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1. 发明专利

JPS4222751B1 失效
公开(公告)号：JPS4222751B1
公开(公告)日：1967-11-07
申请号：JP420065
申请日：1965-01-27
申请人： NORTH AMERICAN AVIATION INC
发明人： EDGAR VALSTAR JACOB
IPC分类号： G05B23/02 , G06G7/625 , G06J1/00

2. 发明专利

NL7700303A Isolated semiconductor devices on a common substrate - with isolation which avoids parasitic junction capacitance and avalanche breakdown 未知
公开(公告)号：NL7700303A
公开(公告)日：1977-04-29
申请号：NL7700303
申请日：1977-01-13
申请人： NORTH AMERICAN AVIATION INC
IPC分类号： H01L21/00 , H01L21/306 , H01L21/762 , H01L23/29 , H01L27/00 , H01L21/94 , H01L21/76
摘要： Monocrystalline semiconductor segments on an insulating crystalline substrate are spaced by interposed insulating portions. The segments are embedded in the substrate and are thermally compatible with it but crystallographically distinct from it. The isolating regions are pref. formed by (a) etching grooves in a semiconductor material where electrical isolation will be required, as in e.g. IC fabrication, (b) coating the etched side with a thin film of thermally compatible electrically insulating material, including in the grooves (c) depositing thermally compatible material on the insulating film including the film in the grooves to form a substrate for the semiconductor, and (d) lapping the exposed surface of the semiconductor until the substrate material in the isolating grooves is exposed.

3. 发明专利

NO133209B 未知
公开(公告)号：NO133209B
公开(公告)日：1975-12-15
申请号：NO16808567
申请日：1967-05-10
申请人： NORTH AMERICAN AVIATION INC
发明人： FRIED W R , SPRAGUE T G
IPC分类号： G01S13/524 , G01S13/528 , G01S13/64 , G01S9/42

4. 发明专利

DE1591334C1 未知
公开(公告)号：DE1591334C1
公开(公告)日：1975-11-06
申请号：DEN0031362
申请日：1967-10-09
申请人： NORTH AMERICAN AVIATION INC
发明人： LEONARD VEHRS JUN CHARLES
IPC分类号： G01S7/36 , G01S13/534 , G01S9/42
摘要： In a non-coherent airborne moving target indicator, doppler processing means for providing a substantially clutter-free target signal. The presence of at least one of a preselected spectral condition and a preselected radial extent condition, indicative of a substantially clutter-referenced signal state, is determined. Such determination is employed for gating control of gated filter means for providing a normally low-pass filtered doppler processor output in the absence of a substantial clutter reference and alternatively providing a high-pass filtered output during the presence of a substantial clutter content.

5. 发明专利

CA972856A AMTI RADAR SYSTEM 未知
公开(公告)号：CA972856A
公开(公告)日：1975-08-12
申请号：CA998020
申请日：1967-08-16
申请人： NORTH AMERICAN AVIATION INC
发明人： VEHRS CHARLES L JR
IPC分类号： G01S7/36 , G01S13/534
摘要： In a non-coherent airborne moving target indicator, doppler processing means for providing a substantially clutter-free target signal. The presence of at least one of a preselected spectral condition and a preselected radial extent condition, indicative of a substantially clutter-referenced signal state, is determined. Such determination is employed for gating control of gated filter means for providing a normally low-pass filtered doppler processor output in the absence of a substantial clutter reference and alternatively providing a high-pass filtered output during the presence of a substantial clutter content.

6. 发明专利

DK129812C 未知
公开(公告)号：DK129812C
公开(公告)日：1975-05-26
申请号：DK269167
申请日：1967-05-23
申请人： NORTH AMERICAN AVIATION INC
发明人： FRIED W R , SPRAGUE T G
IPC分类号： G01S13/524 , G01S13/528 , G01S13/64 , G01S9/42

7. 发明专利

DE1564457C3 未知
公开(公告)号：DE1564457C3
公开(公告)日：1975-04-10
申请号：DE1564457
申请日：1966-10-05
申请人： NORTH AMERICAN AVIATION, INC., EL SEGUNDO, CALIF. (V.ST.A.)
发明人： GODEJAHN JUN., GORDON CHARLES, SANTA ANA, CALIF. (V.ST.A.)
IPC分类号： H01L21/762 , H01L21/76

8. 发明专利

DE1667644C3 未知
公开(公告)号：DE1667644C3
公开(公告)日：1974-02-14
申请号：DE1667644
申请日：1967-02-10
申请人： NORTH AMERICAN AVIATION INC., EL SEGUNDO, CALIF. (V.ST.A.)
发明人： ARGUE, GARY RAMSAY, WOODLAND HILLS , OWENS, BOONE BAILEY, CALABASAS
IPC分类号： C01G5/00 , H01M6/18 , C01B9/06

9. 发明专利

DE1564457A1 未知
公开(公告)号：DE1564457A1
公开(公告)日：1972-07-27
申请号：DE1564457
申请日：1966-10-05
申请人： NORTH AMERICAN AVIATION INC
发明人： CHARLES GODEJAHN JUN GORDON
IPC分类号： H01L21/762 , H01L19/00

10. 发明专利

DE1591313A1 未知
公开(公告)号：DE1591313A1
公开(公告)日：1972-03-09
申请号：DE1591313
申请日：1967-06-07
申请人： NORTH AMERICAN AVIATION INC
发明人： EDISON STONEY WILLIAM
IPC分类号： H01Q3/22 , H04B7/10 , H04B7/204 , H04B7/14
摘要： 1,145,194. Radio signalling. NORTH AMERICAN AVIATION Inc. 28 March, 1967 [7 June, 1966], No. 13999/67. Heading H4L. A directional radio link comprises two radio stations of which a first station has a mechanical scannable first aerial and means for selecting the carrier frequency transmitted by the aerial to correspond with a carrier frequency received from the second station, the second station having a frequency-sensitive. second aerial of the type which transmits or receives in a different direction for each different frequency in a given range and means for selecting the carrier frequency received or transmitted by the second aerial so as to establish communication with the first station. As described, the second station is an artificial earth satellite providing a link between geographically spaced earth stations (or space vehicles) in a multiple access system, a unique carrier frequency (the direction frequency) for each ground station corresponding to the line-of-sight between the ground station and the relay station. Terminal station, Fig. 2.-Aerial 23 is scanned by a control unit 24 under the direction of a programmer 25, and an electronically tunable receiver 26 may provide tracking angle error signals (for utilization by the programmer to control the unit 24) and receives frequency search signals and communication signals from a relay station. Alternatively, a separate angle tracking receiver may be provided. A transmitter 27 supplies signals from the programmer 25 to the aerial 23 and an interface unit 28 couples the sending and receiving units to the radio station and effects any necessary signal conversion. Initially the programmer operates in a search mode in which aerial 23 scans in a search pattern towards a desired relay while a predetermined sequence of radio frequencies is transmitted by transmitter 27 in each of the directions scanned. The search signals may be coded to identify the relay sought and/or the terminal station with which communication is sought. The relay responds to that one of the scanned frequencies corresponding to the direction frequency of the interrogating station by transmitting the same frequency in return (coded to identify the relay) and programmer 25 then functions to cause transmitter 27 and receiver 26 to operate on this frequency, and the control unit 24 will use the angle tracking error signals from the receiver 26 to cause aerial 23 to track the relay. Relay station, Fig. 3.-Spherical coverage by the electronically scanned aerial is provided by six planar arrays 33a to 33f forming the sides of a box-like structure which also houses the remaining equipment of the relay. Solar power units may be housed between the radiation elements of each array. A programmer 35 decodes incoming signals from the receivers 34, the frequency of a received signal indicating the direction angle of the transmitting station, this information being stored at 35. The received signal may include a code indicating the desired station or may include a subcarrier which is a submultiple of the carrier frequency of that station and may be multiplied in the relay to the appropriate carrier frequency. Modified system, Fig. 5.-This system employs different carrier frequencies for transmission and reception, separate receiving and transmitting arrays 38, 39 respectively being provided at the relay station. In the search mode the programmer (station m) via frequency synthesizer 45, causes the transmission of successive up-frequencies (as in Fig. 2) which are received by array 38 of the relay station, each carrier being modulated by a submultiple of the associated down-frequency of the transmitting array 39. When the relay receiver 30 receives an up-frequency corresponding to the direction of station m, i.e. above a predetermined threshold, the sideband is selected by a filter 41a, frequency-multiplied in a multiplier 42a and transmitted via array 39 to the originating station. The station receiver 26 then provides a signal which via the programmer stops the frequency on the correct up-direction carrier frequency. When a second station (also locked on to the relay) seeks to address station m by a conventional ring-through technique, the code of the called station (e.g. preselected combinations of audio-frequencies) are imposed on the down-frequency carrier of the called station by means of a dialling register 49. Dialling register, Fig. 6 (not shown).-This provides a multiple cross-bar switching arrangement in the form of a switching matrix, each column of the matrix being associated with a direction frequency decoder and each row corresponding to a different one of the station codes. Satellite attitude control.-The aerial array of a satellite relay station may be used to measure the satellite's position with reference to a selected terminal station to provide control signals for operation of the attitude controllers.

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