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GB635885A - Improvements relating to aircraft landing gear - Google Patents

Improvements relating to aircraft landing gear

Info

Publication number
GB635885A
GB635885A GB13606/48A GB1360648A GB635885A GB 635885 A GB635885 A GB 635885A GB 13606/48 A GB13606/48 A GB 13606/48A GB 1360648 A GB1360648 A GB 1360648A GB 635885 A GB635885 A GB 635885A
Authority
GB
United Kingdom
Prior art keywords
bogie
undercarriage
landing gear
frame
improvements relating
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
GB13606/48A
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.)
Electro Hydraulics Ltd
Original Assignee
Electro Hydraulics Ltd
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 Electro Hydraulics Ltd filed Critical Electro Hydraulics Ltd
Priority to GB13606/48A priority Critical patent/GB635885A/en
Publication of GB635885A publication Critical patent/GB635885A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/02Undercarriages
    • B64C25/08Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/14Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like fore-and-aft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/34Alighting gear characterised by elements which contact the ground or similar surface  wheeled type, e.g. multi-wheeled bogies
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/50Steerable undercarriages; Shimmy-damping
    • B64C25/505Shimmy damping
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/58Arrangements or adaptations of shock-absorbers or springs
    • B64C25/60Oleo legs
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04MTELEPHONIC COMMUNICATION
    • H04M3/00Automatic or semi-automatic exchanges
    • H04M3/40Applications of speech amplifiers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Signal Processing (AREA)
  • Vehicle Cleaning, Maintenance, Repair, Refitting, And Outriggers (AREA)
  • Handcart (AREA)

Abstract

635,885. Aircraft undercarriages. ELECTRO - HYDRAULICS, Ltd., NEILSON, C. B. V., and HOARE, R. G. May 31, 1948, No. 13606. [Class 4] A bogie-type undercarriage is provided with means, such as an auxiliary shockabsorber 6, arranged to bias the bogie 3 into a position in which only the rear wheel or wheels 2 engage the ground at the moment of contact, such a construction reducing the drag load on the undercarriage owing to the fact that only the rear wheel or wheels are set into rotation upon the initial ground engagement. As shown, the shock-absorber 6 may be of the compression type and connected to the rear end of the bogie frame 3, or it may be of the tension type in which case it is connected to the front of the bogie frame, or between the rear of the frame and a downward extension of the undercarriage leg 5.
GB13606/48A 1948-05-31 1948-05-31 Improvements relating to aircraft landing gear Expired GB635885A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB13606/48A GB635885A (en) 1948-05-31 1948-05-31 Improvements relating to aircraft landing gear

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB13606/48A GB635885A (en) 1948-05-31 1948-05-31 Improvements relating to aircraft landing gear

Publications (1)

Publication Number Publication Date
GB635885A true GB635885A (en) 1950-04-19

Family

ID=10026089

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13606/48A Expired GB635885A (en) 1948-05-31 1948-05-31 Improvements relating to aircraft landing gear

Country Status (1)

Country Link
GB (1) GB635885A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0262591A2 (en) * 1986-09-30 1988-04-06 The Boeing Company Two-stage aircraft landing gear
US4869444A (en) * 1986-09-30 1989-09-26 The Boeing Company Adjustable two-stage aircraft landing gear system
GB2563946A (en) * 2017-06-30 2019-01-02 Airbus Operations Ltd Pitch trimmer

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0262591A2 (en) * 1986-09-30 1988-04-06 The Boeing Company Two-stage aircraft landing gear
EP0262591A3 (en) * 1986-09-30 1988-09-07 The Boeing Company Two-stage aircraft landing gear
US4770372A (en) * 1986-09-30 1988-09-13 The Boeing Company Two-stage aircraft landing gear
US4869444A (en) * 1986-09-30 1989-09-26 The Boeing Company Adjustable two-stage aircraft landing gear system
GB2563946A (en) * 2017-06-30 2019-01-02 Airbus Operations Ltd Pitch trimmer
US11014654B2 (en) 2017-06-30 2021-05-25 Airbus Operations Limited Pitch trimmer

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