GB795050A - Improvements relating to aircraft and aircraft installations - Google Patents

Improvements relating to aircraft and aircraft installations

Info

Publication number
GB795050A
GB795050A GB23809/52A GB2380952A GB795050A GB 795050 A GB795050 A GB 795050A GB 23809/52 A GB23809/52 A GB 23809/52A GB 2380952 A GB2380952 A GB 2380952A GB 795050 A GB795050 A GB 795050A
Authority
GB
United Kingdom
Prior art keywords
aircraft
additional
aerofoil
wing
sept
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
GB23809/52A
Inventor
Alan Arnold Griffith
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB23809/52A priority Critical patent/GB795050A/en
Publication of GB795050A publication Critical patent/GB795050A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant

Abstract

795,050. Reaction propelled aircraft. ROLLSROYCE, Ltd. Sept. 23, 1953 [Sept. 23, 1952], No. 23809 /52. Class 4. An aircraft having a main aerofoil wing structure and an additional aerofoil structure separate from the main wing, which additional structure is arranged to move as a whole with respect to the aircraft to effect control of pitch, roll or yaw, is propelled by an air consuming reaction propulsion means accommodated within said additional structure, the air intake and gas exit being in the leading and trailing edges of said additional aerofoil. A detta-wing aircraft has a main wing structure 10, three tail fins 11 and a two-sectioned tail plane 12, each section being adjustable about an axis 14 and accommodating several gas turbine engines. The air intake may extend substantially along the whole of the leading edge, as described in Specification 656,390. The exhaust gas may pass from the engines to the jet pipes and thence to propelling nozzles or directly to propelling nozzles forming part of the engine. A ram jet engine may be used.
GB23809/52A 1952-09-23 1952-09-23 Improvements relating to aircraft and aircraft installations Expired GB795050A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB23809/52A GB795050A (en) 1952-09-23 1952-09-23 Improvements relating to aircraft and aircraft installations

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB23809/52A GB795050A (en) 1952-09-23 1952-09-23 Improvements relating to aircraft and aircraft installations

Publications (1)

Publication Number Publication Date
GB795050A true GB795050A (en) 1958-05-14

Family

ID=10201660

Family Applications (1)

Application Number Title Priority Date Filing Date
GB23809/52A Expired GB795050A (en) 1952-09-23 1952-09-23 Improvements relating to aircraft and aircraft installations

Country Status (1)

Country Link
GB (1) GB795050A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3240448A (en) * 1962-07-13 1966-03-15 Messerschmitt Ag Tail and elevator construction for airplanes
US3286956A (en) * 1965-07-19 1966-11-22 Douglas Aircraft Co Inc Missile control system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3240448A (en) * 1962-07-13 1966-03-15 Messerschmitt Ag Tail and elevator construction for airplanes
US3286956A (en) * 1965-07-19 1966-11-22 Douglas Aircraft Co Inc Missile control system

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