ES371213A1 - Improvements in and relating to aircraft - Google Patents

Improvements in and relating to aircraft

Info

Publication number
ES371213A1
ES371213A1 ES371213A ES371213A ES371213A1 ES 371213 A1 ES371213 A1 ES 371213A1 ES 371213 A ES371213 A ES 371213A ES 371213 A ES371213 A ES 371213A ES 371213 A1 ES371213 A1 ES 371213A1
Authority
ES
Spain
Prior art keywords
box
aircraft
support structure
cabin
driving element
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
ES371213A
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
Priority claimed from DE19691909447 external-priority patent/DE1909447C3/en
Application filed by Individual filed Critical Individual
Publication of ES371213A1 publication Critical patent/ES371213A1/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms

Abstract

Aircraft, characterized by being made up of an external box suspended from a gimbal to a cabin arranged internally by means of a support structure that includes a series of three successive pivot elements that comprise their respective pivot axes, of which each is arranged perpendicular to any other of said axes that follow or proceed immediately, including a driving element to rotate said box on the aforementioned, this driving element being arranged to transmit a rotary force to said frame or box independently of any counterforce that is exerted by said drive element against any part of said support structure or of said cabin. (Machine-translation by Google Translate, not legally binding)
ES371213A 1969-02-25 1969-09-04 Improvements in and relating to aircraft Expired ES371213A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19691909447 DE1909447C3 (en) 1969-02-25 Rotor aircraft
US84538169A 1969-07-28 1969-07-28

Publications (1)

Publication Number Publication Date
ES371213A1 true ES371213A1 (en) 1971-08-16

Family

ID=25757048

Family Applications (1)

Application Number Title Priority Date Filing Date
ES371213A Expired ES371213A1 (en) 1969-02-25 1969-09-04 Improvements in and relating to aircraft

Country Status (8)

Country Link
DK (1) DK138310B (en)
ES (1) ES371213A1 (en)
FI (1) FI49949C (en)
GB (1) GB1277042A (en)
IL (1) IL33471A (en)
NL (1) NL156646B (en)
NO (1) NO133066C (en)
SE (1) SE341132B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FI974008A (en) * 1997-10-21 1999-04-22 Natural Colour Kari Kirjavaine A habitable means of transport
US6308912B1 (en) 1997-10-21 2001-10-30 Natural Colour Kari Kirjavainen Oy Rotorcraft
CN115303495B (en) * 2022-09-03 2023-06-16 北京金朋达航空科技有限公司 RCS adjusting device for aircraft

Also Published As

Publication number Publication date
DK138310C (en) 1979-01-29
IL33471A (en) 1974-06-30
NO133066B (en) 1975-11-24
IL33471A0 (en) 1970-02-19
NO133066C (en) 1976-03-03
FI49949C (en) 1975-11-10
NL156646B (en) 1978-05-16
SE341132B (en) 1971-12-13
FI49949B (en) 1975-07-31
GB1277042A (en) 1972-06-07
DK138310B (en) 1978-08-14
NL6913036A (en) 1970-08-27

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