CA448266A - Fluid pressure control mechanism - Google Patents

Fluid pressure control mechanism

Info

Publication number
CA448266A
CA448266A CA448266A CA448266DA CA448266A CA 448266 A CA448266 A CA 448266A CA 448266 A CA448266 A CA 448266A CA 448266D A CA448266D A CA 448266DA CA 448266 A CA448266 A CA 448266A
Authority
CA
Canada
Prior art keywords
fluid pressure
pressure control
control mechanism
fluid
pressure
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
CA448266A
Other languages
French (fr)
Inventor
S. Sanford Roy
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 Westinghouse Automotive Air Brake Co
Original Assignee
Bendix Westinghouse Automotive Air Brake Co
Publication date
Application granted granted Critical
Publication of CA448266A publication Critical patent/CA448266A/en
Expired legal-status Critical Current

Links

CA448266A Fluid pressure control mechanism Expired CA448266A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA448266T

Publications (1)

Publication Number Publication Date
CA448266A true CA448266A (en) 1948-05-04

Family

ID=35565954

Family Applications (1)

Application Number Title Priority Date Filing Date
CA448266A Expired CA448266A (en) Fluid pressure control mechanism

Country Status (1)

Country Link
CA (1) CA448266A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4907760A (en) * 1988-05-18 1990-03-13 The Boeing Company Contracting landing gear shock strut
US5775677A (en) * 1995-02-07 1998-07-07 Englund; Arlo C. Air or gas sprung and dampened shock absorber
US5908174A (en) * 1996-10-31 1999-06-01 Coltec Industries Inc. Automatic shrink shock strut for an aircraft landing gear

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4907760A (en) * 1988-05-18 1990-03-13 The Boeing Company Contracting landing gear shock strut
US5775677A (en) * 1995-02-07 1998-07-07 Englund; Arlo C. Air or gas sprung and dampened shock absorber
US5908174A (en) * 1996-10-31 1999-06-01 Coltec Industries Inc. Automatic shrink shock strut for an aircraft landing gear

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