GB1117582A – An improved aircraft fuselage tail formation
– Google Patents
GB1117582A – An improved aircraft fuselage tail formation
– Google Patents
An improved aircraft fuselage tail formation
Info
Publication number
GB1117582A
GB1117582A
GB7081/66A
GB708166A
GB1117582A
GB 1117582 A
GB1117582 A
GB 1117582A
GB 7081/66 A
GB7081/66 A
GB 7081/66A
GB 708166 A
GB708166 A
GB 708166A
GB 1117582 A
GB1117582 A
GB 1117582A
Authority
GB
United Kingdom
Prior art keywords
aircraft fuselage
improved aircraft
fuselage tail
tail formation
engines
Prior art date
1965-07-15
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
GB7081/66A
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.)
1965-07-15
Filing date
1966-02-17
Publication date
1968-06-19
1966-02-17
Application filed by Individual
filed
Critical
Individual
1968-06-19
Publication of GB1117582A
publication
Critical
patent/GB1117582A/en
Status
Expired
legal-status
Critical
Current
Links
Espacenet
Global Dossier
Discuss
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
B64D27/16—Aircraft characterised by the type or position of power plant of jet type
B64D27/20—Aircraft characterised by the type or position of power plant of jet type within or attached to fuselage
B—PERFORMING OPERATIONS; TRANSPORTING
B64—AIRCRAFT; AVIATION; COSMONAUTICS
B64C—AEROPLANES; HELICOPTERS
B64C5/00—Stabilising surfaces
B64C5/06—Fins
Abstract
1,117,582. Aircraft engines and tail mountings. H. HERTEL. 17 Feb., 1966 [15 July, 1965], No. 7081/66. Headings B7G and B7W. A spar extends rearwardly from the rear-end of an aircraft fuselage, and carries the tail and a plurality of engines. Two jet propulsion engines 1 may be arranged one on each side of the spar 2 or more than two may be arranged on individual struts arranged in star formation (Fig. 5, not shown).
GB7081/66A
1965-07-15
1966-02-17
An improved aircraft fuselage tail formation
Expired
GB1117582A
(en)
Applications Claiming Priority (1)
Application Number
Priority Date
Filing Date
Title
DEH56590A
DE1241273B
(en)
1965-07-15
1965-07-15
Airplane with at least one jet engine on the fuselage tail
Publications (1)
Publication Number
Publication Date
GB1117582A
true
GB1117582A
(en)
1968-06-19
Family
ID=7159443
Family Applications (1)
Application Number
Title
Priority Date
Filing Date
GB7081/66A
Expired
GB1117582A
(en)
1965-07-15
1966-02-17
An improved aircraft fuselage tail formation
Country Status (5)
Country
Link
US
(1)
US3455523A
(en)
JP
(1)
JPS4829356B1
(en)
DE
(1)
DE1241273B
(en)
GB
(1)
GB1117582A
(en)
NL
(1)
NL6600041A
(en)
Families Citing this family (10)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
US3971535A
(en)
*
1973-01-05
1976-07-27
The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration
Oblique-wing supersonic aircraft
US4629147A
(en)
*
1984-10-16
1986-12-16
The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration
Over-the-wing propeller
US4901950A
(en)
*
1986-12-31
1990-02-20
Judge Richard J
Aircraft fuselage
JPH06255587A
(en)
*
1993-03-09
1994-09-13
Honda Motor Co Ltd
Aircraft
US5779191A
(en)
*
1996-11-12
1998-07-14
Brislawn; Mark G.
Pylon flap for increasing negative pitching moments
US6089504A
(en)
*
1997-07-21
2000-07-18
Williams Internaitonal Co., L.L.C.
Single engine aircraft
US6170780B1
(en)
*
1997-07-21
2001-01-09
Sam Barlow Williams
Twin engine aircraft
US6199795B1
(en)
*
1997-07-21
2001-03-13
Samuel B. Williams
Twin engine aircraft
US7017508B2
(en)
*
2002-07-12
2006-03-28
Arthur Vanmoor
Hydrodynamically and aerodynamically optimized leading and trailing edge configurations
US10112696B2
(en)
*
2012-11-12
2018-10-30
United Technologies Corporation
Stabilizer sacrificial surfaces
Family Cites Families (6)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
US2863620A
(en)
*
1952-10-04
1958-12-09
Sud Aviation
Jet-propelled aircraft
US2958480A
(en)
*
1953-06-30
1960-11-01
Saulnier Raymond
Aircraft with low aspect-ratio wing
US2969938A
(en)
*
1956-09-17
1961-01-31
Vickers Armstrongs Aircraft
Variable sweepback airplane
US3075728A
(en)
*
1959-07-02
1963-01-29
Kogan Alexandre
Jet airplane engine mounting
GB894797A
(en)
*
1959-10-09
1962-04-26
Rolls Royce
Jet noise silencing apparatus for an aircraft
US3237891A
(en)
*
1964-05-13
1966-03-01
British Aircraft Corp Ltd
Jet-propulsion power-plants for aircraft
1965
1965-07-15
DE
DEH56590A
patent/DE1241273B/en
active
Pending
1966
1966-01-04
NL
NL6600041A
patent/NL6600041A/xx
unknown
1966-02-17
GB
GB7081/66A
patent/GB1117582A/en
not_active
Expired
1966-04-20
JP
JP41024681A
patent/JPS4829356B1/ja
active
Pending
1966-07-11
US
US564287A
patent/US3455523A/en
not_active
Expired – Lifetime
Also Published As
Publication number
Publication date
DE1241273B
(en)
1967-05-24
US3455523A
(en)
1969-07-15
JPS4829356B1
(en)
1973-09-10
NL6600041A
(en)
1967-01-16
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None