SE118333C1 - Device to aircraft - Google Patents

Device to aircraft

Info

Publication number
SE118333C1
SE118333C1 SE669344A SE669344A SE118333C1 SE 118333 C1 SE118333 C1 SE 118333C1 SE 669344 A SE669344 A SE 669344A SE 669344 A SE669344 A SE 669344A SE 118333 C1 SE118333 C1 SE 118333C1
Authority
SE
Sweden
Prior art keywords
aircraft
Prior art date
Application number
SE669344A
Other languages
Unknown language ( )
Swedish (sv)
Inventor
N O Belfrage
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 filed Critical
Priority to SE669344A priority Critical patent/SE118333C1/en
Publication of SE118333C1 publication Critical patent/SE118333C1/en

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 
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/001—Devices not provided for in the groups B64C25/02 - B64C25/68
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B64C25/08—Undercarriages non-fixed, e.g. jettisonable
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/001—Devices not provided for in the groups B64C25/02 - B64C25/68
    • B64C2025/008—Comprising means for modifying their length, e.g. for kneeling, for jumping, or for leveling the aircraft
    • 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
SE669344A 1944-08-19 1944-08-19 Device to aircraft SE118333C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SE669344A SE118333C1 (en) 1944-08-19 1944-08-19 Device to aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE669344A SE118333C1 (en) 1944-08-19 1944-08-19 Device to aircraft

Publications (1)

Publication Number Publication Date
SE118333C1 true SE118333C1 (en) 1947-03-11

Family

ID=1951297

Family Applications (1)

Application Number Title Priority Date Filing Date
SE669344A SE118333C1 (en) 1944-08-19 1944-08-19 Device to aircraft

Country Status (1)

Country Link
SE (1) SE118333C1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2965546A1 (en) * 2010-10-05 2012-04-06 Eurocopter France LANDING TRAIN WITH SKATES AND AIRCRAFT PROVIDED WITH SUCH A LANDING TRAIN
WO2014055269A1 (en) * 2012-10-04 2014-04-10 The Boeing Company Configuring landing supports for landing on uneven terrain

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2965546A1 (en) * 2010-10-05 2012-04-06 Eurocopter France LANDING TRAIN WITH SKATES AND AIRCRAFT PROVIDED WITH SUCH A LANDING TRAIN
US8979024B2 (en) 2010-10-05 2015-03-17 Airbus Helicopters Skid landing gear and an aircraft provided with such landing gear
WO2014055269A1 (en) * 2012-10-04 2014-04-10 The Boeing Company Configuring landing supports for landing on uneven terrain
CN104619591A (en) * 2012-10-04 2015-05-13 波音公司 Configuring landing supports for landing on uneven terrain
CN104619591B (en) * 2012-10-04 2016-12-21 波音公司 The method landed on uneven terrain and the aircraft system using the method

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