ES2026022A6 - Self-adjusting slider assembly for an undercarriage weight switch - Google Patents

Self-adjusting slider assembly for an undercarriage weight switch

Info

Publication number
ES2026022A6
ES2026022A6 ES9002509A ES9002509A ES2026022A6 ES 2026022 A6 ES2026022 A6 ES 2026022A6 ES 9002509 A ES9002509 A ES 9002509A ES 9002509 A ES9002509 A ES 9002509A ES 2026022 A6 ES2026022 A6 ES 2026022A6
Authority
ES
Spain
Prior art keywords
switch
self
adjusting slider
undercarriage
slider assembly
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 - Lifetime
Application number
ES9002509A
Other languages
Spanish (es)
Inventor
William Darnell Ramsey
George Harold Bailey
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.)
Bell Helicopter Textron Inc
Original Assignee
Bell Helicopter Textron Inc
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
Priority claimed from US07/424,291 external-priority patent/US5045649A/en
Application filed by Bell Helicopter Textron Inc filed Critical Bell Helicopter Textron Inc
Publication of ES2026022A6 publication Critical patent/ES2026022A6/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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 
    • B64C25/52—Skis or runners
    • 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 
    • B64C2025/325—Alighting gear characterised by elements which contact the ground or similar surface  specially adapted for helicopters

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Body Structure For Vehicles (AREA)
  • Railway Tracks (AREA)

Abstract

Self-adjusting slider assembly for a weight switch on an undercarriage which comprises an assembly bracket rigidly fixed to the support a device fixed to the switch to connect in a sliding manner the switch with the assembly bracket, reacting the said sliding device to the movement of a part which oscillates about a mean position, and whose sliding device maintains the switch at a virtually constant distance from the said mean position of the oscillating part as the mean position varies with respect to the support, whose support is comprised of an aircraft and the said oscillating part is connected to the undercarriage system of the aircraft.
ES9002509A 1989-10-03 1990-10-03 Self-adjusting slider assembly for an undercarriage weight switch Expired - Lifetime ES2026022A6 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/424,291 US5045649A (en) 1989-10-03 1989-10-03 Self-adjusting slide assembly for weight on gear switch

Publications (1)

Publication Number Publication Date
ES2026022A6 true ES2026022A6 (en) 1992-04-01

Family

ID=23682130

Family Applications (1)

Application Number Title Priority Date Filing Date
ES9002509A Expired - Lifetime ES2026022A6 (en) 1989-10-03 1990-10-03 Self-adjusting slider assembly for an undercarriage weight switch

Country Status (3)

Country Link
CA (1) CA2026331A1 (en)
ES (1) ES2026022A6 (en)
IL (1) IL95878A0 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7742846B2 (en) * 2006-06-02 2010-06-22 Sikorsky Aircraft Corporation Surface contact override landing scheme for a FBW rotary-wing aircraft

Also Published As

Publication number Publication date
CA2026331A1 (en) 1991-04-04
IL95878A0 (en) 1991-07-18

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Legal Events

Date Code Title Description
FA2A Application withdrawn

Effective date: 19930217