027/0165

Abstract: An integrated head-up and panel display system for aircraft cockpits and the like. The system utilizes a wavelength-sensitive fold mirror (25) to separate the HUD image and the panel images. The system includes a monochromatic HUD image source (10) for projecting the HUD image toward the fold mirror (25) and at least one panel display image source (50R) for projecting panel imagery toward the fold mirror. The transmission function of the fold mirror is notched at the wavelength of the monochromatic HUD image source. Thus, the fold mirror reflects the HUD image in the direction of the HUD optical combiner (30) which reflects the HUD image to the system exit pupil (35). The fold mirror (25) is adapted to transmit light in the visible spectra outside the narrow bandwidth of the HUD image source, so that the panel image is transmitted through the fold mirror to a look-down display screen assembly (75R). The screen assembly may be a diffusion screen for providing an image plane at the screen, or an assembly of optical elements for providing a panel image superimposed at the system exit pupil.

Abstract translation: 用于飞机驾驶舱等的集成的平视和面板显示系统。 该系统利用波长敏感的折叠镜（25）来分离HUD图像和面板图像。 该系统包括用于将HUD图像投射到折叠镜（25）的单色HUD图像源（10）和用于将面板图像投射到折叠镜的至少一个面板显示图像源（50R）。 折射镜的透射功能在单色HUD图像源的波长处被切口。 因此，折叠反射镜将HUD图像沿着将HUD图像反射到系统出射光瞳（35）的HUD光学组合器（30）的方向反射。 折叠镜（25）适于透射HUD图像源的窄带宽外的可见光谱中的光，使得面板图像通过折叠镜传输到俯视显示屏组件（75R）。 屏幕组件可以是用于在屏幕处提供图像平面的扩散屏幕，或用于提供叠加在系统出口光瞳上的面板图像的光学元件的组件。

公开(公告)号：WO1987004992A1

公开(公告)日：1987-08-27

申请号：PCT/US1986002458

申请日：1986-11-17

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  APFEL, Steven, L.

IPC: B64G01/40

CPC classification number: F02K9/44 ,  B64G1/26 ,  B64G1/401 ,  B64G1/402

Abstract: A spacecraft propulsion system which integrates the function of the apogee kick motor (AKM) and reaction control system (RCS). In accordance with this invention, a pump-fed AKM is employed which results in lightweight main tanks and pressurization systems. The RCS thrusters are operated by small bellows tanks (48) which are intermittently pressurized by a gas pressurization system (24) to provide high pressure for operation of the RCS thrusters. The system according to this invention enables use of lighter weight main propellant tanks (14, 16) since they do not have to withstand high internal pressures and also enables realization of the numerous advantages of a pump-fed AKM. Several embodiments described various methods for cycling the bellows tanks.

Abstract translation: 一个整合了远地点踢马达（AKM）和反应控制系统（RCS）功能的航天器推进系统。 根据本发明，采用泵送AKM，其导致轻型主缸和加压系统。 RCS推进器由小型波纹管箱（48）操作，这些箱体由气体加压系统（24）间歇地加压，为RCS推进器的运行提供高压。 根据本发明的系统使得能够使用较轻重量的主推进剂罐（14,16），因为它们不必承受高的内部压力，并且还能够实现泵送AKM的众多优点。 几个实施例描述了用于循环波纹管箱的各种方法。

公开(公告)号：WO1987003765A1

公开(公告)日：1987-06-18

申请号：PCT/US1986002015

申请日：1986-09-25

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  KLATT, Robert, W.

IPC: H04N03/09

CPC classification number: H04N3/09

Abstract: An imaging sensor for scanning an image in an object space. The imaging sensor comprises a first and second plurality of infrared detectors. Also provided is a reflecting means for reflecting a predetermined portion of the object space on the first plurality of infrared detectors during first portion of the scanning cycle. The reflecting means is further able to reflect the predetermined portion of the object space on the second plurality of infrared detectors during the second portion of the scanning cycle. In a further embodiment, the orientation of the detectors permits each of the detectors to be calibrated with respect to another of the detectors by a sequential comparison of the outputs of pairs of the detectors whose fields-of-view overlap.

公开(公告)号：WO1987003097A1

公开(公告)日：1987-05-21

申请号：PCT/US1986001985

申请日：1986-09-25

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  DesBRISAY, George, S., Jr. ,  SHAHRIARY, Iradj

IPC: G01R25/00

CPC classification number: H03D13/004 ,  G01R25/00 ,  H03K5/26

Abstract: A phase-frequency discriminator comprising a first RS latch coupled to provide first output signals, said first RS latch including an S input terminal coupled to receive first input signals; a second RS latch coupled to provide second output signals, said second RS latch including an S input terminal coupled to receive second input signals; a third RS latch including an S input terminal coupled to a Q &cir& NOt output terminal of said first RS latch and including a Q &cir& NOt output terminal couples to an R input terminal of said first RS latch and including a Q &cir& NOt output terminal coupled to an R input terminal of said first RS latch; a fourth RS latch including an S input terminal coupled to a Q &cir& NOt output terminal of said second RS latch and including a Q &cir& NOt output terminal coupled to an R input terminal of said second RS latch; and reset means for providing a reset signal when said first and second input signals both have changed from a first to a second logical state such that the first and second output signals change back from the second to the first logical state after a reset time interval substantially long enough for the respective first and second output signals to reach full logic amplitude levels for the second logical state.

Abstract translation: 一种相位鉴频器，包括耦合以提供第一输出信号的第一RS锁存器，所述第一RS锁存器包括耦合以接收第一输入信号的S输入端; 耦合以提供第二输出信号的第二RS锁存器，所述第二RS锁存器包括耦合以接收第二输入信号的S输入端; 第三RS锁存器，包括耦合到所述第一RS锁存器的Q＆CIR和NOt输出端的S输入端，并且包括Q＆CIR和NOt输出端耦合到所述第一RS锁存器的R输入端，并且包括Q＆CIR和NOt输出端耦合 到所述第一RS锁存器的R输入端; 第四RS锁存器，其包括耦合到所述第二RS锁存器的Q＆CIR和NOt输出端的S输入端，并且包括耦合到所述第二RS锁存器的R输入端的Q＆CIR和NOt输出端; 以及复位装置，用于当所述第一和第二输入信号都从第一逻辑状态变为第二逻辑状态时提供复位信号，使得第一和第二输出信号在复位时间间隔基本上从第二逻辑状态改变到第一逻辑状态 足以使相应的第一和第二输出信号达到第二逻辑状态的完全逻辑幅度电平。

公开(公告)号：WO1987002785A1

公开(公告)日：1987-05-07

申请号：PCT/US1986001945

申请日：1986-09-19

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  COCHRAN, Gregory, M.

IPC: G02B26/06

Abstract: An adaptive laser system (10) includes an adaptable laser (12), a waveform sensor (14), an amplitude distribution sensor (16), and a processor (18) for converting data from the sensors into commands for controlling the waveform of a laser beam. Amplitude distribution data is to weight waveform data as the processor determines actuator commands for deforming the laser's main mirror (22). Amplitude weighting permits more accurate determination of the waveform sensor-to-actuator-coupling matrix and more precise optimization of the on-axis intensity of the laser beam across the laser aperture.

公开(公告)号：WO1987002764A1

公开(公告)日：1987-05-07

申请号：PCT/US1986001981

申请日：1986-09-22

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  HERRMANN, Werner ,  MALIS, Albert

IPC: F42B15/027

CPC classification number: F16B2/14 ,  F16B2200/30 ,  F42B10/06 ,  Y10T403/1641 ,  Y10T403/595 ,  Y10T403/61

Abstract: A coupling mechanism for quick attach/disconnect of a control fin to a missile which does not require the use of a separate tool to make the attachment. A first coupling member 24 is mounted on the control fin actuator rod 16. A force regulating means comprised of a spring 28 and retainer bracket 58 are attached to the first coupling member. A second coupling member 26 and a pivotable lever arm 38 are formed as part of the control fin. When the second coupling member is loosly fitted upon the first coupling member, rotation of the lever arm will engage the force regulating means thereby deflecting the spring 28. The reactive force of the spring is exterted through the lever arm, through the control fin, and causes the second coupling member to firmly and securely engage the first coupling member. A means is provided to lock the lever arm in place so as to retain the first and second coupling members in the firmly engaged position even through extreme aerodynamic maneuvers. The lock is easily disengaged manually should it be necessary to remove a control fin from the missile.

公开(公告)号：WO1987002505A2

公开(公告)日：1987-04-23

申请号：PCT/US1986002033

申请日：1986-09-26

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  MAROM, Emanuel ,  SOFFER, Bernard, H. ,  OWECHKO, Yuri ,  DUNNING, Gilmore, J. ,  PEPPER, David, M. ,  KLEIN, Marvin, B. ,  LIND, Richard, C.

IPC: G11C15/00

CPC classification number: G06N3/067 ,  G11C15/00

Abstract: Associative holography memory apparatus (10) which employs a hologram (12) and two phase conjugate mirrors (14, 16). The mirrors (14, 16) are arranged to form a conjugate resonator whereby the output image (44) from the apparatus tends to converge to that stored image most closely associated with an input image (32). Alternate embodiments are described which employ a multiple storage and erasure hologram (52), and which employ only a single phase conjugate mirror (14).

公开(公告)号：WO1987002188A1

公开(公告)日：1987-04-09

申请号：PCT/US1986001912

申请日：1986-09-17

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  SCHNEIDER, Michael, D.

IPC: H01P05/18

CPC classification number: H01P5/183

Abstract: A device for coupling or dividing electromagnetic energy, especially microwaves, between two circuits includes a pair of U-shaped conductors (36, 38) of rectangular cross-section which are coaxially disposed within corresponding slots (32, 34) in an electrically conductive base (30). The conductors have opposing, closely spaced stretches (36c, 38c) at an intersecting juncture in the slots where electromagnetic energy is coupled from one conductor to the other. The conductors are suspended in coaxial relationship within the slots by a pair of coplanar, C-shaped elements (42) which are slidably supported within a second pair of slots (43) in the base and each have cutouts (42a) therein in which the conductors are closely received. A spacer (40) maintains a preselected gap between the opposing stretches of the conductors and is provided with tapered ends (40a, 40b) which cooperate with beveled surfaces (36a, 36b, 38a, 38b) on the conductors to prevent relative lateral movement between the conductors.

公开(公告)号：WO1987002187A1

公开(公告)日：1987-04-09

申请号：PCT/US1986001935

申请日：1986-09-17

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  TSUDA, George, I. ,  AJIOKA, James, S.

IPC: H01P05/12

CPC classification number: H01P5/12

Abstract: A power divider/combiner using two parallel plate radial transmission lines (14, 16) having parallel plate spacing of less than lambda /2 and which operates in a higher order mode, preferably the first higher order circumferential mode TE11. High isolation between amplifiers (34) coupled to the radial transmission lines at their circumferences is achieved by coupling an arrangement of circulators (30, 32, 36) between the amplifiers (34) and the radial transmission lines (14, 16). This isolation arrangement reduces the effects of any spurious signals that are generated by means such as imperfections and imbalances in any active devices coupled to the radial line and permits de-energizing amplifiers as desired for lowering power output without degrading performance.

Abstract translation: 一种功率分配器/组合器，其使用具有小于λ/ 2的平行板间距并且以较高阶模式操作的两个平行板径向传输线（14,16），优选地为第一高阶圆周模式TE11。 通过在放大器（34）和径向传输线（14,16）之间耦合循环器（30,32,36）的布置来实现在其周向耦合到径向传输线路的放大器（34）之间的高隔离度。 这种隔离装置减少了任何寄生信号的影响，这些信号通过诸如耦合到径向线路的任何有源器件中的缺陷和不平衡等方式产生，并且根据需要允许去激励放大器以降低功率输出而不降低性能。

公开(公告)号：WO1987002184A1

公开(公告)日：1987-04-09

申请号：PCT/US1986001915

申请日：1986-09-17

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  WONG, Mon, N. ,  PEEBLES, Ann, L.

IPC: H01P01/12

CPC classification number: H01P1/122 ,  H01P5/182

Abstract: A waveguide switch operable at microwave frequencies is formed of two waveguides (38, 40) of rectangular cross section with a longer wall and a shorter wall, the two waveguides sharing a common shorter wall (50). Two coupling windows (52, 54) are disposed within the common wall for coupling electromagnetic energy between the two waveguides, each coupling window introducing a 90o phase shift. Each window couples one-half the power of an electromagnetic wave from a first of the guides to a second of the guides. The common wall is parallel to the electric field of the coupled wave, with each wave being a TE wave. A 90o phase shift is introduced by each coupling with the result that utilization of both windows produces a summation of the two waves in the second of the waveguides and a cancellation of the two waves in the first of the waveguides. Gates (60, 62) are employed for selectively closing off either one or both of the windows to retain all of the power in the first waveguide, or to close off only one of the waveguides for an equal distribution of the power in both waveguides.