专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US3472028A Aircraft jet engines having afterburners and adjustable jet pipes 失效
标题翻译：具有后燃机和可调喷射管的飞机喷气发动机
公开(公告)号：US3472028A
公开(公告)日：1969-10-14
申请号：US3472028D
申请日：1968-03-28
申请人： SNECMA
发明人： AUBERT JACQUES , SILHOUETTE JEAN-MAX MARIE
IPC分类号： F02K1/16 , F02K1/17 , F02K1/76 , B64C15/00 , F02K1/18
CPC分类号： F02K1/17 , F02K1/16 , F02K1/76

2. 发明专利

FR2577281B1 未知
公开(公告)号：FR2577281B1
公开(公告)日：1987-03-20
申请号：FR8502022
申请日：1985-02-13
申请人： SNECMA
发明人： LAGRANGE JEAN-PAUL , SILHOUETTE JEAN-MAX MARIE
IPC分类号： F01D11/08 , F01D11/18 , F02C7/20
摘要： A device for maintaining clearance between rotor blades and a surrounding housing is disclosed in which the device radially expands or contracts to match the expansion or contraction of the rotor blade tips. The expansion or contraction of the device is achieved by thermal transfer between the device and the gasses passing over the rotor blades. The device has several alternating segments having different thermal characteristics such that the expansion/contraction characteristics of the rotor blade can be accurately matched by the device.

3. 发明专利

FR2468126A1 未知
公开(公告)号：FR2468126A1
公开(公告)日：1981-04-30
申请号：FR7925647
申请日：1979-10-16
申请人： SNECMA
发明人： SILHOUETTE JEAN-MAX MARIE
IPC分类号： F01D17/06 , F02D25/02 , H02P5/48 , G01P3/04 , G01M15/00 , G05D13/64
摘要： A device for detecting a difference between the speeds of rotation of two revolving shafts wherein a movable body is laid out between two dead-head systems mounted opposite one another and caused to rotate by each of the shafts in such a way that the body is displaced between two end positions, either suddenly if the sum of the tensions of the two systems is positive, or gradually if such sum is negative so as to measure, for example, the difference in speeds in a twin engine jet or to produce control devices or devices to trigger automatic systems.

4. 发明专利

DE3663556D1 TURBINE CYLINDER WITH A DEVICE TO ADJUST THE TIP CLEARANCE BETWEEN THE TURBINE BLADES AND THE CYLINDER 未知
公开(公告)号：DE3663556D1
公开(公告)日：1989-06-29
申请号：DE3663556
申请日：1986-02-11
申请人： SNECMA
发明人： LAGRANGE JEAN-PAUL , SILHOUETTE JEAN-MAX MARIE
IPC分类号： F01D11/08 , F01D11/18
摘要： A device for maintaining clearance between rotor blades and a surrounding housing is disclosed in which the device radially expands or contracts to match the expansion or contraction of the rotor blade tips. The expansion or contraction of the device is achieved by thermal transfer between the device and the gasses passing over the rotor blades. The device has several alternating segments having different thermal characteristics such that the expansion/contraction characteristics of the rotor blade can be accurately matched by the device.

5. 发明专利

FR1375826A 未知
公开(公告)号：FR1375826A
公开(公告)日：1964-10-23
申请号：FR944610
申请日：1963-08-13
申请人： SNECMA
发明人： AUBERT JACQUES , SILHOUETTE JEAN-MAX MARIE , MALACHIER MICHEL HENRI XAVIER
IPC分类号： B64C19/00 , C10M169/00 , F02K3/00 , F02K3/10
摘要： 1,073,534. Reheat fuel control systems. SOC. NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION, Aug. 4, 1964 [Aug. 13, 1963], No. 31206/64. Heading F1J. [Also in Division G3] A gas turbine jet propulsion engine includes a pneumatic regulator acting on the fuel supply to continuously regulate the engine thrust and responsive to the engine compressor delivery pressure reduced by a pressure reduction coefficient which is modulated as a continuous function of the delivery pressure. The pneumatic regulator includes a pressure reducing unit 1 divided into chambers 2, 3 by a partition 4 having an orifice 5, the flow cross-section of which is controlled by a tapered needle 6 attached to evacuated capsules 7 under the action of compressor outlet pressure P 2 of the engine. A reduced pressure # m P 2 , in which # m is the pressure reduction coefficient of unit 1, is transmitted through a pipe 10 to act on reheat fuel control devices. The taper of needle 6 is such that # m is inversely proportional to P 2 . A second orifice 11, opening to ambient pressure P o and controlled by needle 12 manually or automatically in response to Mach meter 13, adapts pressure # m P 2 to the required conditions. In a modified unit (1b), Fig. 4 (not shown), compressor outlet pressure P 2 is applied to the interior of capsules 7 through an electric cock (E 3 ) and to a chamber (3b) through an orifice (15). The reduced pressure # m P 2 is communicated through electric cocks (E 2I , E 2II ) to capsules (D I , D II ) respectively controlling the individual reheat fuel valves in a twin engine installation. During normal reheat operation the cocks (E 2I , E 2II , E 3 ) are closed and the capsules (D I , D II ) are controlled by pressures #P 2 communicated through cocks (E 1I , E 1II ) from conventional reducing units (R I , R II ) respectively, coefficient # being constant. To bring the reducing unit (1b) into operation cocks (E 2I , E 2II , E 3 ) are opened and cocks (E 1I , E 1II ) closed. In a modification, Fig. 5 (not shown), a manometric device (23) connects the chambers containing the capsules (D I , D II ) to put the reducing unit (1b) out of operation in the event of any unbalance.

6. 发明专利

GB2175980B PRESSURE REDUCERS 未知
公开(公告)号：GB2175980B
公开(公告)日：1989-02-01
申请号：GB8612371
申请日：1986-05-21
申请人： SNECMA
发明人： SILHOUETTE JEAN-MAX MARIE
IPC分类号： G05D16/06 , G05D16/04 , F16K31/12

7. 发明专利

FR2577281A1 未知
公开(公告)号：FR2577281A1
公开(公告)日：1986-08-14
申请号：FR8502022
申请日：1985-02-13
申请人： SNECMA
发明人： LAGRANGE JEAN-PAUL , SILHOUETTE JEAN-MAX MARIE
IPC分类号： F01D11/08 , F01D11/18 , F02C7/20
摘要： A device for maintaining clearance between rotor blades and a surrounding housing is disclosed in which the device radially expands or contracts to match the expansion or contraction of the rotor blade tips. The expansion or contraction of the device is achieved by thermal transfer between the device and the gasses passing over the rotor blades. The device has several alternating segments having different thermal characteristics such that the expansion/contraction characteristics of the rotor blade can be accurately matched by the device.

8. 发明专利

DE3266709D1 FILTER APPARATUS FOR A LIQUID CONTAINING DIVERSE IMPURITIES 未知
公开(公告)号：DE3266709D1
公开(公告)日：1985-11-07
申请号：DE3266709
申请日：1982-10-22
申请人： SNECMA
发明人： SILHOUETTE JEAN-MAX MARIE
IPC分类号： B01D33/06 , B01D29/00 , B01D33/00 , B01D35/02 , B01D36/04 , B01D37/04 , F02M37/22 , B01D33/10 , B01D29/02 , B01D29/14 , B01D29/32 , B01D35/12

9. 发明专利

DE3065783D1 FLY-WEIGHT UNLATCHING DEVICE 未知
公开(公告)号：DE3065783D1
公开(公告)日：1984-01-05
申请号：DE3065783
申请日：1980-10-03
申请人： SNECMA
发明人： SILHOUETTE JEAN-MAX MARIE
IPC分类号： G05D13/04 , H01H35/10 , H02K11/00
摘要： A weighted trigger device in which the centrifugal force of weights revolving in conjunction with an input shaft is used to displace a movable element axially and in opposition to the force of a spring in order to trigger a control system. The resistance of the weight system is positive and greater at all points to the resistance of the spring.

10. 发明专利

FR2583817A1 未知
公开(公告)号：FR2583817A1
公开(公告)日：1986-12-26
申请号：FR8509360
申请日：1985-06-20
申请人： SNECMA
发明人： LEJARS CLAUDE ROBERT LOUIS , NAUDET JACKY , SILHOUETTE JEAN-MAX MARIE , STENNELER JACQUES MARIE PIERRE
IPC分类号： F04D29/56 , F01D17/16 , F01D9/02 , F02C7/00

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式