Nissan Motor Company Limited

Agc Inc.

Asahi Glass Company, Limited

Other

Kawasaki Steel Corporation

National Space Development Agency of Japan

Meisei Electric Co., Ltd.

Nobuyuki Kaya

Teruo Fujiwara

Yasuhiko Akao

Jiro Kochiyama

Hiroyuki Yashiro

Hidemi Yasui

Nobuhiro Nakamura

Hirofumi Yamamoto

Nobuhiko Imajo

Takehiko Hiruma

Toshiaki Sato

Satoru Takaki

Yasuo Hayashi

Kazunobu Maeshige

Kusuo Furukawa

Masahiro Kishi

Hajime Ogawa

Mamoru Isobe

Takahiro Mashimo

Eiji Ichikura

Naoto Kihara

Katsumi Inoue

Tatsuzo Miyagoe

Takuji Morita

Shoji Kaneda

Kazutaka Maruta

Makoto Miwada

Megumi Kunimine

Hitoshi Takahashi

Yasushi Watanabe

Kunio Shimano

To provide a glass substrate with an antireflection film, which employs glass having high refractive index and which has excellent strength, and an optical member comprising it. A glass substrate with an antireflection film, comprising a glass substrate which consists of glass having refractive index (n) of from 1.68 to 2.00 and which has plate thickness of from 0.01 to 2 mm, and an antireflection film formed on at least one principal plane of the glass substrate.

Glass substrate with antireflection film, and optical member

A laminate including a glass plate and a coating layer, wherein the coating layer includes one or more components selected from the group consisting of silicon nitride, titanium oxide, alumina, niobium oxide, zirconia, indium tin oxide, silicon oxide, magnesium fluoride, and calcium fluoride, wherein a ratio (dc/dg) of a thickness dc of the coating layer to a thickness dg of the glass plate is in a range of 0.05&#xd7;10to 1.2&#xd7;10, and wherein a radius of curvature r1 of the laminate with negating of self-weight deflection is 10 m to 150 m.

Laminate and method for producing laminate

The present invention provides a laminate that can eliminate adsorption defects of a substrate caused by warping of the substrate and enables electronic devices to be manufactured at high yield. The present invention pertains to a laminate that is provided with a support base material, an adhesion layer, and a substrate in said order. The substrate is provided with a dielectric multilayer film in which dielectric layers having different refractive indexes are alternately laminated on an outer surface of the substrate. The substrate provided with the dielectric multilayer film is disposed on the adhesion layer such that the dielectric multilayer film adheres in a peelable manner to the adhesion layer.

Laminate, method for manufacturing electronic device, and method for manufacturing laminate

A translucent substrate includes a glass substrate containing at least one element selected from a group consisting of Bi, Ti and Sn; a coating layer formed on the glass substrate; and a transparent conductive film formed on the coating layer, wherein the coating layer is deposited by a dry depositing method.

Translucent substrate, organic LED element and method of manufacturing translucent substrate

The present invention relates to a light-shielding film-attached glass substrate including: a glass substrate; and a light-shielding film having a multilayer structure and being formed on the glass substrate, in which the light-shielding film having a multilayer structure includes: a first chromium oxynitride film (CrON); and a second chromium oxynitride film (CrON), each satisfying the following conditions and being laminated in this order from the glass substrate side: 0.15&#x3c;x&#x3c;0.5, 0.1&#x3c;y&#x3c;0.35, 0.4&#x3c;x&#x3c;0.65, 0.03&#x3c;x&#x3c;0.15, and 0.09&#x3c;y&#x3c;0.25.

Light-shielding film-attached glass substrate and liquid crystal display device

A liquid crystal display device eliminating an uneven display, which is a D-STN type liquid crystal display device having a compensation cell and a liquid crystal cell for display wherein a difference between the average thicknesses of at least two adjacent glass substrates among glass substrates existing in the compensation cell and the liquid crystal cell for display is 4 &#x3bc;m or more, and preferably not more than 50 &#x3bc;m.

Liquid crystal display device having particular differences in average thickness of adjacent glass substrates

A laminate for forming a substrate with wires, comprising a conductive layer containing Al or an Al alloy as the major component, formed on a substrate and a capping layer containing a Ni&#x2014;Mo alloy as the major component, formed on the conductive layer, a substrate with wires produced by etching the laminate to remove an unnecessary metal, and a method for producing the same.

Laminate, a substrate with wires, an organic EL display element, a connection terminal for the organic EL display element and a method for producing each

Transparent conductive films are provided which provide high sheet resistance, high transparency, high heat resistance and high moisture resistance, wherein the transparent conductive films contain either (a) an oxide film made of a mixed oxide of indium and tin and doped with at least 0.01 and less than 0.6 weight % of nitrogen and a geometrical thickness of from 5 to 25 nm or (b) an oxide film made of a mixed oxide of indium and tin, wherein the oxide film contains tin within a range of from 4.2 to 8.3 atomic % based on indium and a geometrical thickness of from 5 to 20 nm, and where in each case (a) and (b) the oxide film has a light transmittance of more than 90% at a wavelength of 550 nm, transparent conductive film-coated substrates prepared therefrom and touch panels prepared from the transparent conductive film-coated substrates.

Transparent conductive film and method of making the film

An energy transmission arrangement is formed as a subarray panel which emits a microwave energy signal to a target location on the basis of a pilot signal received from the target location. The subarray panel includes a transmission antenna divided into a subarray having a plurality of antenna elements for transmission of the energy signal. The subarray panel further includes pilot signal receiving antennas and thus each subarray panel may function independently and may thus be made lighter and more compact.

Subarray panel for solar energy transmission

An energy receiving satellite has a curved outer surface on which a plurality of energy signal reception antenna elements are arranged. The satellite may also include a pilot signal generator and a plurality of pilot signal transmission antennas arranged at intervals around the curved outer surface of the satellite. The curved surface is composed of a plurality of curved panels which may be folded in an overlapping condition or unfolded such that the panels are disposed adjacently in a circular arrangement.

Energy receiving satellite

An energy transmission arrangement emits a microwave energy signal to a target location on the basis of a pilot signal received from the target location. The arrangement includes a plurality of pilot antennas for receiving the pilot signal and a plurality of antenna elements for transmission of the energy signal. The pilot signal as received at a first pilot antenna is multiplied at a phase conjugation circuit and divided into a plurality of transmission signals corresponding to the plurality of antenna elements. A target direction is calculated based on a phase difference of the pilot signal as received at each of the other pilot antennas and a phase adjustment circuit is provided for adjusting the phases of each of the transmission signals on the basis of the calculated target direction. Electrical energy is then supplied from energy collecting means to a plurality of amplifiers and amplified respectively, on the basis of a corresponding one of the transmission signals, to be supplied to respective antenna elements to be emitted as the microwave energy signal. According to this arrangment, the phase conjugation circuit is active to receive the pilot signal as received at the first pilot antenna as well as the pilot signal as received at a predetermined reference point in the path of the pilot signal for calculating a difference signal for effecting phase correction of the microwave energy signal.

Energy transmission arrangement

A ranging method for measuring the flight distance of a flight object is implemented by means of a simple system construction. The ranging method is also capable of continuing ranging even if an interruption occurs in data transmission. The ranging method comprises the steps of inserting ranging pulses in a telemeter signal transmitted from a transmitting apparatus provided on the flight object, separating and extracting a ranging pulse from a telemeter signal received by a receiving apparatus provided on the ground side, obtaining a time difference between the ranging pulse and a reference clock signal generated in the receiving apparatus on the basis of a time reference equal to that of the transmitting apparatus (clock signal periods t1 and t2 of both time references are equal), and calculating the flight distance. Since there is no need to provide a transponder or the like on the flight object nor to provide a ranging-tracking system on the ground side, it is possible to realize a simple system construction. Since the ranging pulses are transmitted in the state of being contained in the telemeter signal, it is not necessary to independently prepare ranging-signal transmiting means. In addition, since the telemeter signal can be restored at any time on the ground side, it is possible to prevent ranging from being made impossible due to the interruption of transmission of the signal.

Ranging method using telemetering and apparatus employing said method

A painting steel sheet having an improved distinctness of image after painting has a waviness curve of section profile satisfying given relationships, and is produced by temper rolling a steel sheet with work rolls dulled to particular dimensions through laser.

Steel sheets for painting and a method of producing the same

For controlling the attitude of a rocket including a rocket fuselage and a thrust nozzle integrally attached to the rear end of the rocket fuselage and having a nozzle throat located longitudinally intermediate thereof, a rocket attitude control apparatus comprises a plurality of thrust vector control units disposed at the outer periphery of the thrust nozzle between the nozzle throat and the rear end of the thrust nozzle in circumferentially equiangularly spaced relationship to each other, and each including a fluid injecting nozzle projectable and retractable into and out of the thrust nozzle and having an injecting bore therein, wherein said fluid injecting nozzle is permitted to project into the thrust nozzle while being cooled by fluid injected from the injecting bore into the thrust nozzle. The projection of the fluid injecting nozzle causes a stream of combustion gas passing through the thrust nozzle to be partially disturbed for controlling the attitude of the rocket.

Growing community of inventors

Tokyo, Japan

Teruo Fujiwara