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公开(公告)号:US3492525A
公开(公告)日:1970-01-27
申请号:US3492525D
申请日:1968-03-11
Applicant: UNITED AIRCRAFT CORP
Inventor: DAVIS JACK W , PINSLEY EDWARD A , FERREIRA FERNAND J
IPC: H01J17/06 , H01J37/077 , H01J1/20
CPC classification number: H01J37/077 , H01J17/066 , H01J2893/0066
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公开(公告)号:US3699471A
公开(公告)日:1972-10-17
申请号:US3699471D
申请日:1971-07-20
Applicant: UNITED AIRCRAFT CORP
Inventor: MULREADY RICHARD C , PINSLEY EDWARD A
IPC: H01S3/0979 , H01S3/02
CPC classification number: H01S3/0979
Abstract: A series of fences are placed across the side walls of a flow channel forming the optical cavity of a gas dynamic laser which contains the gas dynamic laser flow therein and are positioned between end walls containing the laser beam mirrors and apertures. The fences are positioned lengthwise with the direction of flow and are located on each side wall of the optical cavity. They are spaced so that they will absorb and/or reflect all rays intersecting the optical cavity side walls at a grazing incidence. The invention herein described was made in the course of or under a contract with the Air Force.
Abstract translation: 将一系列栅栏放置在形成气体动态激光器的光腔的流动通道的侧壁上,气动动态激光器包含气体动态激光流,并且位于包含激光束反射镜和孔的端壁之间。 围栏沿着流动方向纵向定位并位于光学腔的每个侧壁上。 它们间隔开,使得它们在掠入射处吸收和/或反射与光腔侧壁相交的所有光线。 本文所述的发明是在与空军签订合同的过程中进行的。
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公开(公告)号:US2870958A
公开(公告)日:1959-01-27
申请号:US55887456
申请日:1956-01-13
Applicant: UNITED AIRCRAFT CORP
Inventor: PINSLEY EDWARD A
CPC classification number: F04D29/681 , F04D27/001 , Y10S415/914
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公开(公告)号:US3514553A
公开(公告)日:1970-05-26
申请号:US3514553D
申请日:1967-11-01
Applicant: UNITED AIRCRAFT CORP
Inventor: PENNEY ALBERT W JR , BULLIS ROBERT H , PINSLEY EDWARD A
CPC classification number: H02K13/00 , B60L5/005 , B60L2200/26
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公开(公告)号:US3308621A
公开(公告)日:1967-03-14
申请号:US33497263
申请日:1963-12-30
Applicant: UNITED AIRCRAFT CORP
Inventor: PINSLEY EDWARD A
IPC: F03H1/00
CPC classification number: F03H1/0081 , H01J27/205
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公开(公告)号:US3140411A
公开(公告)日:1964-07-07
申请号:US5558160
申请日:1960-09-12
Applicant: UNITED AIRCRAFT CORP
Inventor: OICKLE JR CHARLES , PINSLEY EDWARD A
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公开(公告)号:US3886475A
公开(公告)日:1975-05-27
申请号:US33600073
申请日:1973-02-26
Applicant: UNITED AIRCRAFT CORP
Inventor: PINSLEY EDWARD A
IPC: H01S3/0953 , H01S3/04
CPC classification number: H01S3/0953
Abstract: The device includes a closed cycle gas dynamic laser wherein the lasing fluid is recirculated in a closed loop. The closed loop includes a nozzle array, a lasing cavity and a diffuser. The exit of the diffuser is connected to the inlet to the nozzle array with a fuel heat exchanger located in the lasing flow and a pumping means located between the heat exchanger and the nozzle array. To provide for cooling of the pumping means and to improve diffuser performance, gas bled from the diffuser is cooled by two heat exchangers and pumped into cooling passages in the pumping means. The heat exchangers for cooling the flow to the pumping means are located in series and carry fuel from a supply to an injector in said combustor and the heat exchanger in the lasing flow cools the fluid and carries the fuel from a supply to an injector in said combustor.
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公开(公告)号:US3518479A
公开(公告)日:1970-06-30
申请号:US3518479D
申请日:1968-02-27
Applicant: UNITED AIRCRAFT CORP
Inventor: PINSLEY EDWARD A
IPC: H01J37/077 , H01J37/30 , H01J1/50
CPC classification number: H01J37/3007 , H01J37/077
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公开(公告)号:US3268746A
公开(公告)日:1966-08-23
申请号:US7940560
申请日:1960-12-29
Applicant: UNITED AIRCRAFT CORP
Inventor: CONRAD CROWN JOHN , PINSLEY EDWARD A
IPC: H02K44/08
CPC classification number: H02K44/08
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公开(公告)号:US3614656A
公开(公告)日:1971-10-19
申请号:US3614656D
申请日:1968-02-23
Applicant: UNITED AIRCRAFT CORP
Inventor: PINSLEY EDWARD A , BROWN CLYDE O
IPC: H01S3/097 , H01S3/0979 , H01S3/02
CPC classification number: H01S3/097 , H01S3/0979
Abstract: Carbon dioxide is injected into a stream of excited nitrogen by means of one or more manifolds or rods located directly within the laser chamber, disposed adjacent to and movable relative to the laser cavity.
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