IT1255907B - Veicolo aereo ultraleggero, in particolare elicottero. - Google Patents

Veicolo aereo ultraleggero, in particolare elicottero.

Info

Publication number
IT1255907B
IT1255907B ITMI922433A ITMI922433A IT1255907B IT 1255907 B IT1255907 B IT 1255907B IT MI922433 A ITMI922433 A IT MI922433A IT MI922433 A ITMI922433 A IT MI922433A IT 1255907 B IT1255907 B IT 1255907B
Authority
IT
Italy
Prior art keywords
helicopter
ultralight
air vehicle
plane
length
Prior art date
Application number
ITMI922433A
Other languages
English (en)
Original Assignee
Crae Elettromeccanica Spa
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 Crae Elettromeccanica Spa filed Critical Crae Elettromeccanica Spa
Priority to ITMI922433A priority Critical patent/IT1255907B/it
Publication of ITMI922433A0 publication Critical patent/ITMI922433A0/it
Priority to AU51549/93A priority patent/AU5154993A/en
Priority to BR9307278A priority patent/BR9307278A/pt
Priority to PCT/IT1993/000092 priority patent/WO1994010033A1/en
Priority to ZA936671A priority patent/ZA936671B/xx
Priority to CN93118478A priority patent/CN1086184A/zh
Priority to AR93326329A priority patent/AR248246A1/es
Publication of ITMI922433A1 publication Critical patent/ITMI922433A1/it
Application granted granted Critical
Publication of IT1255907B publication Critical patent/IT1255907B/it

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/12Rotor drives
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/08Geodetic or other open-frame structures
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/52Skis or runners
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/12Rotor drives
    • B64C27/14Direct drive between power plant and rotor hub
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C2025/325Alighting gear characterised by elements which contact the ground or similar surface  specially adapted for helicopters
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
  • Tires In General (AREA)
  • Inorganic Compounds Of Heavy Metals (AREA)
  • Current-Collector Devices For Electrically Propelled Vehicles (AREA)
  • Powder Metallurgy (AREA)
  • Toys (AREA)
  • Body Structure For Vehicles (AREA)

Abstract

E' descritto un veicolo aereo ultraleggero, in particolare un elicottero, rientrante nei limiti di peso a vuoto di circa 230 kg e di peso massimo di 450 kg e la cui lunghezza (L) è compresa fra 4950 e 5150 mm. La struttura (50), costituente l'ossatura caratteristica dell'elicottero, è formata da una serie di aste tubolari in lega di titanio, concorrenti in una pluralità di nodi centrali (KC1... KC4) giacenti sul piano di simmetria dell'elicottero e di coppia di nodi laterali (KL1... KL7) simmetrici rispetto al piano stesso, la cui posizione nello spazio, riferita ad una terna di assi, viene definita in funzione della lunghezza (M) della struttura stessa scelta come parametro di base.(Fig. 1)
ITMI922433A 1992-10-23 1992-10-23 Veicolo aereo ultraleggero, in particolare elicottero. IT1255907B (it)

Priority Applications (7)

Application Number Priority Date Filing Date Title
ITMI922433A IT1255907B (it) 1992-10-23 1992-10-23 Veicolo aereo ultraleggero, in particolare elicottero.
AU51549/93A AU5154993A (en) 1992-10-23 1993-09-08 An ultralight aircraft, in particular a helicopter
BR9307278A BR9307278A (pt) 1992-10-23 1993-09-08 Aeronave ultraleve mais especificamente um helicóptero
PCT/IT1993/000092 WO1994010033A1 (en) 1992-10-23 1993-09-08 An ultralight aircraft, in particular a helicopter
ZA936671A ZA936671B (en) 1992-10-23 1993-09-09 An ultralight aircraft in particular a helicopter
CN93118478A CN1086184A (zh) 1992-10-23 1993-10-14 超轻型直升飞机
AR93326329A AR248246A1 (es) 1992-10-23 1993-10-20 Una aeronave ultraliviana, en particular un helicoptero.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ITMI922433A IT1255907B (it) 1992-10-23 1992-10-23 Veicolo aereo ultraleggero, in particolare elicottero.

Publications (3)

Publication Number Publication Date
ITMI922433A0 ITMI922433A0 (it) 1992-10-23
ITMI922433A1 ITMI922433A1 (it) 1994-04-23
IT1255907B true IT1255907B (it) 1995-11-17

Family

ID=11364159

Family Applications (1)

Application Number Title Priority Date Filing Date
ITMI922433A IT1255907B (it) 1992-10-23 1992-10-23 Veicolo aereo ultraleggero, in particolare elicottero.

Country Status (7)

Country Link
CN (1) CN1086184A (it)
AR (1) AR248246A1 (it)
AU (1) AU5154993A (it)
BR (1) BR9307278A (it)
IT (1) IT1255907B (it)
WO (1) WO1994010033A1 (it)
ZA (1) ZA936671B (it)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102774492B (zh) * 2012-06-08 2016-03-30 无锡汉和航空技术有限公司 一种小型无人直升机机身
CN103523199A (zh) * 2013-09-29 2014-01-22 郭献民 一种新型管式结构电动无人直升机
CN103738504B (zh) * 2014-01-06 2017-04-19 深圳市大疆创新科技有限公司 飞行器的装载支架、飞行器及其减震方法
CN105329435A (zh) * 2014-12-19 2016-02-17 四川精石航空科技开发有限公司 一种管式超轻型直升飞机的机架
CN105235896B (zh) * 2015-10-20 2017-04-12 洲际联合超伦科技(北京)有限公司 一种多功能轻型无人直升机

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2818226A (en) * 1951-11-20 1957-12-31 Hiller Helicopters Rotary wing aircraft frame construction
NL6500474A (it) * 1964-09-26 1966-03-28
US3520497A (en) * 1968-06-05 1970-07-14 Rotorway Inc Framework for a helicopter

Also Published As

Publication number Publication date
CN1086184A (zh) 1994-05-04
ZA936671B (en) 1994-04-29
AU5154993A (en) 1994-05-24
WO1994010033A1 (en) 1994-05-11
BR9307278A (pt) 1999-06-01
AR248246A1 (es) 1995-07-12
ITMI922433A1 (it) 1994-04-23
ITMI922433A0 (it) 1992-10-23

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Legal Events

Date Code Title Description
0001 Granted
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19971029