FR845638A - Suspension device applicable, for example, to aircraft landing gear - Google Patents

Suspension device applicable, for example, to aircraft landing gear

Info

Publication number
FR845638A
FR845638A FR845638DA FR845638A FR 845638 A FR845638 A FR 845638A FR 845638D A FR845638D A FR 845638DA FR 845638 A FR845638 A FR 845638A
Authority
FR
France
Prior art keywords
suspension device
landing gear
aircraft landing
device applicable
applicable
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
Other languages
French (fr)
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.)
Kronprinz GmbH
Original Assignee
Kronprinz GmbH
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 Kronprinz GmbH filed Critical Kronprinz GmbH
Application granted granted Critical
Publication of FR845638A publication Critical patent/FR845638A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F16F9/344—Vortex flow passages
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/58—Arrangements or adaptations of shock-absorbers or springs
    • B64C25/60—Oleo legs

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR845638D 1937-11-10 1938-11-04 Suspension device applicable, for example, to aircraft landing gear Expired FR845638A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE845638X 1937-11-10

Publications (1)

Publication Number Publication Date
FR845638A true FR845638A (en) 1939-08-29

Family

ID=6774860

Family Applications (1)

Application Number Title Priority Date Filing Date
FR845638D Expired FR845638A (en) 1937-11-10 1938-11-04 Suspension device applicable, for example, to aircraft landing gear

Country Status (1)

Country Link
FR (1) FR845638A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2475173A1 (en) * 1979-12-18 1981-08-07 Stabilus Gmbh CYLINDER AND PISTON DEVICE
EP0045973A2 (en) * 1980-08-13 1982-02-17 Nissan Motor Co., Ltd. Shock absorber
EP0045954A2 (en) * 1980-08-07 1982-02-17 Nissan Motor Co., Ltd. Shock absorber
US4407397A (en) * 1980-10-16 1983-10-04 Nissan Motor Co., Ltd. Shock absorber with pressure-relief mechanism
US4438833A (en) * 1980-10-22 1984-03-27 Stabilus Gmbh Piston for a pneumatic, hydraulic, or hydropneumatic installation
US4442925A (en) * 1980-09-12 1984-04-17 Nissan Motor Co., Ltd. Vortex flow hydraulic shock absorber
US4475635A (en) * 1980-10-14 1984-10-09 Nissan Motor Company, Limited Vortex flow shock absorber with one-way valve
US10578185B2 (en) 2015-09-14 2020-03-03 Kyb Corporation Shock absorber

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2475173A1 (en) * 1979-12-18 1981-08-07 Stabilus Gmbh CYLINDER AND PISTON DEVICE
EP0045954A2 (en) * 1980-08-07 1982-02-17 Nissan Motor Co., Ltd. Shock absorber
EP0045954A3 (en) * 1980-08-07 1983-02-23 Nissan Motor Company, Limited Shock absorber
EP0161430A3 (en) * 1980-08-07 1986-06-25 Nissan Motor Co., Ltd. Shock absorber
EP0161430A2 (en) * 1980-08-07 1985-11-21 Nissan Motor Co., Ltd. Shock absorber
US4502575A (en) * 1980-08-13 1985-03-05 Nissan Motor Company, Limited Shock absorber
EP0045973A2 (en) * 1980-08-13 1982-02-17 Nissan Motor Co., Ltd. Shock absorber
EP0045973A3 (en) * 1980-08-14 1983-01-12 Nissan Motor Company, Limited Shock absorber
US4442925A (en) * 1980-09-12 1984-04-17 Nissan Motor Co., Ltd. Vortex flow hydraulic shock absorber
US4475635A (en) * 1980-10-14 1984-10-09 Nissan Motor Company, Limited Vortex flow shock absorber with one-way valve
US4407397A (en) * 1980-10-16 1983-10-04 Nissan Motor Co., Ltd. Shock absorber with pressure-relief mechanism
US4438833A (en) * 1980-10-22 1984-03-27 Stabilus Gmbh Piston for a pneumatic, hydraulic, or hydropneumatic installation
US10578185B2 (en) 2015-09-14 2020-03-03 Kyb Corporation Shock absorber

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