GB947909A - Leak test equipment - Google Patents

Leak test equipment

Info

Publication number
GB947909A
GB947909A GB3614861A GB3614861A GB947909A GB 947909 A GB947909 A GB 947909A GB 3614861 A GB3614861 A GB 3614861A GB 3614861 A GB3614861 A GB 3614861A GB 947909 A GB947909 A GB 947909A
Authority
GB
United Kingdom
Prior art keywords
contacts
circuit
switch
vacuum
relay
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
Application number
GB3614861A
Inventor
Frederick W Martin
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Bendix Corp
Original Assignee
Bendix Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Bendix Corp filed Critical Bendix Corp
Priority to GB3614861A priority Critical patent/GB947909A/en
Publication of GB947909A publication Critical patent/GB947909A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M3/00Investigating fluid-tightness of structures
    • G01M3/02Investigating fluid-tightness of structures by using fluid or vacuum
    • G01M3/26Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M3/00Investigating fluid-tightness of structures
    • G01M3/02Investigating fluid-tightness of structures by using fluid or vacuum
    • G01M3/26Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors
    • G01M3/32Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors for containers, e.g. radiators
    • G01M3/3236Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors for containers, e.g. radiators by monitoring the interior space of the containers

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Examining Or Testing Airtightness (AREA)

Abstract

947,909. Brake testing apparatus. BENDIX CORPORATION. Oct. 9, 1961, No. 36148/61. Heading F2E. Apparatus for testing a vacuum or compressed air servomotor or other pneumatic component of a fluid-pressure braking system to determine its rate of leakage comprises a source of vacuum or pressure to which the component is connected together with a pressuresensitive switch, the switch being connected in a circuit including a " pass " and a " reject " circuit, means for connecting the source to the component and pressure-sensitive switch for a predetermined time after which the " pass " or " reject " circuit is energized according to whether or not a predetermined vacuum or pressure has been reached, and further means for subsequently disconnecting the source if the " pass " circuit has been energized to initiate a further step of the test whereby, if after a further predetermined time the vacuum or pressure remaining is above the predetermined value, the " pass " circuit is again energized, otherwise the " reject " circuit is energized. As shown, the flow of air exhausted from a vacuum servo 22 to be tested by a vacuum source 11 is adjusted to a predetermined rate by a valve 14, the flow being initiated by a solenoid-operated valve 16 which is opened upon energization of its winding 34 resulting from the depression of a START switch and the consequent energization of relay CR1 and closure of contacts CR1-c. This initiates the first step during which a relay TD2 having delayed action contacts TD2 -DAE is also energized. As the degree of vacuum increases the pressure in chamber 46 of pressure-sensitive switch 42 is reduced and acts on a diaphragm 41 which in turn acts on the plunger of a two-way micro-switch VS-1 via a spring 44 which normally maintains its contacts 1, 2 closed. If after the expiry of the time delay the vacuum reached is insufficient to release the plunger of switch VS-1 the contacts TD2-DAE close to energize the " reject " circuit comprising red light R and relay CR2 which opens contacts CR2-b in the " pass " circuit. If, however, the plunger of switch VS-1 is released before expiry of the time delay contacts 1, 2 open and contacts 2, 3 close so that relay TD1 is energized. This relay has instantaneous and delay contacts, the former including contacts TD1-DAE which energize the " pass " circuit to illuminate green light G, contacts TD1-a which open the circuit of relay TD2, and contacts TD1-b which open to de-energize the solenoid valve 16. As a result, the vacuum source is cut off and the pressure in chamber 46 will rise if leakage is present. If, before the expiry of the time delay of relay TD1, the plunger of switch VS-1 is again depressed the " reject " circuit is completed by way of its contacts 1, 2. If, however, the plunger of switch VS-1 is not again depressed before this time has expired the delay contacts TD1-DAE close to energize the " pass " circuit whereupon relay CR3 opens contacts CR3-a in the " reject " circuit. The final result of the test as indicated by the light R of G therefore remains after the component has been removed from the test apparatus until the circuit network is reset by depression of a RESET button.
GB3614861A 1961-10-09 1961-10-09 Leak test equipment Expired GB947909A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3614861A GB947909A (en) 1961-10-09 1961-10-09 Leak test equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3614861A GB947909A (en) 1961-10-09 1961-10-09 Leak test equipment

Publications (1)

Publication Number Publication Date
GB947909A true GB947909A (en) 1964-01-29

Family

ID=10385438

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3614861A Expired GB947909A (en) 1961-10-09 1961-10-09 Leak test equipment

Country Status (1)

Country Link
GB (1) GB947909A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2452095A1 (en) * 1979-03-22 1980-10-17 Dungs Karl Gmbh & Co SEALING TESTING APPARATUS
US5372031A (en) * 1993-07-01 1994-12-13 Harmand; Brice Device for vacuum testing of closed systems
CN112378603A (en) * 2020-11-18 2021-02-19 北京自动化控制设备研究所 Leakage rate detection method and system for atomic gas chamber

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2452095A1 (en) * 1979-03-22 1980-10-17 Dungs Karl Gmbh & Co SEALING TESTING APPARATUS
US5372031A (en) * 1993-07-01 1994-12-13 Harmand; Brice Device for vacuum testing of closed systems
CN112378603A (en) * 2020-11-18 2021-02-19 北京自动化控制设备研究所 Leakage rate detection method and system for atomic gas chamber

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