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41. 发明专利

GB750618A Improvements in arrangement for the control of the jet in reaction-propulsion units 未知
公开(公告)号：GB750618A
公开(公告)日：1956-06-20
申请号：GB1536453
申请日：1953-06-03
申请人： SNECMA
发明人： KADOSCH MARCEL , BERTIN JEAN HENRI
IPC分类号： F02C3/06 , F02K1/28 , F02K1/30 , F02K1/32
摘要： 750,618. Jet propulsion plant. SOC. NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION. June 3, 1953 [June 5, 1952], No. 15364/53. Class 110(3) [Also in Group XXXIII] A jet propulsion unit is characterized by the provision of a jet deflecting device comprising a plurality of guide vanes extending outside the normal flow path of the jet and spaced therealong and controllable means for urging said jet towards said vanes, and a device for varying the area of said nozzle comprising fluid-injecting means opening into said jet in a generally crosswise direction with respect thereto at the periphery of said jet and upstream of said vanes, said fluid injecting means being designed for forming a transverse screen-like jet adapted to reduce the effective area of said nozzle and to urge the boundary layers of said jet clear of said vanes. The exhaust nozzle 35 carries deflector baffles 43 and a centrally disposed body 38 formed with outwardly and rearwardly directed orifices 40, 41 supplied with gas under pressure through a valve - 44, whereby the exhaust stream may be diverted outwardly to pass through the baffles 43. An additional orifice 36 extends circumferentially round an annular chamber 36a also supplied with pressure gas through a valve 45, whereby the exhaust stream may be contracted and, when orifices 40 and 41 are inoperative, prevented from spreading outwardly into contact with the rearmost baffles 43. Specifications 696,088 [Group XXXIII], 745,630 and 750,601 are referred to.

42. 发明专利

GB750601A Improvements in jet nozzles and jet propulsion units 未知
公开(公告)号：GB750601A
公开(公告)日：1956-06-20
申请号：GB1105451
申请日：1951-05-10
申请人： SNECMA
发明人： KADOSCH MARCEL , PARIS FRANCOIS GILBERT , BERTIN JEAN , MARCHAL RAYMOND HIPPOLYTE
IPC分类号： B64C15/02 , F02K1/32 , F15C1/00
摘要： 750,601. Jet propulsion nozzles. SOC. NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION. May 10, 1951 [June 16, 1950], No. 11054/51. Class 110(3) [Also in Group XXXIII] In a jet propulsion engine having an air compressor for example a jet turbine engine, a device is provided for deflecting the jet stream towards flow guiding means arranged laterally of the jet stream. Auxiliary nozzle means open into the main jet stream opposite the flow guiding means and are adapted to form a screen-like fluid obstacle when supplied with air under pressure from the engine compressor which causes the main jet stream to be deflected towards the flow guiding means. In Fig. 2 the downstream portion 49 of the jet nozzle is movable so that when in the extended position shown in the upper half of the Figure an annular orifice 48 is formed. A hollow faired member 45 is supported at the centre of the jet nozzle by struts 46 and when it is desired to deflect the jet stream, air is supplied from the engine compressor through the pipe 46a and issues through the nozzle 47 in the member 45 and causes the jet stream to be deflected through the lateral orifice 48. In Fig. 4 a hollow faired member 53 extends across the downstream end of the jet nozzle which is of rectangular section and air under pressure issues through the slots 54. Flap members 55 are pivotally mounted at the downstream end of the jet nozzle and when in the operative position shown at the upper half of Fig. 4 form a curved path for the deflected jet stream. The deflection of the jet stream may be assisted by applying suction to the slots 58 in the pivoted flaps. In Fig. 8 a hollow faired member 53 is mounted vertically in the jet nozzle and the deflected jet stream issues through lateral orifices 13, 13a which are provided with curved deflector vanes 44. In other embodiments retractable solid deflector members are provided in addition and cause deflection of the jet stream if the deflection caused by the jet of air under pressure is insufficient. Specifications 691,302, 691, 984 [Group XXXIII] and 750, 623 are referred to.

43. 发明专利

DE944287C 未知
公开(公告)号：DE944287C
公开(公告)日：1956-06-14
申请号：DES0040626
申请日：1954-08-31
申请人： SNECMA
发明人： BERTIN JEAN HENRI , KADOSCH MARCEL
IPC分类号： F02K1/56

44. 发明专利

DE942782C 未知
公开(公告)号：DE942782C
公开(公告)日：1956-05-09
申请号：DES0040627
申请日：1954-08-31
申请人： SNECMA
发明人： BERTIN JEAN HENRI , KADOSCH MARCEL
IPC分类号： F02K1/56

45. 发明专利

DE941333C 未知
公开(公告)号：DE941333C
公开(公告)日：1956-04-05
申请号：DES0028717
申请日：1952-05-28
申请人： SNECMA
发明人： KADOSCH MARCEL , GILBERT FRANCOIS , FOLL JEAN LE , BERTIN JEAN
IPC分类号： F02C3/06

46. 发明专利

GB745692A Control of air flow over an aircraft wing 未知
公开(公告)号：GB745692A
公开(公告)日：1956-02-29
申请号：GB2359953
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： B64C23/00
摘要： 745,692. Controlling boundary layer. SOC. NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION. Dec. 31, 1951 [Jan. 4, 1951], No. 23599/53. Divided out of 745,630, [Group XXVI]. Class 4. A device for controlling the flow of air over the upper surface of an aircraft wing comprises nozzle means on a support member spaced from and in the vicinity of said upper surface, said nozzle means opening out opposite said surface and being fed with gas under pressure, the flow of the latter being under the control of a valve. A cambered wing 15 has hollow auxiliary aerofoils 16 mounted above the upper surface and formed with jet orifices 17 which may be normal to the local airflow or inclined thereto. The wings 16 are fed with gas under a pressure which may be varied by a valve incorporated in the supply system.

47. 发明专利

FR64965E 未知
公开(公告)号：FR64965E
公开(公告)日：1955-12-15
申请号：FR64965D
申请日：1953-05-06
申请人： SNECMA
发明人： BERTIN JEAN-HENRI , KADOSCH MARCEL , MAUNOURY FRANCOIS-MARIE-LOUIS
IPC分类号： F02K1/28

48. 发明专利

FR63348E 未知
公开(公告)号：FR63348E
公开(公告)日：1955-09-13
申请号：FR63348D
申请日：1952-12-12
申请人： SNECMA
发明人： BERTIN JEAN-HENRI , KADOSCH MARCEL , GELIN PAUL
IPC分类号： F01D5/14 , F01D17/12 , F02C7/04 , F02K1/28 , F02K1/32 , F02K1/64 , F02K7/02 , F02K7/04 , F02K7/067

49. 发明专利

FR62474E 未知
公开(公告)号：FR62474E
公开(公告)日：1955-06-14
申请号：FR62474D
申请日：1952-02-16
申请人： SNECMA
发明人： MARCHAL RAYMOND-HIPPOLYTE , MAUNOURY FRANCOIS-MARIE-LOUIS , TURINETTI HENRI , KADOSCH MARCEL , BERTIN JEAN
IPC分类号： B64C9/38 , F02K1/32 , F02K1/58

50. 发明专利

FR1088953A 未知
公开(公告)号：FR1088953A
公开(公告)日：1955-03-14
申请号：FR1088953D
申请日：1953-09-01
申请人： SNECMA
发明人： BERTIN JEAN-HENRI , KADOSCH MARCEL
IPC分类号： F02K1/56

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