GB563467A - Improvements in aircraft - Google Patents

Improvements in aircraft

Info

Publication number
GB563467A
GB563467A GB4113/42A GB411342A GB563467A GB 563467 A GB563467 A GB 563467A GB 4113/42 A GB4113/42 A GB 4113/42A GB 411342 A GB411342 A GB 411342A GB 563467 A GB563467 A GB 563467A
Authority
GB
United Kingdom
Prior art keywords
plane
flaps
fuselage
ailerons
elevators
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
GB4113/42A
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.)
Phillips & Powis Aircraft Ltd
Original Assignee
Phillips & Powis Aircraft Ltd
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 Phillips & Powis Aircraft Ltd filed Critical Phillips & Powis Aircraft Ltd
Priority to GB4113/42A priority Critical patent/GB563467A/en
Publication of GB563467A publication Critical patent/GB563467A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/12—Canard-type aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Wind Motors (AREA)

Abstract

563,467. Aeroplanes. PHILLIPS & POWIS AIRCRAFT, Ltd., and MILES, G. H. March 27, 1942, No. 4113. [Class 4] A tandem plane aeroplane has camber changing flaps on both planes, the forward plane being fitted in addition with elevators and the rear wing with ailerons. A forward plane 14 is fitted with elevators 13, which do not extend to the wing tips, and with camber varying flaps. The rear plane 15 is swept back and is provided with flaps 19 and ailerons 20. The forward plane 14 is at the lower part of the fuselage and the rear plane at the upper part and both are of lifting section with positive incidence. Power units 16 mounted on the rear plane drive airscrews 17. Rudders 12 are mounted at the tips of the plane 15 or at the rearward extremities of the power unit nacelles, and an additional directional control 18 is provided at the tail of the fuselage. By fitting flaps to both planes their simultaneous use does not alter the trim of the aeroplane. According to the Provisional Specification an engine may drive a further airscrew at the rear of the fuselage.
GB4113/42A 1942-03-27 1942-03-27 Improvements in aircraft Expired GB563467A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB4113/42A GB563467A (en) 1942-03-27 1942-03-27 Improvements in aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4113/42A GB563467A (en) 1942-03-27 1942-03-27 Improvements in aircraft

Publications (1)

Publication Number Publication Date
GB563467A true GB563467A (en) 1944-08-16

Family

ID=9771014

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4113/42A Expired GB563467A (en) 1942-03-27 1942-03-27 Improvements in aircraft

Country Status (1)

Country Link
GB (1) GB563467A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3778926A (en) * 1972-08-11 1973-12-18 Gentle Toy Co Inc Slow-flying aircraft
CN106828872A (en) * 2017-02-10 2017-06-13 北京航空航天大学 The HAE tandem rotor aircraft aerodynamic arrangement of empennage is supported using rear wing high

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3778926A (en) * 1972-08-11 1973-12-18 Gentle Toy Co Inc Slow-flying aircraft
CN106828872A (en) * 2017-02-10 2017-06-13 北京航空航天大学 The HAE tandem rotor aircraft aerodynamic arrangement of empennage is supported using rear wing high
CN106828872B (en) * 2017-02-10 2019-10-29 北京航空航天大学 Using the high rear wing high altitude long time tandem rotor aircraft aerodynamic arrangement of support empennage

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