DE740221C - Device for braking a nose-wheel aircraft landing on a ship's deck - Google Patents

Device for braking a nose-wheel aircraft landing on a ship's deck

Info

Publication number
DE740221C
DE740221C DEH164674D DEH0164674D DE740221C DE 740221 C DE740221 C DE 740221C DE H164674 D DEH164674 D DE H164674D DE H0164674 D DEH0164674 D DE H0164674D DE 740221 C DE740221 C DE 740221C
Authority
DE
Germany
Prior art keywords
nose
wheel
brake cable
braking
ship
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
DEH164674D
Other languages
German (de)
Inventor
Kurt Paarmann
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.)
Heinkel Flugzeugwerke E GmbH
Original Assignee
Heinkel Flugzeugwerke E GmbH
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 Heinkel Flugzeugwerke E GmbH filed Critical Heinkel Flugzeugwerke E GmbH
Priority to DEH164674D priority Critical patent/DE740221C/en
Application granted granted Critical
Publication of DE740221C publication Critical patent/DE740221C/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/68—Arrester hooks

Description

Einrichtung zum Abbremsen eines auf einem Schiffsdeck landenden Bugradflugzeuges Die Erfindung bezieht sich auf eine Einrichtung zum Abbremsen eines auf einem Schiffsdeck landenden Bugradflugzeuges.Device for braking a nose-wheel aircraft landing on a ship's deck The invention relates to a device for braking an on a ship deck landing nose-wheel aircraft.

Es ist bekannt, Bugradflugzeuge bei ihrer Landung auf einem Schiffsdeck mit kurzer Landestrecke durch ein quer zur Landerichtung gespanntes Bremsseil abzubremsen, das von einer am Flugzeug in Flugrichtung hinter dem Bugradfahrwerk angebrachten Fangvorrichtung aufgefangen wird. Um zu vermeiden, daß das Flugzeug bereits mit seinem Bugrad bzw. Bugradfahrwerk gegen das Bremsseil anläuft und sich dadurch gegebenenfalls überschlagen kann, hat man bis.la;ng eine besondere Einrichtung zum Niederhalten des Bremsseiles bis zum Darüberrollen des Bugrades vorgesehen und mit dieser Einrichtung eine weitere Einrichtung vereinigt oder gekuppelt, die vorzugsweise durch das Bugrad ausgelöst wird und dabei das: Bremsseil in die zum Abbremsen des Flugzeuges ge:eignete Höhenlage bringt.It is known to see nose-wheel planes landing on a ship deck to brake with a short landing distance using a brake cable stretched across the landing direction, the one attached to the aircraft in the direction of flight behind the nose wheel landing gear Safety gear is caught. To avoid having the plane already with you his nose wheel or nose wheel landing gear runs against the brake cable and thereby possibly can overturn, you have a special device to hold down until.la; ng of the brake cable to roll over the nose wheel and provided with this device another device united or coupled, preferably through the nose wheel is triggered and the brake cable is in the one suitable for braking the aircraft Altitude brings.

Die Erfindung hat zum Ziel, die bei den bekannten Einrichtungen vorhandenen besouderen Sicherungs- und Auslöseeinrichtungen für das Bremsseil zu vermeiden. Zu diesem Zweck wird gemäß der Erfindung vorgeschlagen, am Hauptfahrwerk des Bugradflugzeuges .einen schräg nach vorn unten auslaufenden Ausleger und am Bugradfahrwerk einen Abweiser für das Bremsseil anzubringen. Der Ausleger dient zum Überführen des Bremsseiles in die für das Hauptfahrwerk geeignete Höhenlage, während der Abweiser das Bremsseil bis zum Darüberrollen des Bugrades niederhält. i In der Zeichnung ist der Erfindungsgegenstand in einem Ausführungsbeispiel, im Schema von der Seite gesehen, dargestellt.The invention aims at the existing in the known devices avoid special safety and release devices for the brake cable. For this purpose it is proposed according to the invention, on the main landing gear of the nose-wheel aircraft .a boom tapering forward and downwards and one on the nose wheel landing gear Attach deflectors for the brake cable. The boom is used to transfer the brake cable to an altitude suitable for the main landing gear, while the deflector pulls the brake cable until the nose wheel rolls over. i The subject of the invention is in the drawing in one embodiment, seen in the diagram from the side, shown.

Es bezeichnet a ein Bugradflugzeug mit Bugrad b. c ist ein am Bugradfahnverk angebrachter Abweiser, der das Bremsseil e während des Darüberrollens des Bugrades b niederhält. Am Hauptfahrwerk i des Flugzeuges ist ein schräg nach vorn unten verlaufender Ausleger g- angebracht, der das Bremsseile in die zum Abbremsen geeignete Höhenlage zwangsläufig überführt.It denotes a a nose wheel aircraft with nose wheel b. c is an am Bugradfahnverk attached deflector, which the brake cable e while rolling over the nose wheel b holds down. On the main landing gear i of the aircraft there is an inclined forward and downward one Boom g-attached that brings the brake cables to the height suitable for braking inevitably transferred.

Claims (1)

PATENTANSPRUCH: Einrichtung zum Abbremsen eines auf einem Schiffsdeck landenden Bugradflugzeuges, bestehend aus .einer am Bugradflugzeug vorgesehenen Fangvorrichtung für ein quer zur Landerichtung gespanntts Bremsseil sowie ,einer das Bremsseil während des Darüberrollens des Bugrades niedrighaltenden Sicherheitseinrichtung, dadurch.' gekennzeichnet, daß am Hauptfahrwerk des Bugradflugzeuges ein schräg nach vorn unten verlaufender, zur Überführung des Bremsseiles (2) in die Bremslage dienender Ausleger (g) und am Bugradfahrwerk als Sicherheitseinrichtung ein Abweiser (c) für das Bremsseil (e) angebracht ist. Zur Abgrenzung des Anmeldungsgegenstandes vom Stand der Technik ist im Erteilungsverfahren in Betracht gezogen worden: deutsche Patentschrift ....... Nr. 279 5z3.PATENT CLAIM: Device for braking a nose-wheel aircraft landing on a ship's deck, consisting of a safety device provided on the nose-wheel aircraft for a brake cable tensioned transversely to the landing direction and a safety device that keeps the brake cable low while the nose wheel rolls over. characterized in that on the main landing gear of the nose-wheel aircraft a cantilever (g) which runs diagonally downwards and serves to transfer the brake cable (2) into the braking position and a deflector (c) for the brake cable (e) is attached to the nose-wheel undercarriage as a safety device. To distinguish the subject of the application from the state of the art, the following was considered in the granting procedure: German patent specification ....... No. 279 5z3.
DEH164674D 1941-02-23 1941-02-23 Device for braking a nose-wheel aircraft landing on a ship's deck Expired DE740221C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DEH164674D DE740221C (en) 1941-02-23 1941-02-23 Device for braking a nose-wheel aircraft landing on a ship's deck

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEH164674D DE740221C (en) 1941-02-23 1941-02-23 Device for braking a nose-wheel aircraft landing on a ship's deck

Publications (1)

Publication Number Publication Date
DE740221C true DE740221C (en) 1943-10-14

Family

ID=7184026

Family Applications (1)

Application Number Title Priority Date Filing Date
DEH164674D Expired DE740221C (en) 1941-02-23 1941-02-23 Device for braking a nose-wheel aircraft landing on a ship's deck

Country Status (1)

Country Link
DE (1) DE740221C (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2954946A (en) * 1957-06-28 1960-10-04 Edgar A O'neil Apparatus for assisting the landing of aircraft
CN110816822A (en) * 2019-12-06 2020-02-21 西安爱生技术集团公司 Be used for unmanned aerial vehicle to block hook band pulley hook head structure

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE279523C (en) *

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE279523C (en) *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2954946A (en) * 1957-06-28 1960-10-04 Edgar A O'neil Apparatus for assisting the landing of aircraft
CN110816822A (en) * 2019-12-06 2020-02-21 西安爱生技术集团公司 Be used for unmanned aerial vehicle to block hook band pulley hook head structure

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