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WO1989007073A3 - Aircraft - Google Patents

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Info

Publication number
WO1989007073A3
WO1989007073A3 PCT/DE1989/000072 DE8900072W WO8907073A3 WO 1989007073 A3 WO1989007073 A3 WO 1989007073A3 DE 8900072 W DE8900072 W DE 8900072W WO 8907073 A3 WO8907073 A3 WO 8907073A3
Authority
WO
WIPO (PCT)
Prior art keywords
rotors
rotor
aircraft
slipstream
ailerons
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.)
Ceased
Application number
PCT/DE1989/000072
Other languages
German (de)
French (fr)
Other versions
WO1989007073A2 (en
Inventor
F W Weissheimer
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.)
INGEBORG WEISSHEIMER TECHNISCHE und VERMOEGENSVERWA
INGEBORG WEISSHEIMER TECH und
Original Assignee
INGEBORG WEISSHEIMER TECHNISCHE und VERMOEGENSVERWA
INGEBORG WEISSHEIMER TECH und
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 DE3804415A external-priority patent/DE3804415A1/en
Application filed by INGEBORG WEISSHEIMER TECHNISCHE und VERMOEGENSVERWA, INGEBORG WEISSHEIMER TECH und filed Critical INGEBORG WEISSHEIMER TECHNISCHE und VERMOEGENSVERWA
Publication of WO1989007073A2 publication Critical patent/WO1989007073A2/en
Publication of WO1989007073A3 publication Critical patent/WO1989007073A3/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/08—Influencing air flow over aircraft surfaces, not otherwise provided for using Magnus effect
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/003—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage
    • B64C39/005—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage about a horizontal transversal axis

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Retarders (AREA)

Abstract

An aircraft possesses two rotors (13, 14) driven by the engine, which drives the propeller simultaneously. By virtue of the fact that the tail plane is located entirely within the slipstream and that the ailerons and the landing flaps are located behind the rotor in the backwardly-directed airstream which flows over the rotor, optimal flight characteristics are achieved in conjunction with a V-shaped setting of the two rotors (13, 14).
PCT/DE1989/000072 1988-02-08 1989-02-07 Aircraft Ceased WO1989007073A2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DEP3804415.3 1988-02-08
DE3804415A DE3804415A1 (en) 1986-08-09 1988-02-08 Rotor aircraft (rotary-wing aircraft), control systems

Publications (2)

Publication Number Publication Date
WO1989007073A2 WO1989007073A2 (en) 1989-08-10
WO1989007073A3 true WO1989007073A3 (en) 1989-08-24

Family

ID=6347306

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/DE1989/000072 Ceased WO1989007073A2 (en) 1988-02-08 1989-02-07 Aircraft

Country Status (2)

Country Link
AU (1) AU3340089A (en)
WO (1) WO1989007073A2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2022087C (en) * 1990-07-27 1995-02-21 Jean-Paul Picard Topside tangential jet lift device for rotating cylinders
GB9207016D0 (en) * 1992-04-30 1992-05-13 Walden Graeme K Antigravity lift & propulsion and guidance system
US5875627A (en) * 1995-06-07 1999-03-02 Jeswine; William W. Fluid propulsion system for accelerating and directionally controlling a fluid

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1927535A (en) * 1929-10-03 1933-09-19 Zap Dev Corp Aircraft
US2681775A (en) * 1951-05-24 1954-06-22 Orazi Paolo Convertible airplane having autorotatable sustaining elements
US3140065A (en) * 1962-06-27 1964-07-07 Alvarez-Calderon Alberto High lift and control system for aircraft
GB2195308A (en) * 1986-09-23 1988-04-07 Lawrence Albert Holmes Rotating wing aircraft
DE3627085A1 (en) * 1986-08-09 1988-06-23 Weissheimer Geb Wengler Rotor aircraft RO II

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1927535A (en) * 1929-10-03 1933-09-19 Zap Dev Corp Aircraft
US2681775A (en) * 1951-05-24 1954-06-22 Orazi Paolo Convertible airplane having autorotatable sustaining elements
US3140065A (en) * 1962-06-27 1964-07-07 Alvarez-Calderon Alberto High lift and control system for aircraft
DE3627085A1 (en) * 1986-08-09 1988-06-23 Weissheimer Geb Wengler Rotor aircraft RO II
GB2195308A (en) * 1986-09-23 1988-04-07 Lawrence Albert Holmes Rotating wing aircraft

Also Published As

Publication number Publication date
WO1989007073A2 (en) 1989-08-10
AU3340089A (en) 1989-08-25

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