DE4337850A1 - Rudder, aileron and elevator for front of aircraft - Google Patents

Rudder, aileron and elevator for front of aircraft

Info

Publication number
DE4337850A1
DE4337850A1 DE19934337850 DE4337850A DE4337850A1 DE 4337850 A1 DE4337850 A1 DE 4337850A1 DE 19934337850 DE19934337850 DE 19934337850 DE 4337850 A DE4337850 A DE 4337850A DE 4337850 A1 DE4337850 A1 DE 4337850A1
Authority
DE
Germany
Prior art keywords
rudder
aircraft
aileron
elevator
rudders
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.)
Withdrawn
Application number
DE19934337850
Other languages
German (de)
Inventor
Fritz Hausser
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.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to DE19934337850 priority Critical patent/DE4337850A1/en
Publication of DE4337850A1 publication Critical patent/DE4337850A1/en
Withdrawn legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/08—Aircraft not otherwise provided for having multiple wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/04—Noseplanes

Abstract

The aircraft has on its front, a rudder and/or an aileron and/or an elevator which are for use as an amplifying means for the rear rudders, or as the sole means for directing the aircraft. The front placement of these rudders give a quicker reaction for directing the aircraft.

Description

Stand der TechnikState of the art

Herkömmliche Flugkörper haben die Ruder an der hinteren Seite des Körpers plaziert.Conventional missiles have the rudders on the rear Placed side of the body.

Problemproblem

Der angegebenen Erfindung liegt das Problem zugrunde, die Reaktion des Körpers zu verbessern und schneller zu machen.The stated invention is based on the problem improve the body's response and faster close.

Erzielbare VorteileAchievable advantages

Die mit der Erfindung erzielten Vorteile bestehen insbesondere darin, daß die Flugkörper die an der vorderen Seite des Körpers die Seitenruder und/oder die Querruder und/oder die Höhenruder plaziert haben, als Einzige oder als Verstärkung der hinteren Ruder, reagieren schneller beim Lenken.The advantages achieved with the invention exist especially in that the missiles at the front side of the body the rudder and / or have placed the ailerons and / or the elevators, as the only one or as reinforcement of the rear rudders, react faster when steering.

Form, Länge, Breite und genaue Plazierung der Ruder hängt von der Größe, Form und Geschwindigkeit des des Flugkörpers ab.Shape, length, width and exact position of the rudders depends on the size, shape and speed of the of the missile.

Ein Beispiel von vielen Möglichkeiten ist in der Zeichnung dargestellt.An example of many possibilities is in the Drawing shown.

Claims (1)

Oberbegriff
Flugkörper die an der vorderen Seite die Seitenruder und/oder die Querruder und/oder die Höhenruder plaziert haben, als Einzige oder als Verstärkung der hinteren Ruder.
Kennzeichnender Teil
Flugkörper die an der vorderen Seite die Seitenruder und/oder die Querruder und/oder die Höhenruder als Einzige oder als Verstär­ kung der hinteren Ruder hat, reagieren schneller beim Lenken.Generic term
Missiles that have the rudder and / or aileron and / or elevator placed on the front, as the only one or as reinforcement of the rear rudder.
Characteristic part
Missiles that have the rudder and / or aileron and / or elevator on the front side as the only one or as a reinforcement of the rear rudder react faster when steering.
DE19934337850 1993-11-05 1993-11-05 Rudder, aileron and elevator for front of aircraft Withdrawn DE4337850A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE19934337850 DE4337850A1 (en) 1993-11-05 1993-11-05 Rudder, aileron and elevator for front of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19934337850 DE4337850A1 (en) 1993-11-05 1993-11-05 Rudder, aileron and elevator for front of aircraft

Publications (1)

Publication Number Publication Date
DE4337850A1 true DE4337850A1 (en) 1995-05-18

Family

ID=6501927

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19934337850 Withdrawn DE4337850A1 (en) 1993-11-05 1993-11-05 Rudder, aileron and elevator for front of aircraft

Country Status (1)

Country Link
DE (1) DE4337850A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2001062591A1 (en) * 2000-02-25 2001-08-30 Michael May Aircraft

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2421524A1 (en) * 1973-05-04 1974-11-21 Larson Birgitta Eva Helena VEHICLE WITH A RESISTANCE REDUCING LOW DUCK TAIL
DE1578144B1 (en) * 1964-09-16 1979-06-21 Gen Dynamics Corp Control device for a rotating steering projectile
DE3047389A1 (en) * 1979-12-17 1981-09-17 Motorola, Inc., 60196 Schaumburg, Ill. Canard-type guided missile - has stabiliser at rear end with appreciably less wing span than canard surfaces preceding it
US4917333A (en) * 1988-05-11 1990-04-17 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Actuated forebody strakes
DE3342861A1 (en) * 1982-11-26 1992-05-07 Secr Defence Brit IMPROVEMENTS ON AIRCRAFT AND OTHER HULLS

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1578144B1 (en) * 1964-09-16 1979-06-21 Gen Dynamics Corp Control device for a rotating steering projectile
DE2421524A1 (en) * 1973-05-04 1974-11-21 Larson Birgitta Eva Helena VEHICLE WITH A RESISTANCE REDUCING LOW DUCK TAIL
DE3047389A1 (en) * 1979-12-17 1981-09-17 Motorola, Inc., 60196 Schaumburg, Ill. Canard-type guided missile - has stabiliser at rear end with appreciably less wing span than canard surfaces preceding it
DE3342861A1 (en) * 1982-11-26 1992-05-07 Secr Defence Brit IMPROVEMENTS ON AIRCRAFT AND OTHER HULLS
US4917333A (en) * 1988-05-11 1990-04-17 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Actuated forebody strakes

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
2-161294 A.,M-1022,Sep. 10,1990,Vol.14,No.418 *
Automatic Flight Control Systems, Prentice Hall, New York, 1990, S.3,4 *
JP Patents Abstracts of Japan: 1-217200 A.,M- 899,Nov. 29,1989,Vol.13,No.535 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2001062591A1 (en) * 2000-02-25 2001-08-30 Michael May Aircraft

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Legal Events

Date Code Title Description
8101 Request for examination as to novelty
8105 Search report available
8139 Disposal/non-payment of the annual fee