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GB578837A - Improvements in and relating to aircraft - Google Patents

Improvements in and relating to aircraft

Info

Publication number
GB578837A
GB578837A GB13199/41A GB1319941A GB578837A GB 578837 A GB578837 A GB 578837A GB 13199/41 A GB13199/41 A GB 13199/41A GB 1319941 A GB1319941 A GB 1319941A GB 578837 A GB578837 A GB 578837A
Authority
GB
United Kingdom
Prior art keywords
duct
compressor
wing
aircraft
flap
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
GB13199/41A
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.)
WILLIAM HERBERT VICTOR CLARKE
Boulton Paul Aircraft Ltd
Original Assignee
WILLIAM HERBERT VICTOR CLARKE
Boulton Paul 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 WILLIAM HERBERT VICTOR CLARKE, Boulton Paul Aircraft Ltd filed Critical WILLIAM HERBERT VICTOR CLARKE
Priority to GB13199/41A priority Critical patent/GB578837A/en
Publication of GB578837A publication Critical patent/GB578837A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/38—Jet flaps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/30—Wing lift efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

578,837. Propelling aircraft. BOULTON PAUL AIRCRAFT, Ltd., and CLARKE, W. H. V. Oct. 14, 1941, No. 13199. [Class 4] An aircraft wing has one or. more ducts therein for receiving a jet propulsion unit, the duct, or each duct, having an elongated inlet orifice at the leading edge of the wing and an elongated outlet orifice in the upper surface of the wing near the trailing edge, the intermediate portion of the duct being of circular cross-section to accommodate the compressor and combustion chamber of the unit, the change of cross-section along the duct being gradual. A compressor 1 is driven by a turbine 2 to the rear of a combustion chamber 3, and the gases are discharged over the rear flaps 5 or over the ailerons of the wing to increase their effectiveness. A flap 7 at the upper edge of the rear orifice is linked to the flap 5 and remains parallel to it throughout its adjustment range so that the jet is always tangential to the flap or aileron. An electric starting motor at the front of the compressor acts as a generator when the compressor is running.
GB13199/41A 1941-10-14 1941-10-14 Improvements in and relating to aircraft Expired GB578837A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB13199/41A GB578837A (en) 1941-10-14 1941-10-14 Improvements in and relating to aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB13199/41A GB578837A (en) 1941-10-14 1941-10-14 Improvements in and relating to aircraft

Publications (1)

Publication Number Publication Date
GB578837A true GB578837A (en) 1946-07-15

Family

ID=10018637

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13199/41A Expired GB578837A (en) 1941-10-14 1941-10-14 Improvements in and relating to aircraft

Country Status (1)

Country Link
GB (1) GB578837A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2641422A (en) * 1947-02-18 1953-06-09 Rolls Royce Exhaust system for gas turbine engines in aircraft
DE1021249B (en) * 1953-04-08 1957-12-19 Power Jets Res & Dev Ltd Installation on transverse drive surfaces, in particular aircraft wings
US3043538A (en) * 1960-04-11 1962-07-10 Rolls Royce Power plant for use in jet sustained aircraft
DE1198145B (en) * 1958-08-01 1965-08-05 Firth Cleveland Ltd Flow bodies, in particular transverse drive surfaces, with circulation that can be influenced by blowing out flow medium jets
WO2024233976A1 (en) * 2023-05-11 2024-11-14 Cosmic Aerospace, Inc. Aerodynamic lifting structures having embedded engines, and associated systems

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2641422A (en) * 1947-02-18 1953-06-09 Rolls Royce Exhaust system for gas turbine engines in aircraft
DE1021249B (en) * 1953-04-08 1957-12-19 Power Jets Res & Dev Ltd Installation on transverse drive surfaces, in particular aircraft wings
DE1198145B (en) * 1958-08-01 1965-08-05 Firth Cleveland Ltd Flow bodies, in particular transverse drive surfaces, with circulation that can be influenced by blowing out flow medium jets
US3043538A (en) * 1960-04-11 1962-07-10 Rolls Royce Power plant for use in jet sustained aircraft
WO2024233976A1 (en) * 2023-05-11 2024-11-14 Cosmic Aerospace, Inc. Aerodynamic lifting structures having embedded engines, and associated systems

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