empennage

Empennage
	The empennage of a Boeing 747-200

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出典(authority):フリー百科事典『ウィキペディア（Wikipedia）』「2015/01/07 13:17:05」(JST)

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The empennage (/ˌɑːmpɨˈnɑːʒ/ or /ˈɛmpɨnɪdʒ/),^[1]^[2] also known as the tail or tail assembly, of most aircraft^[1]^[2] gives stability to the aircraft, in a similar way to the feathers on an arrow;^[3] the term derives from the French for this.^[4] Most aircraft feature an empennage incorporating vertical and horizontal stabilising surfaces which stabilise the flight dynamics of yaw and pitch,^[1]^[2] as well as housing control surfaces.

In spite of effective control surfaces, many early aircraft that lacked a stabilising empennage were virtually unflyable. Even so-called "tailless aircraft" usually have a tail fin (vertical stabiliser). Heavier than air aircraft without any kind of empennage are rare.

Structure

Structurally, the empennage consists of the entire tail assembly, including the fin, the tailplane and the part of the fuselage to which these are attached.^[1]^[2] On an airliner this would be all the flying and control surfaces behind the rear pressure bulkhead.

The front, usually fixed section of the tailplane is called the tailplane or horizontal stabiliser and is used to provide pitch stability. The rear section is called the elevator and is usually hinged to the horizontal stabiliser. The elevator is a movable aerofoil that controls changes in pitch, the up-and-down motion of the aircraft's nose. Some aircraft employ an all-moving stabiliser and elevators in one unit, known as a stabilator.^[1]^[2]

The vertical tail structure (or fin) has a fixed front section called the vertical stabiliser, used to restrict side-to-side motion of the aircraft (yawing). The rear section of the vertical fin is the rudder, a movable aerofoil that is used to turn the aircraft in combination with the ailerons.^[1]^[2]

Some aircraft are fitted with a tail assembly that is hinged to pivot in two axes forward of the fin and stabiliser, in an arrangement referred to as a movable tail. The entire empennage is rotated vertically to actuate the horizontal stabiliser, and sideways to actuate the fin.^[5]

The aircraft's cockpit voice recorder and flight data recorder are often located in the empennage, because the aft of the aircraft provides better protection for these in most aircraft crashes.

Trim

In some aircraft trim devices are provided to eliminate the need for the pilot to maintain constant pressure on the elevator or rudder controls.^[5]^[6]

The trim device may be:

a trim tab on the rear of the elevators or rudder which act to change the aerodynamic load on the surface. Usually controlled by a cockpit wheel or crank.^[5]^[7]
an adjustable stabiliser into which the stabiliser may be hinged at its spar and adjustably jacked a few degrees in incidence either up or down. Usually controlled by a cockpit crank.^[5]^[8]
a bungee trim system which uses a spring to provide an adjustable preload in the controls. Usually controlled by a cockpit lever.^[5]^[6]
an anti-servo tab used to trim some elevators and stabilators as well as increased control force feel. Usually controlled by a cockpit wheel or crank.^[5]
a servo tab used to move the main control surface, as well as act as a trim tab. Usually controlled by a cockpit wheel or crank.^[5]

Multi-engined aircraft often have trim tabs on the rudder to reduce the pilot effort required to keep the aircraft straight in situations of asymmetrical thrust, such as single engine operations.^[7]

Tail configurations

Aircraft empennage designs may be classified broadly according to the fin and tailplane configurations.

The overall shapes of individual tail surfaces (tailplane planforms, fin profiles) are similar to wing planforms.

Tailplanes

The tailplane comprises the tail-mounted fixed horizontal stabiliser and movable elevator. Besides its planform, it is characterised by:

Number of tailplanes - from 0 (tailless or canard) to 3 (Roe triplane)
Location of tailplane - mounted high, mid or low on the fuselage, fin or tail booms.
Fixed stabiliser and movable elevator surfaces, or a single combined stabilator or flying tail.^[9] (General Dynamics F-111)

Some locations have been given special names:

Cruciform tail - The horizontal stabilisers are placed midway up the vertical stabiliser, giving the appearance of a cross when viewed from the front. Cruciform tails are often used to keep the horizontal stabilisers out of the engine wake, while avoiding many of the disadvantages of a T-tail. Examples include the Hawker Sea Hawk and Douglas A-4 Skyhawk.
T-tail - The horizontal stabiliser is mounted on top of the fin, creating a "T" shape when viewed from the front. T-tails keep the stabilisers out of the engine wake, and give better pitch control. T-tails have a good glide ratio, and are more efficient on low speed aircraft. However, T-tails are more likely to enter a deep stall, and are more difficult to recover from a spin. T-tails must be stronger, and therefore heavier than conventional tails. T-tails also have a larger radar cross section. Examples include the Gloster Javelin, Boeing 727 and McDonnell Douglas DC-9.

Fuselage mounted

Cruciform

T-tail

Flying tailplane

Fins

The fin comprises the fixed vertical stabiliser and rudder. Besides its profile, it is characterised by:

Number of fins - usually one or two.
Location of fins - on the fuselage (over or under), tailplane, tail booms or wings

Twin fins may be mounted at various points:

Twin tail A twin tail, also called an H-tail, consists of two small vertical stabilisers on either side of the horizontal stabiliser. Examples include the Antonov An-225 Mriya, B-25 Mitchell, Avro Lancaster, and ERCO Ercoupe.
Twin boom A twin boom has two fuselages or booms, with a vertical stabiliser on each, and a horizontal stabiliser between them. Examples include the P-38 Lightning, de Havilland Vampire, Sadler Vampire, and Edgley Optica.
Wing mounted midwing as on the F7U Cutlass or on the wing tips as on the Handley Page Manx and Rutan Long-EZ

Tailplane mounted

Twin tail boom

Wing mounted

Unusual fin configurations include:

No fin - as on the McDonnell Douglas X-36. This configuration is sometimes incorrectly referred to as "tailless".
Multiple fins - examples include the Lockheed Constellation (three), Bellanca 14-13 (three), and the Northrop Grumman E-2 Hawkeye (four).
Ventral fin - underneath the fuselage. Often used in addition to a conventional fin as on the (North American X-15 and Dornier Do 335).

Triple fins

Ventral fin

V and X tails

An alternative to the fin-and-tailplane approach is provided by the V-tail and X-tail designs. Here, the tail surfaces are set at diagonal angles, with each surface contributing to both pitch and yaw. The control surfaces, sometimes called ruddervators, act differentially to provide yaw control (in place of the rudder) and act together to provide pitch control (in place of the elevator).^[1]

V tail: A V-tail can be lighter than a conventional tail in some situations and produce less drag, as on the Fouga Magister trainer, Northrop Grumman RQ-4 Global Hawk RPV and X-37 spacecraft. A V-tail may also have a smaller radar signature. Other aircraft featuring a V-tail include the Beechcraft Model 35 Bonanza, and Davis DA-2. A slight modification to the V-tail can be found on the Waiex and Monnet Moni called a Y-tail.

Inverted V tail:The unmanned Predator uses an inverted V-tail as do the Lazair and Mini-IMP.

X tail: The Lockheed XFV and Convair XFY Pogo both featured "X" tails, which were reinforced and fitted with a wheel on each surface so that the craft could sit on its tail and take off and land vertically.

Pelikan: The Pelikan tail is an all-flying variation on the V tail. It was proposed for the Boeing X-32 but abandoned, and has not yet been used on any aircraft. The design is claimed to have the advantages of greater pitch control and a smaller radar signature.^{[citation needed]}

V-tail

Inverted V-tail

X-tail

Pelikan tail

Box kite tails

Some of the earliest aircraft combined horizontal and vertical stabilisers in a box kite design, such as the 1910 Bristol Boxkite.^{[citation needed]}

Tailless

The DH108 Swallow

A tailless aircraft (often tail-less) traditionally has all its horizontal control surfaces on its main wing surface. It has no horizontal stabiliser - either tailplane or canard foreplane (nor does it have a second wing in tandem arrangement). A 'tailless' type usually still has a vertical stabilising fin (vertical stabiliser) and control surface (rudder). However, NASA adopted the 'tailless' description for the novel X-36 research aircraft which has a canard foreplane but no vertical fin.^{[citation needed]}

The most successful tailless configuration has been the tailless delta, especially for combat aircraft.^{[citation needed]}

References

^ ^a ^b ^c ^d ^e ^f ^g Crane, Dale: Dictionary of Aeronautical Terms, third edition, page 194. Aviation Supplies & Academics, 1997. ISBN 1-56027-287-2
^ ^a ^b ^c ^d ^e ^f Aviation Publishers Co. Limited, From the Ground Up, page 10 (27th revised edition) ISBN 0-9690054-9-0
^ Air Transport Association (10 November 2011). "ATA Airline Handbook Chapter 5: How Aircraft Fly". Archived from the original on 10 November 2011. Retrieved 5 March 2013.
^ "Empennage". Oxford Dictionaries Online. Oxford Dictionaries. Retrieved 5 March 2013.
^ ^a ^b ^c ^d ^e ^f ^g Aviation Publishers Co. Limited, From the Ground Up, page 14 (27th revised edition) ISBN 0-9690054-9-0
^ ^a ^b Reichmann, Helmet: Flying Sailplanes, page 26. Thompson Publications, 1980.
^ ^a ^b Transport Canada: Flight Training Manual 4th Edition, page 12. Gage Educational Publishing Company, 1994. ISBN 0-7715-5115-0
^ Crane, Dale: Dictionary of Aeronautical Terms, third edition, page 524. Aviation Supplies & Academics, 1997. ISBN 1-56027-287-2
^ Anderson, John D., Introduction to Flight, 5th ed, p 517

English Journal

Aqua-[4-(hy-droxy-imino-meth-yl)pyridine-κN](imino-diacetato-κO,N,O')copper(II).

Yang Y, Chai W, Song L, Yang Y, Chen J.
Acta crystallographica. Section E, Structure reports online.Acta Crystallogr Sect E Struct Rep Online.2011 Sep 1;67(Pt 9):m1291-2. doi: 10.1107/S1600536811033459. Epub 2011 Aug 27.
In the title complex, [Cu(C(4)H(5)NO(4))(C(6)H(6)N(2)O)(H(2)O)], conventionally abbreviated Cu(IDA)(4-OXPy)(H(2)O), where IDA is imino-diacetate and 4-OXPy is 4-(hy-droxy-imino-meth-yl)pyridine, the Cu(II) atom exhibits a distorted square-pyramidal coordination geometry, which is constructed from tw
PMID 22065407

Japanese Journal

航空機用高分子系複合材料の動向

吉岡健一
高分子 57(9), 769, 2008-09-01
… Development of inter-laminar toughening technology realized composite empennage of Boeing 777, followed by "plastic airframe" of its new model 787. …
NAID 10024263399

MRJ尾翼桁間構造適用に向けたA-VaRTM技術開発 (航空宇宙特集号)

山下満広,坂川亨,武田文人 [他]
三菱重工技報 45(4), 2-5, 2008
NAID 40016379142

夫婦別姓 : 日本における結婚と姓名変更の政策について(<特集>>日本の言語問題)

マーハジョン C.
社会言語科学 2(1), 25-36, 1999-09-30
結婚とは単に結婚する当人同士の個人的な問題ではなく,社会的な関連性をもつ儀式である.その儀式のなかで,未婚から既婚へのカテゴリーの変化が一番如実に現れるのが「名前」であろう.結婚によって姓名を変更するという行為は,社会によって我々の意識の中にある刷り込みが行われるという意味で心理的な問題であるといえる.結婚後新しい姓を持つということは,人間関係をもう一度最初から新たな形で規定し直す手段である.ある …
NAID 110009569899

Related Pictures

The Empennage C150 empennage The rudder is attached to the back of the Figure 2-10. Empennage components. the fuselage (body), wings, empennage Empennage d'un Airbus A380 Figure 7: Empennage components. PARKZONE_EMPENNAGE_HORIZONTAL_RADIAN