[go: up one dir, main page]

ES2028657A6 - Self-regulated autogyro - Google Patents

Self-regulated autogyro

Info

Publication number
ES2028657A6
ES2028657A6 ES9100415A ES9100415A ES2028657A6 ES 2028657 A6 ES2028657 A6 ES 2028657A6 ES 9100415 A ES9100415 A ES 9100415A ES 9100415 A ES9100415 A ES 9100415A ES 2028657 A6 ES2028657 A6 ES 2028657A6
Authority
ES
Spain
Prior art keywords
rotor
pair
propellers
rotors
self
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
ES9100415A
Other languages
Spanish (es)
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 ES9100415A priority Critical patent/ES2028657A6/en
Publication of ES2028657A6 publication Critical patent/ES2028657A6/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Landscapes

  • Handcart (AREA)
  • Wind Motors (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)

Abstract

It comprises a pair of propulsion propellers 6,7 and a pair of lift rotors 8,9, and each one of the rotors 8,9 is located behind each one of the propellers 6,7 and in the zone 16 and 17 covered by the air impelled by each one of them, such that the rotors 8,9 are subjected to a lifting force on account of the air impelled by the propellers 6,7. Each pair of wings 10,1112,13 of the rotor 8,9 is integral with a common shaft 18 which rotates about its own axis of symmetry, such that when, on the wing 10,12, on one side of the rotor 8,9, the leading angle is reduced, on the wing 11,13 on the other side the leading angle increases, the leading angle being inverted on each one of the wings 10,1112,13 when each one of them is in the position of the other, when the rotor 8,9 turns through half a revolution. Self-regulation of the cyclic passage effect and an increase in the lifting force are achieved.
ES9100415A 1991-02-18 1991-02-18 Self-regulated autogyro Expired - Lifetime ES2028657A6 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES9100415A ES2028657A6 (en) 1991-02-18 1991-02-18 Self-regulated autogyro

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES9100415A ES2028657A6 (en) 1991-02-18 1991-02-18 Self-regulated autogyro

Publications (1)

Publication Number Publication Date
ES2028657A6 true ES2028657A6 (en) 1992-07-01

Family

ID=8271268

Family Applications (1)

Application Number Title Priority Date Filing Date
ES9100415A Expired - Lifetime ES2028657A6 (en) 1991-02-18 1991-02-18 Self-regulated autogyro

Country Status (1)

Country Link
ES (1) ES2028657A6 (en)

Similar Documents

Publication Publication Date Title
BR9001816A (en) AIRCRAFT WITH PAIR OF ROTATION ROTORS IN THE OTHERWISE
DE60300840D1 (en) whiz
ES439834A1 (en) Wind turbine
ES413589A1 (en) Aircraft transporter
GB1531511A (en) Rotary device driven by a moving fluid
EP0095908A3 (en) Speed control apparatus
GB1205757A (en) Improvements in or relating to rotor heads for rotary wing aircraft
GB1269417A (en) Improvements in or relating to aircraft
AU3005789A (en) Blade for high-performance shrouded propeller, multi-blade shrouded propeller provided with such blades and tail rotor arrangement with shrouded propeller for rotary wing aircraft
JPS6432144A (en) Flutter excitor
JPS6429700A (en) Multistage fluidic machine
GB1308023A (en) Bladed rotors
HU9603281D0 (en) Propeller propulsion unit for aircraft
ES2028657A6 (en) Self-regulated autogyro
CA2075752A1 (en) Increasing Lift on Helicopter Rotor Blades and Airplane Propellers
WO1989008580A3 (en) Energy efficient asymmetric pre-swirl vane and twisted propeller propulsion system
GB1176828A (en) An Improved Flying Toy.
GB1467712A (en) Helicopter rotor hub
ATE146943T1 (en) HEAT PROTECTION DEVICE, SUCH AS PARASOL, HAVING A SOLAR-POWERED VENTILATION SYSTEM
GB1519368A (en) Air separator
GB598878A (en) Improvements in or relating to rotary wing aircraft
GB1507503A (en) Means for producing lift
FR2453287A1 (en) Wind-driven motor for energy generation - uses staggered rotor stages each with stator vanes directing wind against circumferential rotor blades
RU94011879A (en) Method and device for control of resultant aerodynamic force of propeller
GB920894A (en) Improvements in or relating to aircraft

Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 19991102