ES8400316A1 - Improvements in the structure of articulated aircraft (Machine-translation by Google Translate, not legally binding) - Google Patents

Improvements in the structure of articulated aircraft (Machine-translation by Google Translate, not legally binding)

Info

Publication number
ES8400316A1
ES8400316A1 ES511626A ES511626A ES8400316A1 ES 8400316 A1 ES8400316 A1 ES 8400316A1 ES 511626 A ES511626 A ES 511626A ES 511626 A ES511626 A ES 511626A ES 8400316 A1 ES8400316 A1 ES 8400316A1
Authority
ES
Spain
Prior art keywords
translation
machine
legally binding
google translate
aircraft
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
ES511626A
Other languages
Spanish (es)
Other versions
ES511626A0 (en
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to ES511626A priority Critical patent/ES8400316A1/en
Publication of ES511626A0 publication Critical patent/ES511626A0/en
Publication of ES8400316A1 publication Critical patent/ES8400316A1/en
Expired legal-status Critical Current

Links

Landscapes

  • Tires In General (AREA)

Abstract

Structure of aircraft-rocket with articulated wings that serve as a landing system.the wings in delta (13) are composed, each of them, of a fixed part solidarity to the fusilage (10) and of another hydraulicly operated mobile that can form with the fixed angles of up to 90j. The mobile part can, also, deploy each side leaves sheets (14 and 15) with which can also form angles of up to 90j. These unfolded structures are formed by a couple of tripods that serve aerodynamic brake and finally, in collaboration with shock absorbers, (20,21 ...), of the support of the ship already stopped. (Machine-translation by Google Translate, not legally binding)
ES511626A 1982-04-01 1982-04-01 Improvements in the structure of articulated aircraft (Machine-translation by Google Translate, not legally binding) Expired ES8400316A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES511626A ES8400316A1 (en) 1982-04-01 1982-04-01 Improvements in the structure of articulated aircraft (Machine-translation by Google Translate, not legally binding)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES511626A ES8400316A1 (en) 1982-04-01 1982-04-01 Improvements in the structure of articulated aircraft (Machine-translation by Google Translate, not legally binding)

Publications (2)

Publication Number Publication Date
ES511626A0 ES511626A0 (en) 1983-11-01
ES8400316A1 true ES8400316A1 (en) 1983-11-01

Family

ID=8484041

Family Applications (1)

Application Number Title Priority Date Filing Date
ES511626A Expired ES8400316A1 (en) 1982-04-01 1982-04-01 Improvements in the structure of articulated aircraft (Machine-translation by Google Translate, not legally binding)

Country Status (1)

Country Link
ES (1) ES8400316A1 (en)

Also Published As

Publication number Publication date
ES511626A0 (en) 1983-11-01

Similar Documents

Publication Publication Date Title
GB2059023B (en) Double fabric retractable self-erecting wing for missile
DE69302242D1 (en) Helicopter fuselage structure
EP0319051A3 (en) Pivotally mounted high energy absorbing aircraft tail skid assembly having predetermined failure mode
JPS5621979A (en) Truck structure for construction vehicle
GB8706134D0 (en) Inflatable aerodynamic wing structure
IT8249118A0 (en) EXTENDABLE RISER COMPLEX FOR SELF-ERECTING RETRACTABLE WINGS, PARTICULARLY FOR MISSILE
AU8843182A (en) Spring-erected telescopic wing support structure
NO175710C (en) System to aid in the control of a helicopter carrying a load, especially during stationary flight
ES8400316A1 (en) Improvements in the structure of articulated aircraft (Machine-translation by Google Translate, not legally binding)
DK140879A (en) AERODYNAMIC SCREEN FOR CABINS FOR HEAVY TRANSPORT VEHICLES
GB2056617B (en) Marine landing structure with omni directional energy absorbing characteristics
RU97100066A (en) AVIATION STARTING COMPLEX
GB2165513B (en) Inflatable aeroplane wing structure
BR7906363A (en) HYDROPNEUMATIC SUSPENSION, ESPECIALLY FOR MOTOR VEHICLES WITH A LOAD PLATFORM
HK36588A (en) An airframe having a self-erecting wing structure
GB2056029B (en) Strut structure for suspending loads under aircraft
RU1821416C (en) Main support of ski-wheeled landing gear of aircraft
JPH02109766A (en) Leg of water-surface gliding boat
IT7921057A0 (en) RUDDER FOR THE AERODYNAMIC GENERATION OF MOMENTS ON AIRPLANES.
IT8040056A0 (en) FAIRING, IN PARTICULAR TO BE APPLIED ON THE ROOF OF THE CABIN OF TRUCKS
ES8801521A1 (en) Extensible launch bridge mechanized from the vehicle that transports it (Machine-translation by Google Translate, not legally binding)
IT8967356A0 (en) FAIRED HELICOPTER WITH RETRACTABLE FLOATER
Roskam Forward swept wings and commuter airplanes
IT8422535V0 (en) FLEXIBLE STICK STRUCTURE, SUITABLE FOR BINDING AND ALLOWING TO GOVERN THE VEHICLE OF VEHICLES IN GENERAL FOR CHILDREN.
ES291430U (en) New perfected aircraft (Machine-translation by Google Translate, not legally binding)