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1. 发明授权

US2914916A Arrangement for controlling the flow of a fluid by means of an auxiliary flow 失效
标题翻译：用于通过辅助流控制流体流动的布置
公开(公告)号：US2914916A
公开(公告)日：1959-12-01
申请号：US39723353
申请日：1953-12-09
申请人： SNECMA
发明人： GELIN PAUL , KADOSCH MARCEL
IPC分类号： F02K1/28 , F02K1/32 , F15D1/08
CPC分类号： F15D1/08 , F02K1/28 , F02K1/32 , Y10S415/914

2. 发明专利

DE976186C 未知
公开(公告)号：DE976186C
公开(公告)日：1963-04-18
申请号：DES0048301
申请日：1952-01-01
申请人： SNECMA
发明人： KADOSCH MARCEL
IPC分类号： F01D5/14

3. 发明专利

CA610808A DEVICE FOR CONTROLLING THE FLOW DIRECTION OF A REACTION JET ISSUING FROM A NOZZLE 未知
公开(公告)号：CA610808A
公开(公告)日：1960-12-20
申请号：CA610808D
申请人： SNECMA
发明人： MARCHAL RAYMOND H , KADOSCH MARCEL , PARIS FRANCOIS G , BERTIN JEAN

4. 发明专利

CA584432A JET DEFLECTING DEVICE 未知
公开(公告)号：CA584432A
公开(公告)日：1959-10-06
申请号：CA584432D
申请人： SNECMA
发明人： SALLE LOUIS M G DE LA , TURINETTI HENRI , BERTIN JEAN H , MAUNOURY FRANCOIS M L , KADOSCH MARCEL

5. 发明专利

CA575560A JET NOZZLES AND JET PROPULSION UNITS 未知
公开(公告)号：CA575560A
公开(公告)日：1959-05-12
申请号：CA575560D
申请人： SNECMA
发明人： MARCHAL RAYMOND H , KADOSCH MARCEL , BERTIN JEAN , FRANCE FRANCOIS G

6. 发明专利

CA568189A GRID DEFLECTOR FOR JET-PROPULSION UNITS 未知
公开(公告)号：CA568189A
公开(公告)日：1958-12-30
申请号：CA568189D
申请人： SNECMA
发明人： BERTIN JEAN H , KADOSCH MARCEL

7. 发明专利

CA566326A CONTROL DEVICES OF THE CROSS-SECTION AREA OF A NOZZLE 未知
公开(公告)号：CA566326A
公开(公告)日：1958-11-18
申请号：CA566326D
申请人： SNECMA
发明人： BAUGER LOUIS A J , KADOSCH MARCEL , MAUNOURY FRANCOIS M L , BERTIN JEAN H

8. 发明专利

DE1026629B 未知
公开(公告)号：DE1026629B
公开(公告)日：1958-03-20
申请号：DES0048300
申请日：1951-12-31
申请人： SNECMA
发明人： KADOSCH MARCEL , FOLL JEAN LE , MAUNOURY FRANCOIS MARIE LOUIS , BERTIN JEAN
IPC分类号： B64C21/04

9. 发明专利

DE1011288B 未知
公开(公告)号：DE1011288B
公开(公告)日：1957-06-27
申请号：DES0051102
申请日：1953-10-08
申请人： SNECMA
发明人： BERTIN JEAN HENRI , KADOSCH MARCEL , MAUNOURY FRANCOIS MARIE LOUIS
IPC分类号： B64C27/82

10. 发明专利

GB770025A Device for steering aircraft, rockets and the like, having a jet propelling nozzle 未知
公开(公告)号：GB770025A
公开(公告)日：1957-03-13
申请号：GB2710353
申请日：1953-10-02
申请人： SNECMA
发明人： BERTIN JEAN HENRI , KADOSCH MARCEL , MAUNOURY FRANCOIS MARIE LOUIS
IPC分类号： B64C9/38 , F02K9/82
摘要： 770,025. Reaction propelled aircraft. SOC. NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION. Oct. 2, 1953 [Oct. 10, 1952], No. 27103/53. Class 4. [Also in Group XXVI] A device for steering an aircraft having a jet propulsion nozzle is characterized by a tubular member 4 having a longitudinal slot 2, mounted at the nozzle outlet and rotatable relatively thereto about its axis, the latter being perpendicular to the nozzle axis, the slot opening into the jet at an angle depending on the position of member 4, the latter being connected to a source of gas under pressure. In the embodiment of Fig. 1, a rectangular section nozzle 1 is provided with a curved smooth extension 3 along one of its longer sides, and has on its opposite side a cylinder 4, provided with a slot 2, rotatable in a part cylindrical housing 5 secured to the nozzle. A servo-operated toothed rack may rotate a pinion fast to the cylinder. The interior of the cylinder is connected through a valve to a source of pressure, e.g. the compressor or combustion chambers of a turbo-jet unit, so that a transverse jet of variable direction issues from slot 2. Variation of the direction of the transverse jet varies the direction of the main jet to control the aircraft. In a modification, the housing 5 comprises a wide slot, and a wide slot is provided in the cylinder 2, so that rotation thereof causes the slots more or less to overlap, controlling the quantity of flow in the directing jet. In this case the valve in the pressure supply line, which may be of the simple full on or full off type, may be omitted. Specifications 691,302, 691,948 and 696,088 are referred to.

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