RU95122096A - Flying vehicle water landing system - Google Patents

Flying vehicle water landing system

Info

Publication number
RU95122096A
RU95122096A RU95122096/11A RU95122096A RU95122096A RU 95122096 A RU95122096 A RU 95122096A RU 95122096/11 A RU95122096/11 A RU 95122096/11A RU 95122096 A RU95122096 A RU 95122096A RU 95122096 A RU95122096 A RU 95122096A
Authority
RU
Russia
Prior art keywords
water
helicopter
pressure accumulators
flying vehicle
landing system
Prior art date
Application number
RU95122096/11A
Other languages
Russian (ru)
Other versions
RU2089453C1 (en
Inventor
В.В. Смольников
Б.Н. Ильичев
В.М. Пестов
Ю.Л. Макаревич
А.И. Бычков
Original Assignee
Научно-производственное объединение "Искра"
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 Научно-производственное объединение "Искра" filed Critical Научно-производственное объединение "Искра"
Priority to RU9595122096A priority Critical patent/RU2089453C1/en
Publication of RU95122096A publication Critical patent/RU95122096A/en
Application granted granted Critical
Publication of RU2089453C1 publication Critical patent/RU2089453C1/en

Links

Classifications

    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Emergency Lowering Means (AREA)

Abstract

FIELD: lifesaving appliances; emergency landing of helicopters on water. SUBSTANCE: system has inflatable floats connected with independent pressure accumulators. Pressure accumulators are mounted together with floats on helicopter case for rotation about longitudinal axis. EFFECT: reduced mass, enhanced stability of helicopter on water and improved operational characteristics of system.

Claims (1)

Изобретение относится к спасательным средствам, применяемым в аварийных ситуациях на воде, и может быть использовано для аварийной посадки летательных аппаратов, например вертолетов. Система содержит надувные поплавки, газосвязанные с автономными аккумуляторами давления. Аккумуляторы давления с закрепленными на них поплавками установлены на корпусе вертолета с возможностью вращения вокруг своей продольной оси. Предлагаемое изобретение позволяет снизить массу конструкции, повысить устойчивость вертолета во время нахождения его в воде, улучшить эксплуатационные характеристики системы.The invention relates to rescue equipment used in emergency situations on the water, and can be used for emergency landing of aircraft, such as helicopters. The system contains inflatable floats, gas-connected with autonomous pressure accumulators. Pressure accumulators with floats fixed to them are mounted on the helicopter body with the possibility of rotation around its longitudinal axis. The present invention allows to reduce the mass of the structure, to increase the stability of the helicopter while it is in the water, to improve the operational characteristics of the system.
RU9595122096A 1995-12-27 1995-12-27 Flying vehicle water landing system RU2089453C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU9595122096A RU2089453C1 (en) 1995-12-27 1995-12-27 Flying vehicle water landing system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU9595122096A RU2089453C1 (en) 1995-12-27 1995-12-27 Flying vehicle water landing system

Publications (2)

Publication Number Publication Date
RU95122096A true RU95122096A (en) 1996-12-10
RU2089453C1 RU2089453C1 (en) 1997-09-10

Family

ID=20175169

Family Applications (1)

Application Number Title Priority Date Filing Date
RU9595122096A RU2089453C1 (en) 1995-12-27 1995-12-27 Flying vehicle water landing system

Country Status (1)

Country Link
RU (1) RU2089453C1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2678220B1 (en) * 2011-02-25 2017-10-11 Archimedes Pty Ltd Buoyancy system
RU2678238C1 (en) * 2017-08-31 2019-01-24 Акционерное общество "Долгопрудненское конструкторское бюро автоматики" Inflatable chassis of aircraft
RU2678243C1 (en) * 2017-08-31 2019-01-24 Акционерное общество "Долгопрудненское конструкторское бюро автоматики" Aircraft inflatable chassis float
RU2678728C1 (en) * 2017-08-31 2019-01-31 Акционерное общество "Долгопрудненское конструкторское бюро автоматики" Inflatable chassis of aircraft
PL244467B1 (en) 2019-10-09 2024-01-29 Adaptronica Spolka Z Ograniczona Odpowiedzialnoscia Adaptive emergency landing device for a flying object, especially for an unmanned aerial vehicle
RU2767566C1 (en) * 2021-09-15 2022-03-17 Акционерное общество "Национальный центр вертолетостроения им. М.Л. Миля и Н.И. Камова" (АО "НЦВ Миль и Камов") Helicopter emergency ballonet system

Also Published As

Publication number Publication date
RU2089453C1 (en) 1997-09-10

Similar Documents

Publication Publication Date Title
RU93043825A (en) COMBINED AIRCRAFT
CA2349076A1 (en) Safety system for a helicopter
SE8402466D0 (en) NEGATIVE INCREASE WARNING SYSTEM AFTER STARTING
RU95122096A (en) Flying vehicle water landing system
WO2003026959A3 (en) Emergency floatation system for helicopters
GB1514347A (en) Helicopter rotors
DE3378036D1 (en) Air craft structure for take-off and landing on the feet of the pilot
RU92011037A (en) AIRCRAFT EMERGENCY DRIVE SYSTEM
RU94018410A (en) Flying vehicle landing gear retraction and extension drive
RU1819797C (en) Airship
RU94031383A (en) System of emergency landing of flying vehicles with main rotor
RU1773804C (en) Parachute system
RU94031384A (en) Emergency landing system for flying vehicles with main rotor
RU94009357A (en) COMBINED AVIATION SYSTEM OF FLIGHT SAFETY
JPS62113691A (en) Balloon floating in air and disaster marking tool using said balloon
RU2075861C1 (en) METHOD FOR EMERGENCY LEAVING THE AIRCRAFT CREW
RU93051846A (en) UNIVERSAL HOUSING OF THE AIRCRAFT
Phelan Affordable start
RU94040257A (en) Method of rescue of flying vehicle
SWANSON et al. Unique crew escape concepts for ATS mission aircraft
KUGLER Air rescue service in the Federal Republic of Germany Requirements for the helicopter
JPS62113690A (en) Balloon floating in air and disaster marking tool using said balloon
GILLESPIE Helicopter Pilot/Copilot survival system
Knoche Night rescue operation procedure over sea with bell UH-1 D helicopters
RU93032526A (en) MULTI-PUPPING PARASHCLE SYSTEM