GB686662A - Improvements relating to direct-acting hydraulic shock-absorbers - Google Patents
Improvements relating to direct-acting hydraulic shock-absorbersInfo
- Publication number
- GB686662A GB686662A GB11481/48A GB1148148A GB686662A GB 686662 A GB686662 A GB 686662A GB 11481/48 A GB11481/48 A GB 11481/48A GB 1148148 A GB1148148 A GB 1148148A GB 686662 A GB686662 A GB 686662A
- Authority
- GB
- United Kingdom
- Prior art keywords
- piston
- cylinder
- valve
- hydraulic shock
- rigid
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F22—STEAM GENERATION
- F22D—PREHEATING, OR ACCUMULATING PREHEATED, FEED-WATER FOR STEAM GENERATION; FEED-WATER SUPPLY FOR STEAM GENERATION; CONTROLLING WATER LEVEL FOR STEAM GENERATION; AUXILIARY DEVICES FOR PROMOTING WATER CIRCULATION WITHIN STEAM BOILERS
- F22D11/00—Feed-water supply not provided for in other main groups
- F22D11/02—Arrangements of feed-water pumps
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D33/00—Equipment for handling moulds
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/001—Shrouded propellers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/36—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto having an ejector
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/10—Sliding-contact bearings for exclusively rotary movement for both radial and axial load
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
- F16F9/06—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium using both gas and liquid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
- F16F9/06—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium using both gas and liquid
- F16F9/066—Units characterised by the partition, baffle or like element
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
- F16F9/32—Details
- F16F9/3207—Constructional features
- F16F9/3214—Constructional features of pistons
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
- F16F9/32—Details
- F16F9/34—Special valve constructions; Shape or construction of throttling passages
- F16F9/3415—Special valve constructions; Shape or construction of throttling passages characterised by comprising plastics, elastomeric or porous elements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
- F16F9/32—Details
- F16F9/34—Special valve constructions; Shape or construction of throttling passages
- F16F9/348—Throttling passages in the form of annular discs or other plate-like elements which may or may not have a spring action, operating in opposite directions or singly, e.g. annular discs positioned on top of the valve or piston body
- F16F9/3482—Throttling passages in the form of annular discs or other plate-like elements which may or may not have a spring action, operating in opposite directions or singly, e.g. annular discs positioned on top of the valve or piston body the annular discs being incorporated within the valve or piston body
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2326/00—Articles relating to transporting
- F16C2326/43—Aeroplanes; Helicopters
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Water Supply & Treatment (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Fluid-Damping Devices (AREA)
Abstract
686,662. Hydraulic shock-absorbers. BOURCIER DE CARBON DE PREVINQUIERES, C. M. L. L. April 27, 1948 [May 31, 1947; July 2, 1947; Jan. 21, 1948; March 10, 1948], Nos. 11481/48, 11482/48, 11483/48 and 11484/48. Class 108 (iii). A direct - acting hydraulic shock - absorber comprises a piston spaced from the cylinder wall so that liquid flows between the outer surface of the piston and the cylinder wall in the form of a thin film the piston having means co-operating with the cylinder wall to centre it in the cylinder. The piston shown in Fig. 3 comprises a series of rigid or resilient washers 10 of less diameter than the cylinder bore, clamped on the piston rod between a pair of end plates 13 which are apertured at 14. The washers 10 may be radially slotted and may (as shown), or may not, Fig. o (not shown), be provided with spacers 12. The washers 10 may be replaced by a solid cylindrical portion occupying about the same axial length and of less diameter than the cylinder bore in order to provide a peripheral liquid-damping clearance. The central portion of reduced diameter may be of material which has a different thermal expansion coefficient from that of the cylinder in order to compensate for changes in viscosity due to temperature changes. The piston may be provided with two axial passages containing respective spring-loaded ball valves 6, 7 (Fig. 9), which relieve excess pressure on either side of the piston. The end plates may each be formed with an abutment of part-cylindrical profile. In the constructions shown in Fig. 9, the cylinder space above the piston includes a chamber 21 separated from the remainder of the space by a head 27. Flow into the space 21 is controlled by a spring-loaded ball valve 22, and flow in the reverse direction by a flap valve 25. Specification 686,723 is referred to. In the Specification as open to inspection under Sect. 91, the valve 25 of Fig. 9 may be rigid with the head 27 which has segmental portions removed which allow flexing of the valve. The bellows 29 may be replaced by a tubular dust shield rigid and concentric with the piston rod 1 and having drain holes at its bottom. This subject-matter does not appear in the Specification as accepted.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR56846T | 1948-03-10 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB686662A true GB686662A (en) | 1953-01-28 |
Family
ID=55070603
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB11481/48A Expired GB686662A (en) | 1948-03-10 | 1948-04-27 | Improvements relating to direct-acting hydraulic shock-absorbers |
Country Status (4)
Country | Link |
---|---|
BE (1) | BE482165A (en) |
CH (1) | CH280928A (en) |
FR (2) | FR948067A (en) |
GB (1) | GB686662A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106704446A (en) * | 2017-01-18 | 2017-05-24 | 常州容大结构减振股份有限公司 | Combined segmentation energy consumption type variable damping viscous damper |
CN106763431A (en) * | 2017-01-17 | 2017-05-31 | 常州容大结构减振股份有限公司 | A kind of rotary Effects of Viscous Fluid Damper |
CN114309519A (en) * | 2020-09-29 | 2022-04-12 | 上海梅山钢铁股份有限公司 | Method for determining elasticity coefficient of load-reducing spring of continuous casting stopper rod flow control mechanism |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2852108A (en) * | 1951-10-11 | 1958-09-16 | Richard B Ransom | Motion damping device |
GB821030A (en) * | 1954-12-06 | 1959-09-30 | Boge Gmbh | Improvements in and relating to hydraulic shock dampers |
US4099602A (en) * | 1977-08-31 | 1978-07-11 | P. L. Porter Company | Hydraulic positioner with bidirectional detenting action |
JPS56120841A (en) * | 1980-02-27 | 1981-09-22 | Nissan Motor Co Ltd | Shock absorber |
-
0
- BE BE482165D patent/BE482165A/xx unknown
-
1947
- 1947-05-31 FR FR948067D patent/FR948067A/en not_active Expired
- 1947-07-02 FR FR56846D patent/FR56846E/en not_active Expired
-
1948
- 1948-04-27 GB GB11481/48A patent/GB686662A/en not_active Expired
- 1948-05-13 CH CH280928D patent/CH280928A/en unknown
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106763431A (en) * | 2017-01-17 | 2017-05-31 | 常州容大结构减振股份有限公司 | A kind of rotary Effects of Viscous Fluid Damper |
CN106704446A (en) * | 2017-01-18 | 2017-05-24 | 常州容大结构减振股份有限公司 | Combined segmentation energy consumption type variable damping viscous damper |
CN114309519A (en) * | 2020-09-29 | 2022-04-12 | 上海梅山钢铁股份有限公司 | Method for determining elasticity coefficient of load-reducing spring of continuous casting stopper rod flow control mechanism |
CN114309519B (en) * | 2020-09-29 | 2024-06-04 | 上海梅山钢铁股份有限公司 | Method for determining spring elastic coefficient of load shedding spring of continuous casting stopper rod flow control mechanism |
Also Published As
Publication number | Publication date |
---|---|
FR56846E (en) | 1952-10-07 |
BE482165A (en) | 1900-01-01 |
CH280928A (en) | 1952-02-15 |
FR948067A (en) | 1949-07-21 |
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