Patent US4695013A successfully refreshed from Google Patents.
US4695013A
Expired / Lapsed
US
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Landing aid
Assignee: Individual
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Filing: 1984-10-10
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Granted: 1987-09-22
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Expires: 2004-10-10
Abstract
Abstract A warning device, for a helicopter with a tail rotor and a mechanical protection device therefor, for giving during emergency power-loss landings a flare signal to the pilot to initiate flare followed by a tail/ground contact warning signal when the helicopter tail approaches too closely the ground. The warning device comprises in one embodiment a height-finder with two switchable transmitting/receiving antennas mounted at the helicopter tail to produce respectively, when switched into use, a height-finding beam backwards and obliquely downwards or forwards and obliquely downwards. Height signals obtained initially using antenna 40 are processed by computing means and initiate at a predetermined initial flare altitude a flare warning signal whereafter height signals from antenna 26 are used to determine the sink rate of the tail and in dependence upon this sink rate and the instantaneous height, a warning signal is initiated if this corresponds to a predetermined relative relationship. The higher the sink rate, the greater is the height at which the tail/ground contact warning signal is initiated and vice versa. In a second embodiment, the height-finder uses a single beam the main axis of which extends backwards and obliquely downwards but of which the lobe pattern is broad enough such that vertical height measurement can be made with the helicopter in both the flare and pre-flare situation.
Inventors
- 👤 Ulrich Trampnau
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-31 17:05
CPC Classifications
B; B64; B64C; B64C27/00; B64C27/006
Claims Analysis
Total Claims: 11
Claim 1
Independent Claim
162 words
A landing aid, for a helicopter with a tail rotor, for assisting a pilot to carry out a simulated or real auto-rotation landing, said landing aid comprising means for giving a height-measurement by transmitting and receiving high frequency electromagnetic wave beams, positioned at a tail of a helicopter, said high frequency electromagnetic wave beam having an axis which is directed backwardly and obliquely downward from the tail of the helicopter, means for calculating the tail height responsive to a receipt of the reflected electromagnetic wave signals; computing means for computing the tail sink rate responsive to at least one of said height measurements or reflected electromagnetic wave signal, means for providing a flare signal to tell a pilot when to start a landing flare, and means for providing a warning signal to tell a pilot when to stop the landing flare responsive to the tail sink rate relative to its instantaneous height and a corresponding value indicating a danger of a tail/ground.
Claim 2
Dependent Claim
162 words
A landing aid, for a helicopter with a tail rotor, for assisting a pilot to carry out a simulated or real auto-rotation landing, said landing aid comprising means for giving a height-measurement by transmitting and receiving high frequency electromagnetic wave beams, positioned at a tail of a helicopter, said high frequency electromagnetic wave beam having an axis which is directed backwardly and obliquely downward from the tail of the helicopter, means for calculating the tail height responsive to a receipt of the reflected electromagnetic wave signals; computing means for computing the tail sink rate responsive to at least one of said height measurements or reflected electromagnetic wave signal, means for providing a flare signal to tell a pilot when to start a landing flare, and means for providing a warning signal to tell a pilot when to stop the landing flare responsive to the tail sink rate relative to its instantaneous height and a corresponding value indicating a danger of a tail/ground.
Claim 3
Dependent Claim
85 words
The landing aid according to claim 1 wherein the transmitting and receiving means comprise at least a first means for transmitting said high frequency electromagnetic wave beam or first and second transmitting and receiving beams, means for transmitting a second high frequency electromagnetic wave beam directed substantially vertically downwardly, and wherein the height calculation means is effected responsive to the second beam signals prior to the giving of the flare signal and responsive to said first beam signal after the giving of said flare signal.
Claim 4
Dependent Claim
64 words
The landing aid according to claim 1 wherein said high frequency electromagnetic wave beam is sufficiently broad to ensure that both when the helicopter is at a customary auto-rotation attitude in a descent prior to flare and when it is in the steepest normal flare attitude, reflected wave signals are receivable from the ground substantially vertically below the tail mounted transmitting and receiving means.
Claim 5
Dependent Claim
39 words
The landing aid according to claim 1 and means for giving the flare and warning signals to a pilot head-set via a connector interposed in a normal connection between the head-set and standard radio equipment located on said helicopter.
Claim 6
Dependent Claim
92 words
The landing aid according to claim 1 wherein said height-measuring means is in a first "add-on" module containing its own power supply in a housing with means for releasably clamping the housing to the helicopter tail; the means for generator the flare and warning signals is in a second module which is removable positioned in a cabin of said helicopter and which is connectable to the helicopter power supply; and the first module has signal transmitting means for transmitting height and speed information signals to signal receiving means for the second module.
Claim 7
Dependent Claim
59 words
The landing aid according to claim 2 wherein the height-measuring means and said means for transmitting and receiving beams are formed by a single height determining radar equipment feeding two separate transmit/receive antennas via a switching arrangement, one of said transmit/receive antennas being for the first beam and the other of said transmit/receive antennas being for the second beam.
Claim 8
Dependent Claim
45 words
The landing aid according to claim 2 and means wherein on take-off the operative height-measuring beam is said first beam, and means for changing the operative beam from the first to the second beam as soon as the helicopter exceeds a predetermined initial flare altitude.
Claim 9
Dependent Claim
18 words
The landing aid according to claim 6 wherein the signal transmitting and signal receiving means are electro-optical means.
Claim 10
Dependent Claim
18 words
The landing aid according to claim 6 wherein the signal transmitting and signal receiving means are radio devices.
Claim 11
Dependent Claim
73 words
The landing aid according to claim 3 wherein the height measuring means is a radar height-finding unit having transmitting and receiving means comprising a transmitting antenna and a receiving antenna spaced not more than about 15 cm apart, means for transmitting a radiation which has a carrier frequency between 26.5 and 40 GHz, and a band width which is such that a height measurement accuracy of better than approximately ±15 cm is obtained.
References Cited (Backward Citations)
US2412003A
Cited
US3279724A
Cited
US3375518A
Cited
US3765766A
Cited
US3979717A
Cited
US4027838A
Cited
US4293840A
Cited
US4241346A
Cited
US4528564A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1990-09-21 | 1991-03-23 | 1991-09-22 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1994-09-21 | 1995-03-23 | 1995-09-22 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1998-09-21 | 1999-03-23 | 1999-09-22 | $7700.00 | Window Closed / Lapsed |