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SU65025A1 - Device for actuating instruments on airplanes - Google Patents

Device for actuating instruments on airplanes

Info

Publication number
SU65025A1
SU65025A1 SU9232A SU9232A SU65025A1 SU 65025 A1 SU65025 A1 SU 65025A1 SU 9232 A SU9232 A SU 9232A SU 9232 A SU9232 A SU 9232A SU 65025 A1 SU65025 A1 SU 65025A1
Authority
SU
USSR - Soviet Union
Prior art keywords
channel
zone
airplanes
wing
actuating instruments
Prior art date
Application number
SU9232A
Other languages
Russian (ru)
Inventor
А.И. Сильман
Original Assignee
А.И. Сильман
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 А.И. Сильман filed Critical А.И. Сильман
Priority to SU9232A priority Critical patent/SU65025A1/en
Application granted granted Critical
Publication of SU65025A1 publication Critical patent/SU65025A1/en

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Description

УСТРОЙСТВО ДЛЯ ПРИВОДА В ДЕЙСТВИЕ ПРИБОРОВ НАDEVICE FOR THE DRIVE IN THE EFFECT OF DEVICES ON

За влено 25  нвпр  1944 года в Нлркомгшиапром за ЛЬ 9232 (331002) Опубликовано 31 августа 1945 годаFiled 25 NPR 1944 in Nlrkomshiaprom for L 9232 (331002) Published on August 31, 1945

Дл  приведени  в действие воздз шных турбинок указател  поворота и других гироскопических приборов «а самолетах прИ.меи ютс  трубки Вентури. Трубки ВентурИ увеличивают лобовое сопротивление и требуют дли.нных путей дл  соединени  с прибсрвми.In order to actuate turntable throttles and other gyroscopic instruments, airplanes use Venturi tubes. Venturi tubes increase drag and require long paths to connect to the ribs.

Предлагаемое устройство дл  привода ;в действие турэинок приборов- на са молетах не требует 1- о;гальзо ван1И  трубок Вентурк и имеет ту особенность, что отводнон канал турбинкк |ВЫ1веден на поверхность крыла или фюзел жа в зоне отрицательных давлений.The proposed device for driving a device does not require a 1-o device; the device turns a turret; one of the galvanic tubes of the Venturk has the peculiarity that the turbine channel |

На чертеже изображен продоль1;ый разрез примерной формы выполнени  детали устройства.The drawing shows a longitudinal section of an exemplary form of the device part.

Отводной канал турбинки выведен на наружную новерхность крыла са1молета или его фюзел жа, над которой, вследствие обтекани  встречным потоком воздуха, «аход тс  зона отрицательных да1вле1ГИЙ . Входн:е 1отверсти1е. дл  воздуха должно быть расположено на позерхности IB зоне положительных да1влений. Турбинка ра.сполагаетс  -бл:иже к устью отводного канала.The branch duct of the impeller is led to the outer surface of the aircraft’s wing or its fuselage, over which, due to the flow of opposite air flow, there is a zone of negative distances. Entrance: e 1 hole. for air, it must be located on surface IB of the positive-pressure zone. The impeller is located -bl: ilk to the mouth of the branch canal.

САМОЛЕТАХAIRCRAFT

Так KaiK разрежение в зоне отрицательных давлений может оказатьс  недостаточным дл  питани  турбинки ;воздухом, то устье 3 канала 4 быть расположено на удобообтехаемой поверхности выступа 2, монтированного на поверхности 1 крыла или фюзел жа в зоне отрицательных давлений. Выходной конец канала 4 может быть окружен подогревающим приспособлением 5 той или иной конструкции дл  предотвращени  оэледенен11Я и занесени  канала -снегом.Since KaiK negative pressure in the zone of negative pressure may be insufficient to supply the turbine with air, then the mouth 3 of channel 4 can be located on the workable surface of the protrusion 2 mounted on the surface 1 of the wing or fuselage in the zone of negative pressure. The output end of the channel 4 may be surrounded by a heating device 5 of one or another structure to prevent ice from entering and channeling by snow.

Предмет изобретени Subject invention

Claims (3)

1.Устройство дл  привода в действие приборов на -самолетах. с применением аюздушной турбинк;:, о т л и чающеес  тем, что отводной канал тхрбинки выведен на понерхнссть крыла или фюзе.т жа в зоне отрицательных давлений.1. A device for operating instruments on aircraft. with the use of ayuzdushnaya turbine;:, about tl and it is so that the discharge channel of the thrbinka is brought to the bottom of the wing or fuse. in the zone of negative pressures. 2. выполнени  устройства по п. 1, от л и ч л ю щ а   с   тем,2. the device according to claim 1, from l and h что устье канала 4 расположено на удобообтекаемой поверхности выступа 2, монтированного на крыле или фюзел жа в зоне отрицательных давлений.that the mouth of channel 4 is located on the streamlined surface of the protrusion 2 mounted on the wing or the fuselage in the zone of negative pressures. 3. Устройство по пп. 1-2, отличающеес  тем, что выходной конец канала 4 окружен3. The device according to PP. 1-2, characterized in that the output end of channel 4 is surrounded подогревающим приспособлением 5 дл  предотвращени  обледенени  и занесени  сиего.м канала.heating device 5 to prevent icing and entry of the seiyem.m channel. / /
SU9232A 1944-01-25 1944-01-25 Device for actuating instruments on airplanes SU65025A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU9232A SU65025A1 (en) 1944-01-25 1944-01-25 Device for actuating instruments on airplanes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU9232A SU65025A1 (en) 1944-01-25 1944-01-25 Device for actuating instruments on airplanes

Related Child Applications (1)

Application Number Title Priority Date Filing Date
SU6950A Division SU60195A1 (en) 1937-04-19 1937-04-19 Method of dephenolization of supra-resin waters

Publications (1)

Publication Number Publication Date
SU65025A1 true SU65025A1 (en) 1944-11-30

Family

ID=48245443

Family Applications (1)

Application Number Title Priority Date Filing Date
SU9232A SU65025A1 (en) 1944-01-25 1944-01-25 Device for actuating instruments on airplanes

Country Status (1)

Country Link
SU (1) SU65025A1 (en)

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