GB948590A - Flutter damper - Google Patents
Flutter damperInfo
- Publication number
- GB948590A GB948590A GB27762/62A GB2776262A GB948590A GB 948590 A GB948590 A GB 948590A GB 27762/62 A GB27762/62 A GB 27762/62A GB 2776262 A GB2776262 A GB 2776262A GB 948590 A GB948590 A GB 948590A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shaft
- housing
- chambers
- fluid
- bore
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fluid-Damping Devices (AREA)
Abstract
948,590. Hydraulic dampers. LIONELPACIFIC Inc. July 19, 1962, No. 27762/62. Heading F2S. An hydraulic damper comprises a housing having a chamber 24 at least part of which is cylindrical, the chamber being closed at each end by members 46, 60 which are provided with bores coaxial with the chamber and forming a clearance fit for a shaft 20. The shaft 20 and the cylindrical chamber wall are provided with at least one longitudinal vane 80, 82, 84 and rib 26, 28, 30 respectively, which rib(s) extends between closure members 46, 60, there being a small clearance between the adjacent faces of the rib(s) and shaft and of the vane(s) and chamber wall. In the construction shown, six variable chambers (a), (b), (c), (d), (e) and (f) are formed in the housing. The shaft 20 is mounted at each end in bearings 53, 66 which are pre-loaded by members 58, 70 screwed into the housing. A temperature-sensitive metering device is housed in a bore 168 of shaft 20. The device includes a stack of bi-metallic thermostatic elements 182 mounted on a rod 180 which is adjustably positioned in the bore 168 by screw members 174, 176. The thermostatic elements at one end engage a washer 194 of a spring-loaded valve element 190, the position of which varies the metering effect between ports 212, 216 and a groove 200 of an axially tapered depression 198 in the valve element 190. Variable chambers (a), (c) and (e) communicate with groove 200 through ports 206, 208, 210 and ports 202, 203, 204 respectively and chambers (b), (d) and (f) communicate with bore 164 through ports 218, 220, 222 (not shown). Thus in operation fluid may pass from one set of variable chambers to the other set through the tapered depression 198. A reservoir housing 14 is formed integral with the shaft housing, the reservoir being provided with a spring- loaded piston 100 having a bore in which a fluid filling device 118, 122, 124 and a filtering device 116 are positioned. Pressurized fluid is fed into the two sets of variable chambers through commo n passage 130 and then through branch passages 136, 134 (not shown) and ball valves 144, 145 (not shown). Bleed chambers, passages and grooves for escaping fluid and gases which may have been entrained in the damping fluid are formed at each end of the shaft housing, these chambers, passages and grooves being vented through ducts 160, 162 into the fluid reservoir.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB27762/62A GB948590A (en) | 1962-07-19 | 1962-07-19 | Flutter damper |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB27762/62A GB948590A (en) | 1962-07-19 | 1962-07-19 | Flutter damper |
Publications (1)
Publication Number | Publication Date |
---|---|
GB948590A true GB948590A (en) | 1964-02-05 |
Family
ID=10264856
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB27762/62A Expired GB948590A (en) | 1962-07-19 | 1962-07-19 | Flutter damper |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB948590A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2457042A1 (en) * | 1974-01-02 | 1975-07-10 | Messier Fa | ROTARY SHOCK ABSORBER |
GB2145798A (en) * | 1983-09-01 | 1985-04-03 | Fichtel & Sachs Ag | Volume compensation in hydraulic rotary-vane dampers |
CN103195855A (en) * | 2013-04-28 | 2013-07-10 | 伊卡路斯(苏州)车辆系统有限公司 | Hydraulic buffer system for rotary dampers |
-
1962
- 1962-07-19 GB GB27762/62A patent/GB948590A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2457042A1 (en) * | 1974-01-02 | 1975-07-10 | Messier Fa | ROTARY SHOCK ABSORBER |
GB2145798A (en) * | 1983-09-01 | 1985-04-03 | Fichtel & Sachs Ag | Volume compensation in hydraulic rotary-vane dampers |
CN103195855A (en) * | 2013-04-28 | 2013-07-10 | 伊卡路斯(苏州)车辆系统有限公司 | Hydraulic buffer system for rotary dampers |
CN103195855B (en) * | 2013-04-28 | 2015-05-20 | 伊卡路斯(苏州)车辆系统有限公司 | Hydraulic buffer system for rotary dampers |
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