JPS6483494A - Shortening device of landing gliding distance - Google Patents

Shortening device of landing gliding distance

Info

Publication number
JPS6483494A
JPS6483494A JP23709187A JP23709187A JPS6483494A JP S6483494 A JPS6483494 A JP S6483494A JP 23709187 A JP23709187 A JP 23709187A JP 23709187 A JP23709187 A JP 23709187A JP S6483494 A JPS6483494 A JP S6483494A
Authority
JP
Japan
Prior art keywords
flap
aircraft
landing
upward
operated
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.)
Pending
Application number
JP23709187A
Other languages
Japanese (ja)
Inventor
Yasutaka Kimura
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries 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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP23709187A priority Critical patent/JPS6483494A/en
Publication of JPS6483494A publication Critical patent/JPS6483494A/en
Pending legal-status Critical Current

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Abstract

PURPOSE: To achieve shortening of a landing run distance by composing a flap of an aircraft to be operated upward automatically or manually after grounding at the time of landing for generating negative lift downward to improve braking effect by friction with a road surface. CONSTITUTION: An aircraft comprises main wings 1, flaps 3', and legs 11. In this case, the flap 3' is composed in such a way that it can be operated more upward than a neutral position. A flap actuation operation device 12 is mounted on an airframe for determining if the aircraft is grounded or not, determining if upward operation of the flap 3' is to be conducted automatically or manually, giving drive command for the flap 3', etc. When the aircraft is running at a specified speed V after landing, the flap 3' is operated upward to generate negative lift L downward. A large friction is thus generated between the aircraft and a road surface, so aircraft braking effect is improved. Landing run distance can thus be shortened.
JP23709187A 1987-09-24 1987-09-24 Shortening device of landing gliding distance Pending JPS6483494A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP23709187A JPS6483494A (en) 1987-09-24 1987-09-24 Shortening device of landing gliding distance

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP23709187A JPS6483494A (en) 1987-09-24 1987-09-24 Shortening device of landing gliding distance

Publications (1)

Publication Number Publication Date
JPS6483494A true JPS6483494A (en) 1989-03-29

Family

ID=17010274

Family Applications (1)

Application Number Title Priority Date Filing Date
JP23709187A Pending JPS6483494A (en) 1987-09-24 1987-09-24 Shortening device of landing gliding distance

Country Status (1)

Country Link
JP (1) JPS6483494A (en)

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