Improvements relating to Pressure Reducing Valves
1,174,252. Pressure-reducing valves; fluid pressure brakes. DUNLOP CO. Ltd. 7 July, 1967 [9 July, 1966], No. 30930/66.- Headings F2F and F2V. A pressure-reducing valve for an aircraft braking system has a spool 5 slidable in a bore 3 of the body 2 to permit flow of fluid from inlet 10 to outlet 11....
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creator | SAMUEL ERIC HARVEY |
description | 1,174,252. Pressure-reducing valves; fluid pressure brakes. DUNLOP CO. Ltd. 7 July, 1967 [9 July, 1966], No. 30930/66.- Headings F2F and F2V. A pressure-reducing valve for an aircraft braking system has a spool 5 slidable in a bore 3 of the body 2 to permit flow of fluid from inlet 10 to outlet 11. The spool has a bore 19 in which is slidably received a spring-loaded piston 16, the end 21 thereof being subject through ports 20 in the spool to inlet pressure that under normal conditions neutralizes the spring-loading. The inlet pressure acts on an area equal to that of the piston cross-section on the spool while the outlet pressure passes through bores 23, 24 and restriction 18 of a secondary relief valve 25 to act on the whole of the area of the spool end in chamber 26. The spool thus acts as a differential piston reducing the pressure of the fluid passing through the valve. If the inlet pressure drops the spring-loading 30 of the piston 16 compensates to prevent outlet pressure drop. A main relief valve 37 is provided and is connected to a fluid return opening 12 as is a leakage passage 36 which is connected via bore 35 to waist 33 of piston 16. |
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A pressure-reducing valve for an aircraft braking system has a spool 5 slidable in a bore 3 of the body 2 to permit flow of fluid from inlet 10 to outlet 11. The spool has a bore 19 in which is slidably received a spring-loaded piston 16, the end 21 thereof being subject through ports 20 in the spool to inlet pressure that under normal conditions neutralizes the spring-loading. The inlet pressure acts on an area equal to that of the piston cross-section on the spool while the outlet pressure passes through bores 23, 24 and restriction 18 of a secondary relief valve 25 to act on the whole of the area of the spool end in chamber 26. The spool thus acts as a differential piston reducing the pressure of the fluid passing through the valve. If the inlet pressure drops the spring-loading 30 of the piston 16 compensates to prevent outlet pressure drop. A main relief valve 37 is provided and is connected to a fluid return opening 12 as is a leakage passage 36 which is connected via bore 35 to waist 33 of piston 16.</description><language>eng</language><subject>ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL ; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL ; CONTROLLING ; PERFORMING OPERATIONS ; PHYSICS ; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OFVEHICLES ; REGULATING ; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES ; TRANSPORTING ; VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF ; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES ; VEHICLES IN GENERAL</subject><creationdate>1969</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19691217&DB=EPODOC&CC=GB&NR=1174252A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19691217&DB=EPODOC&CC=GB&NR=1174252A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SAMUEL ERIC HARVEY</creatorcontrib><title>Improvements relating to Pressure Reducing Valves</title><description>1,174,252. Pressure-reducing valves; fluid pressure brakes. DUNLOP CO. Ltd. 7 July, 1967 [9 July, 1966], No. 30930/66.- Headings F2F and F2V. A pressure-reducing valve for an aircraft braking system has a spool 5 slidable in a bore 3 of the body 2 to permit flow of fluid from inlet 10 to outlet 11. The spool has a bore 19 in which is slidably received a spring-loaded piston 16, the end 21 thereof being subject through ports 20 in the spool to inlet pressure that under normal conditions neutralizes the spring-loading. The inlet pressure acts on an area equal to that of the piston cross-section on the spool while the outlet pressure passes through bores 23, 24 and restriction 18 of a secondary relief valve 25 to act on the whole of the area of the spool end in chamber 26. The spool thus acts as a differential piston reducing the pressure of the fluid passing through the valve. If the inlet pressure drops the spring-loading 30 of the piston 16 compensates to prevent outlet pressure drop. A main relief valve 37 is provided and is connected to a fluid return opening 12 as is a leakage passage 36 which is connected via bore 35 to waist 33 of piston 16.</description><subject>ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL</subject><subject>BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL</subject><subject>CONTROLLING</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OFVEHICLES</subject><subject>REGULATING</subject><subject>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</subject><subject>TRANSPORTING</subject><subject>VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF</subject><subject>VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES</subject><subject>VEHICLES IN GENERAL</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1969</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDD0zC0oyi9LzU3NKylWKErNSSzJzEtXKMlXCChKLS4uLUpVCEpNKU0GCYYl5pSlFvMwsKYl5hSn8kJpbgZ5N9cQZw_d1IL8-NTigsTk1LzUknh3J0NDcxMjUyNHY8IqABFYKw0</recordid><startdate>19691217</startdate><enddate>19691217</enddate><creator>SAMUEL ERIC HARVEY</creator><scope>EVB</scope></search><sort><creationdate>19691217</creationdate><title>Improvements relating to Pressure Reducing Valves</title><author>SAMUEL ERIC HARVEY</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_GB1174252A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>1969</creationdate><topic>ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL</topic><topic>BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL</topic><topic>CONTROLLING</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OFVEHICLES</topic><topic>REGULATING</topic><topic>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</topic><topic>TRANSPORTING</topic><topic>VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF</topic><topic>VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES</topic><topic>VEHICLES IN GENERAL</topic><toplevel>online_resources</toplevel><creatorcontrib>SAMUEL ERIC HARVEY</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>SAMUEL ERIC HARVEY</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Improvements relating to Pressure Reducing Valves</title><date>1969-12-17</date><risdate>1969</risdate><abstract>1,174,252. Pressure-reducing valves; fluid pressure brakes. DUNLOP CO. Ltd. 7 July, 1967 [9 July, 1966], No. 30930/66.- Headings F2F and F2V. A pressure-reducing valve for an aircraft braking system has a spool 5 slidable in a bore 3 of the body 2 to permit flow of fluid from inlet 10 to outlet 11. The spool has a bore 19 in which is slidably received a spring-loaded piston 16, the end 21 thereof being subject through ports 20 in the spool to inlet pressure that under normal conditions neutralizes the spring-loading. The inlet pressure acts on an area equal to that of the piston cross-section on the spool while the outlet pressure passes through bores 23, 24 and restriction 18 of a secondary relief valve 25 to act on the whole of the area of the spool end in chamber 26. The spool thus acts as a differential piston reducing the pressure of the fluid passing through the valve. If the inlet pressure drops the spring-loading 30 of the piston 16 compensates to prevent outlet pressure drop. A main relief valve 37 is provided and is connected to a fluid return opening 12 as is a leakage passage 36 which is connected via bore 35 to waist 33 of piston 16.</abstract><oa>free_for_read</oa></addata></record> |
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subjects | ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL CONTROLLING PERFORMING OPERATIONS PHYSICS PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OFVEHICLES REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES VEHICLES IN GENERAL |
title | Improvements relating to Pressure Reducing Valves |
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